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src/test/resources/replay/replay-inverse-loc-02.txt
View file @ acf902ea
......@@ -9,7 +9,7 @@ DEM cell: t0 latIndex 123 lonIndex 102 elevation 1.870339491485550e+03
DEM cell: t0 latIndex 124 lonIndex 101 elevation 1.832853313250435e+03
DEM cell: t0 latIndex 124 lonIndex 102 elevation 1.866819199623890e+03
sensor: sensorName s0 nbPixels 2000 position 1.500000000000000e+00 0.000000000000000e+00 -2.000000000000000e-01
inverse location: sensorName s0 latitude -3.930305027145593e-01 longitude 2.502739578717502e+00 elevation 1.853045504720662e+03 minLine 0 maxLine 2000 lightTime true aberration true
inverse location: sensorName s0 latitude -3.930305027145593e-01 longitude 2.502739578717502e+00 elevation 1.853045504720662e+03 minLine 0 maxLine 2000 lightTime true aberration true refraction false
sensor mean plane: sensorName s0 minLine 0 maxLine 2000 maxEval 50 accuracy 1.000000000000000e-02 normal 1.000000000000000e+00 0.000000000000000e+00 0.000000000000000e+00 cachedResults 5 lineNumber 1.753079999999941e+03 date 2012-01-01T12:30:01.12961999999991Z target -4.733584770718903e+06 3.515842173828561e+06 -2.428300713188566e+06 targetDirection 4.440892098500626e-16 -7.496646388847980e-01 6.618178973144536e-01 -1.357198500050715e-08 -1.198160098465607e-08 -1.357198500050715e-08 lineNumber 1.753079999999936e+03 date 2012-01-01T12:30:01.12961999999990Z target -4.733634454810624e+06 3.515791377291927e+06 -2.428292161157289e+06 targetDirection 1.221245327087672e-15 -7.496479456645485e-01 6.618368058373009e-01 -1.357209409884309e-08 -1.198230643978911e-08 -1.357209409884309e-08 lineNumber 1.753080000000098e+03 date 2012-01-01T12:30:01.12962000000015Z target -4.733684171891571e+06 3.515740571824192e+06 -2.428283613116900e+06 targetDirection 2.664535259100376e-15 -7.496312519673904e-01 6.618557139390744e-01 -1.357220357852602e-08 -1.198301226854942e-08 -1.357220357852602e-08 lineNumber 1.753080000000016e+03 date 2012-01-01T12:30:01.12962000000002Z target -4.733734047015606e+06 3.515689711809538e+06 -2.428275079609979e+06 targetDirection 1.110223024625157e-15 -7.496145577933011e-01 6.618746216197999e-01 -1.357231495356307e-08 -1.198371980774984e-08 -1.357231495356307e-08 lineNumber 1.753080000000124e+03 date 2012-01-01T12:30:01.12962000000019Z target -4.733783920649958e+06 3.515638855451895e+06 -2.428266547191616e+06 targetDirection 1.665334536937735e-15 -7.495978631423109e-01 6.618935288794415e-01 -1.357242629275803e-08 -1.198442735245515e-08 -1.357242629275803e-08
sensor datation: sensorName s0 lineNumber 1.000000000000000e+03 date 2012-01-01T12:30:00.00000000000000Z
span: minDate 2012-01-01T12:29:57.50000000000000Z maxDate 2012-01-01T12:30:02.50000000000000Z tStep 1.000000000000000e-03 tolerance 5.000000000000000e+00 inertialFrame EME2000
......@@ -28,14 +28,14 @@ sensor LOS: sensorName s0 date 2012-01-01T12:30:01.12961999999997Z pixelNumber 5
sensor LOS: sensorName s0 date 2012-01-01T12:30:01.12961999999997Z pixelNumber 6 los 0.000000000000000e+00 -7.496980238944815e-01 6.617800790056386e-01
sensor datation: sensorName s0 lineNumber 1.753079999999893e+03 date 2012-01-01T12:30:01.12961999999984Z
inverse location result: lineNumber 1.753079999999893e+03 pixelNumber 5.000000000428289e+00
inverse location: sensorName s0 latitude -3.930323254721546e-01 longitude 2.502727645691323e+00 elevation 1.847490708944211e+03 minLine 0 maxLine 2000 lightTime true aberration true
inverse location: sensorName s0 latitude -3.930323254721546e-01 longitude 2.502727645691323e+00 elevation 1.847490708944211e+03 minLine 0 maxLine 2000 lightTime true aberration true refraction false
sensor datation: sensorName s0 lineNumber 1.753080000000180e+03 date 2012-01-01T12:30:01.12962000000027Z
sensor rate: sensorName s0 lineNumber 1.753080000000180e+03 rate 6.666666666666666e+02
sensor datation: sensorName s0 lineNumber 1.753080000000150e+03 date 2012-01-01T12:30:01.12962000000022Z
sensor LOS: sensorName s0 date 2012-01-01T12:30:01.12962000000022Z pixelNumber 7 los 0.000000000000000e+00 -7.497147156838981e-01 6.617611692196904e-01
sensor datation: sensorName s0 lineNumber 1.753080000000120e+03 date 2012-01-01T12:30:01.12962000000018Z
inverse location result: lineNumber 1.753080000000120e+03 pixelNumber 6.000000000570598e+00
inverse location: sensorName s0 latitude -3.930341476421113e-01 longitude 2.502715716159622e+00 elevation 1.841953904196975e+03 minLine 0 maxLine 2000 lightTime true aberration true
inverse location: sensorName s0 latitude -3.930341476421113e-01 longitude 2.502715716159622e+00 elevation 1.841953904196975e+03 minLine 0 maxLine 2000 lightTime true aberration true refraction false
sensor datation: sensorName s0 lineNumber 1.753080000000450e+03 date 2012-01-01T12:30:01.12962000000067Z
sensor rate: sensorName s0 lineNumber 1.753080000000450e+03 rate 6.666666666666666e+02
sensor LOS: sensorName s0 date 2012-01-01T12:30:01.12962000000027Z pixelNumber 8 los 0.000000000000000e+00 -7.497314069963494e-01 6.617422590127325e-01
......
src/test/resources/replay/replay-inverse-loc-03.txt
View file @ acf902ea
# Rugged library dump file, created on 2015-07-23T14:25:51Z
# all units are SI units (m, m/s, rad ...)
sensor: sensorName s0 nbPixels 2552 position 0.000000000000000e+00 0.000000000000000e+00 0.000000000000000e+00
inverse location: sensorName s0 latitude 1.426113542156674e+00 longitude -8.868185262195961e-01 elevation 3.102209319249422e+01 minLine -23040 maxLine 39851 lightTime false aberration false
inverse location: sensorName s0 latitude 1.426113542156674e+00 longitude -8.868185262195961e-01 elevation 3.102209319249422e+01 minLine -23040 maxLine 39851 lightTime false aberration false refraction false
sensor mean plane: sensorName s0 minLine -23040 maxLine 39851 maxEval 50 accuracy 1.000000000000000e-02 normal 9.994827482027009e-01 -2.652758464258975e-02 1.818029972819145e-02 cachedResults 6 lineNumber 2.496503931691230e+04 date 2015-07-07T18:40:12.48786757028467Z target 5.829885691015603e+05 -7.150938152185429e+05 6.289925119642745e+06 targetDirection -1.574993670955663e-02 8.911384689865436e-02 9.958969132317702e-01 -2.069121568391233e-07 2.118875364268554e-08 -2.069121568391233e-07 lineNumber 2.498990311831761e+04 date 2015-07-07T18:40:12.52680428328538Z target 5.827831035018093e+05 -7.152819110623585e+05 6.290040934506435e+06 targetDirection -1.574653262138034e-02 8.923613956787135e-02 9.958860166231007e-01 -2.106025594148216e-07 6.293169679808365e-08 -2.106025594148216e-07 lineNumber 2.501446735659665e+04 date 2015-07-07T18:40:12.56527188043036Z target 5.825914009565986e+05 -7.154869255677856e+05 6.290306437975926e+06 targetDirection -1.574243698611968e-02 8.937839743168323e-02 9.958733241483490e-01 -2.139580511938570e-07 1.003165269577007e-07 -2.139580511938570e-07 lineNumber 2.503906484840334e+04 date 2015-07-07T18:40:12.60379155259964Z target 5.823982602071301e+05 -7.156902096509174e+05 6.290556499572599e+06 targetDirection -1.573844749711850e-02 8.951962023030334e-02 9.958607025403716e-01 -2.164310151145369e-07 1.276529299636964e-07 -2.164310151145369e-07 lineNumber 2.506393183649445e+04 date 2015-07-07T18:40:12.64273325595032Z target 5.821928312311379e+05 -7.158784186376551e+05 6.290673076115117e+06 targetDirection -1.573492577246402e-02 8.964463942750402e-02 9.958495120914844e-01 -2.189036239175299e-07 1.552935576937779e-07 -2.189036239175299e-07 lineNumber 2.508894303441162e+04 date 2015-07-07T18:40:12.68190079188860Z target 5.819807540563018e+05 -7.160584640312950e+05 6.290717393595084e+06 targetDirection -1.573177124337613e-02 8.976098395370098e-02 9.958390819470831e-01 -2.207684005657831e-07 1.758718590383612e-07 -2.207684005657831e-07
sensor datation: sensorName s0 lineNumber 8.405500000000000e+03 date 2015-07-07T18:39:46.55562900000000Z
span: minDate 2015-07-07T18:38:55.00000000000000Z maxDate 2015-07-07T18:40:35.80000000000000Z tStep 1.000000000000000e-01 tolerance 1.000000000000000e+01 inertialFrame EME2000
......
src/tutorials/java/AffinagePleiades/AffinageRugged.java deleted 100644 → 0
View file @ 4430eac3
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package AffinagePleiades;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.hipparchus.optim.nonlinear.vector.leastsquares.LeastSquaresOptimizer.Optimum;
import java.io.File;
import java.util.Locale;
import java.util.Collections;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataProvidersManager;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitExceptionWrapper;
import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
import org.orekit.orbits.Orbit;
import org.orekit.rugged.api.AlgorithmId;
import org.orekit.rugged.api.BodyRotatingFrameId;
import org.orekit.rugged.api.EllipsoidId;
import org.orekit.rugged.api.InertialFrameId;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.api.RuggedBuilder;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.AngularDerivativesFilter;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.PVCoordinates;
/**
* Parameter estimation context
* @author Jonathan Guinet
*
*/
public class AffinageRugged {
public static void main(String[] args) {
try {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
File home = new File(System.getProperty("user.home"));
//File orekitData = new File(home, "workspace/data/orekit-data");
File orekitData = new File(home, "COTS/orekit-data");
DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
//CreateOrbit
OrbitModel orbitmodel = new OrbitModel();
BodyShape earth = orbitmodel.createEarth();
NormalizedSphericalHarmonicsProvider gravityField = orbitmodel.createGravityField();
//create Pleiades Viewing Model
PleiadesViewingModel pleiadesViewingModel = new PleiadesViewingModel();
AbsoluteDate minDate = pleiadesViewingModel.getMinDate();
AbsoluteDate maxDate = pleiadesViewingModel.getMaxDate();
AbsoluteDate refDate = pleiadesViewingModel.getDatationReference();
Orbit orbit = orbitmodel.createOrbit(gravityField.getMu(), refDate);
PVCoordinates PV = orbit.getPVCoordinates(earth.getBodyFrame());
GeodeticPoint gp = earth.transform(PV.getPosition(), earth.getBodyFrame(), orbit.getDate());
System.out.format(" **** Orbit Definition **** %n");
System.out.format(Locale.US, "Geodetic Point at date %s : φ = %8.10f °, λ = %8.10f %n",orbit.getDate().toString(),
FastMath.toDegrees(gp.getLatitude()),
FastMath.toDegrees(gp.getLongitude()));
System.out.format(" **** Build Viewing Model **** %n");
// Build Rugged ...
RuggedBuilder ruggedBuilder = new RuggedBuilder();
LineSensor lineSensor = pleiadesViewingModel.getLineSensor();
ruggedBuilder.addLineSensor(lineSensor);
ruggedBuilder.setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID);
ruggedBuilder.setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF);
ruggedBuilder.setTimeSpan(minDate,maxDate, 0.001, 5.0).
setTrajectory(InertialFrameId.EME2000,
orbitmodel.orbitToPV(orbit, earth, minDate.shiftedBy(-0.0), maxDate.shiftedBy(+0.0), 0.25),
8, CartesianDerivativesFilter.USE_PV,
orbitmodel.orbitToQ(orbit, earth, minDate.shiftedBy(-0.0), maxDate.shiftedBy(+0.0), 0.25),
2, AngularDerivativesFilter.USE_R);
Rugged rugged = ruggedBuilder.build();
Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
AbsoluteDate firstLineDate = lineSensor.getDate(pleiadesViewingModel.dimension/2);
System.out.format("date %s %n",firstLineDate.toString());
Vector3D los = lineSensor.getLOS(firstLineDate,0);
GeodeticPoint upLeftPoint = rugged.directLocation(firstLineDate, position, los);
System.out.format(Locale.US, "upper left point: φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(upLeftPoint.getLatitude()),
FastMath.toDegrees(upLeftPoint.getLongitude()),
upLeftPoint.getAltitude());
los = lineSensor.getLOS(firstLineDate,pleiadesViewingModel.dimension-1);
GeodeticPoint upRightPoint = rugged.directLocation(firstLineDate, position, los);
System.out.format(Locale.US, "upper right point: φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(upRightPoint.getLatitude()),
FastMath.toDegrees(upRightPoint.getLongitude()),upRightPoint.getAltitude());
los = lineSensor.getLOS(firstLineDate,pleiadesViewingModel.dimension/2);
GeodeticPoint centerPoint = rugged.directLocation(firstLineDate, position, los);
System.out.format(Locale.US, "center point: φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(centerPoint.getLatitude()),
FastMath.toDegrees(centerPoint.getLongitude()),centerPoint.getAltitude());
System.out.format(" **** Add roll and pitch values **** %n");
double rollValue = FastMath.toRadians( 0.1);
double pitchValue = FastMath.toRadians(-0.3);
double factorValue = 0.5;
System.out.format("roll : %3.5f pitch : %3.5f factor : %3.5f \n",rollValue,pitchValue,factorValue);
rugged.
getLineSensor("line").
getParametersDrivers().
filter(driver -> driver.getName().equals("roll")).
findFirst().get().setValue(rollValue);
rugged.
getLineSensor("line").
getParametersDrivers().
filter(driver -> driver.getName().equals("pitch")).
findFirst().get().setValue(pitchValue);
rugged.
getLineSensor("line").
getParametersDrivers().
filter(driver -> driver.getName().equals("factor")).
findFirst().get().setValue(factorValue);
System.out.format(" **** Generate Measures **** %n");
MeasureGenerator measure = new MeasureGenerator(pleiadesViewingModel,rugged);
int lineSampling = 1000;
int pixelSampling = 1000;
measure.CreateMeasure(lineSampling, pixelSampling);
System.out.format("nb TiePoints %d %n", measure.getMeasureCount());
System.out.format(" **** Reset Roll/Pitch/Factor **** %n");
rugged.
getLineSensor(pleiadesViewingModel.getSensorName()).
getParametersDrivers().
filter(driver -> driver.getName().equals("roll") || driver.getName().equals("pitch")).
forEach(driver -> {
try {
driver.setSelected(true);
driver.setValue(0.0);
} catch (OrekitException e) {
throw new OrekitExceptionWrapper(e);
}
});
rugged.
getLineSensor(pleiadesViewingModel.getSensorName()).
getParametersDrivers().
filter(driver -> driver.getName().equals("factor")).
forEach(driver -> {
try {
driver.setSelected(true);
driver.setValue(1.0); // default value: no Z scale factor applied
} catch (OrekitException e) {
throw new OrekitExceptionWrapper(e);
}
});
System.out.format(" **** Initial Residuals **** %n");
LocalisationMetrics initlialResiduals = new LocalisationMetrics(measure.getMapping(),rugged);
System.out.format("residuals max : %3.6e mean %3.6e %n",initlialResiduals.getMaxResidual(),initlialResiduals.getMeanResidual());
System.out.format(" **** Start optimization **** %n");
// perform parameters estimation
int maxIterations = 15;
double convergenceThreshold = 1e-12;
System.out.format("iterations max %d convergence threshold %3.6e \n",maxIterations, convergenceThreshold);
Optimum optimum = rugged.estimateFreeParameters(Collections.singletonList(measure.getMapping()), maxIterations,convergenceThreshold);
System.out.format(" Optimization performed in %d iterations \n",optimum.getEvaluations());
// check estimated values
double estimatedRoll = rugged.getLineSensor(pleiadesViewingModel.getSensorName()).
getParametersDrivers().
filter(driver -> driver.getName().equals("roll")).
findFirst().get().getValue();
double rollError = (estimatedRoll - rollValue);
System.out.format("Estimated roll %3.5f roll error %3.6e %n", estimatedRoll, rollError);
double estimatedPitch = rugged.getLineSensor(pleiadesViewingModel.getSensorName()).
getParametersDrivers().
filter(driver -> driver.getName().equals("pitch")).
findFirst().get().getValue();
double pitchError = (estimatedPitch - pitchValue);
System.out.format("Estimated pitch %3.5f pitch error %3.6e %n ", estimatedPitch, pitchError);
double estimatedFactor = rugged.getLineSensor(pleiadesViewingModel.getSensorName()).
getParametersDrivers().
filter(driver -> driver.getName().equals("factor")).
findFirst().get().getValue();
double factorError = (estimatedFactor - factorValue);
System.out.format("Estimated factor %3.5f factor error %3.6e %n ", estimatedFactor, factorError);
System.out.format(" **** Compute Statistics **** %n");
LocalisationMetrics localisationResiduals = new LocalisationMetrics(measure.getMapping(),rugged);
System.out.format("residuals max : %3.6e mean %3.6e %n",localisationResiduals.getMaxResidual(),localisationResiduals.getMeanResidual());
//RealVector residuals = optimum.getResiduals();
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
} catch (RuggedException re) {
System.err.println(re.getLocalizedMessage());
System.exit(1);
}
}
}
src/tutorials/java/AffinagePleiades/LocalisationMetrics.java deleted 100644 → 0
View file @ 4430eac3
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package AffinagePleiades;
import org.hipparchus.linear.ArrayRealVector;
import org.hipparchus.linear.RealVector;
import org.orekit.rugged.api.SensorToGroundMapping;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.time.AbsoluteDate;
import java.util.Collections;
import java.util.Collection;
import java.util.Map;
import java.util.Set;
import java.util.Iterator;
import java.util.Locale;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
/** class for measure generation
* @author Jonathan Guinet
*/
public class LocalisationMetrics {
/** mapping */
private Set <Map.Entry<SensorPixel, GeodeticPoint>> groundTruthMappings;
private Set <Map.Entry<SensorPixel, GeodeticPoint>> estimationMappings;
private Rugged rugged;
private LineSensor sensor;
private PleiadesViewingModel viewingModel;
private int measureCount;
/* max residual distance */
private double resMax;
/* mean residual distance */
private double resMean;
/** Simple constructor.
* <p>
*
* </p>
*/
public LocalisationMetrics(SensorToGroundMapping groundTruthMapping, Rugged rugged) throws RuggedException
{
groundTruthMappings = groundTruthMapping.getMappings();
this.rugged = rugged;
this.sensor = rugged.getLineSensor(groundTruthMapping.getSensorName());
this.computeMetrics();
}
/** Get the maximum residual;
* @return max residual
*/
public double getMaxResidual() {
return resMax;
}
/** Get the mean residual;
* @return mean residual
*/
public double getMeanResidual() {
return resMean;
}
public void computeMetrics() throws RuggedException {
//final RealVector longDiffVector;
//final RealVector latDiffVector;
//final RealVector altDiffVector;
RealVector distanceVector = new ArrayRealVector();
double count=0;
resMax = 0;
int k = groundTruthMappings.size();
Iterator<Map.Entry<SensorPixel, GeodeticPoint>> gtIt = groundTruthMappings.iterator();
while (gtIt.hasNext()) {
Map.Entry<SensorPixel, GeodeticPoint> gtMapping =gtIt.next();
final SensorPixel gtSP = gtMapping.getKey();
final GeodeticPoint gtGP = gtMapping.getValue();
AbsoluteDate date = sensor.getDate(gtSP.getLineNumber());
GeodeticPoint esGP = rugged.directLocation(date, sensor.getPosition(),
sensor.getLOS(date, (int) gtSP.getPixelNumber()));
double lonDiff = esGP.getLongitude() - gtGP.getLongitude();
double latDiff = esGP.getLatitude() - gtGP.getLatitude();
double altDiff = esGP.getAltitude() - gtGP.getAltitude();
//longDiffVector.append(lonDiff);
//latDiffVector.append(latDiff);
//altDiffVector.append(altDiff);
double distance = Math.sqrt( lonDiff * lonDiff + latDiff * latDiff + altDiff * altDiff );
count += distance;
if (distance > resMax)
{
resMax = distance;
}
//distanceVector.append(distance);
}
//resMax = distanceVector.getMaxValue();
//System.out.format(Locale.US, "max: %3.6e %n ",distanceVector.getMaxValue() );
resMean = count / k ;
//System.out.format("number of points %d %n", k);
}
}
src/tutorials/java/AffinagePleiades/MeasureGenerator.java deleted 100644 → 0
View file @ 4430eac3
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package AffinagePleiades;
import org.orekit.rugged.api.SensorToGroundMapping;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.time.AbsoluteDate;
import org.orekit.bodies.GeodeticPoint;
/** class for measure generation
* @author Jonathan Guinet
*/
public class MeasureGenerator {
/** mapping */
private SensorToGroundMapping mapping;
private Rugged rugged;
private LineSensor sensor;
private PleiadesViewingModel viewingModel;
private int measureCount;
/** Simple constructor.
* <p>
*
* </p>
*/
public MeasureGenerator(PleiadesViewingModel viewingModel, Rugged rugged) throws RuggedException
{
// generate reference mapping
String sensorName = viewingModel.getSensorName();
mapping = new SensorToGroundMapping(sensorName);
this.rugged = rugged;
this.viewingModel = viewingModel;
sensor = rugged.getLineSensor(mapping.getSensorName());
measureCount = 0;
}
public SensorToGroundMapping getMapping() {
return mapping;
}
public int getMeasureCount() {
return measureCount;
}
public void CreateMeasure(final int lineSampling,final int pixelSampling) throws RuggedException
{
for (double line = 0; line < viewingModel.dimension; line += lineSampling) {
AbsoluteDate date = sensor.getDate(line);
for (int pixel = 0; pixel < sensor.getNbPixels(); pixel += pixelSampling) {
GeodeticPoint gp2 = rugged.directLocation(date, sensor.getPosition(),
sensor.getLOS(date, pixel));
mapping.addMapping(new SensorPixel(line, pixel), gp2);
measureCount++;
}
}
}
}
src/tutorials/java/AffinagePleiades/OrbitModel.java deleted 100644 → 0
View file @ 4430eac3
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package AffinagePleiades;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.ode.nonstiff.DormandPrince853Integrator;
import org.hipparchus.util.FastMath;
import java.util.ArrayList;
import java.util.List;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.attitudes.NadirPointing;
import org.orekit.attitudes.YawCompensation;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.CelestialBodyFactory;
import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.errors.OrekitException;
import org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel;
import org.orekit.forces.gravity.ThirdBodyAttraction;
import org.orekit.forces.gravity.potential.GravityFieldFactory;
import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.frames.Transform;
import org.orekit.orbits.CircularOrbit;
import org.orekit.orbits.Orbit;
import org.orekit.orbits.OrbitType;
import org.orekit.orbits.PositionAngle;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.KeplerianPropagator;
import org.orekit.propagation.numerical.NumericalPropagator;
import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
import org.orekit.utils.Constants;
import org.orekit.utils.IERSConventions;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.TimeStampedAngularCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
/**
* Orbit Model class to generate PV and Q
* @author jguinet
*
*/
public class OrbitModel {
public static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz)
throws OrekitException {
AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
Vector3D position = new Vector3D(px, py, pz);
Vector3D velocity = new Vector3D(vx, vy, vz);
PVCoordinates pvITRF = new PVCoordinates(position, velocity);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
Vector3D pEME2000 = transform.transformPosition(pvITRF.getPosition());
Vector3D vEME2000 = transform.transformVector(pvITRF.getVelocity());
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pEME2000, vEME2000, Vector3D.ZERO));
}
public void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList,
String absDate, double q0, double q1, double q2, double q3) {
AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
Rotation rotation = new Rotation(q0, q1, q2, q3, true);
TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
}
public BodyShape createEarth()
throws OrekitException {
return new OneAxisEllipsoid(Constants.WGS84_EARTH_EQUATORIAL_RADIUS,
Constants.WGS84_EARTH_FLATTENING,
FramesFactory.getITRF(IERSConventions.IERS_2010, true));
}
public NormalizedSphericalHarmonicsProvider createGravityField()
throws OrekitException {
return GravityFieldFactory.getNormalizedProvider(12, 12);
}
public Orbit createOrbit(double mu,AbsoluteDate date)
throws OrekitException {
// the following orbital parameters have been computed using
// Orekit tutorial about phasing, using the following configuration:
//
// orbit.date = 2012-01-01T00:00:00.000
// phasing.orbits.number = 143
// phasing.days.number = 10
// sun.synchronous.reference.latitude = 0
// sun.synchronous.reference.ascending = false
// sun.synchronous.mean.solar.time = 10:30:00
// gravity.field.degree = 12
// gravity.field.order = 12
Frame eme2000 = FramesFactory.getEME2000();
//return new CircularOrbit(7173352.811913891,
return new CircularOrbit(694000.0 + Constants.WGS84_EARTH_EQUATORIAL_RADIUS,//ajouter Rayon
-4.029194321683225E-4, 0.0013530362644647786,
FastMath.toRadians(98.2), //pleiades inclinaison 98.2
//FastMath.toRadians(-86.47),
FastMath.toRadians(-86.47+180),
FastMath.toRadians(135.9+0.3), PositionAngle.TRUE,
eme2000, date, mu);
}
public Propagator createPropagator(BodyShape earth,
NormalizedSphericalHarmonicsProvider gravityField,
Orbit orbit)
throws OrekitException {
AttitudeProvider yawCompensation = new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth));
SpacecraftState state = new SpacecraftState(orbit,
yawCompensation.getAttitude(orbit,
orbit.getDate(),
orbit.getFrame()),
1180.0);
// numerical model for improving orbit
OrbitType type = OrbitType.CIRCULAR;
double[][] tolerances = NumericalPropagator.tolerances(0.1, orbit, type);
DormandPrince853Integrator integrator =
new DormandPrince853Integrator(1.0e-4 * orbit.getKeplerianPeriod(),
1.0e-1 * orbit.getKeplerianPeriod(),
tolerances[0], tolerances[1]);
integrator.setInitialStepSize(1.0e-2 * orbit.getKeplerianPeriod());
NumericalPropagator numericalPropagator = new NumericalPropagator(integrator);
numericalPropagator.addForceModel(new HolmesFeatherstoneAttractionModel(earth.getBodyFrame(), gravityField));
numericalPropagator.addForceModel(new ThirdBodyAttraction(CelestialBodyFactory.getSun()));
numericalPropagator.addForceModel(new ThirdBodyAttraction(CelestialBodyFactory.getMoon()));
numericalPropagator.setOrbitType(type);
numericalPropagator.setInitialState(state);
numericalPropagator.setAttitudeProvider(yawCompensation);
return numericalPropagator;
}
public List<TimeStampedPVCoordinates> orbitToPV(Orbit orbit, BodyShape earth,
AbsoluteDate minDate, AbsoluteDate maxDate,
double step)
throws OrekitException {
Propagator propagator = new KeplerianPropagator(orbit);
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
propagator.setMasterMode(step, new OrekitFixedStepHandler() {
public void init(SpacecraftState s0, AbsoluteDate t) {
}
public void handleStep(SpacecraftState currentState, boolean isLast) {
list.add(new TimeStampedPVCoordinates(currentState.getDate(),
currentState.getPVCoordinates().getPosition(),
currentState.getPVCoordinates().getVelocity(),
Vector3D.ZERO));
}
});
propagator.propagate(maxDate);
return list;
}
public List<TimeStampedAngularCoordinates> orbitToQ(Orbit orbit, BodyShape earth,
AbsoluteDate minDate, AbsoluteDate maxDate,
double step)
throws OrekitException {
Propagator propagator = new KeplerianPropagator(orbit);
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<TimeStampedAngularCoordinates>();
propagator.setMasterMode(step, new OrekitFixedStepHandler() {
public void init(SpacecraftState s0, AbsoluteDate t) {
}
public void handleStep(SpacecraftState currentState, boolean isLast) {
list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
currentState.getAttitude().getRotation(),
Vector3D.ZERO, Vector3D.ZERO));
}
});
propagator.propagate(maxDate);
return list;
}
}
src/tutorials/java/fr/cs/examples/AtmosphericRefractionExamples.java 0 → 100644
View file @ acf902ea
package fr.cs.examples;
import java.io.File;
import java.net.URISyntaxException;
import java.text.DecimalFormat;
import java.text.DecimalFormatSymbols;
import java.util.ArrayList;
import java.util.List;
import java.util.Locale;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.stat.descriptive.DescriptiveStatistics;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.frames.Transform;
import org.orekit.rugged.api.AlgorithmId;
import org.orekit.rugged.api.BodyRotatingFrameId;
import org.orekit.rugged.api.EllipsoidId;
import org.orekit.rugged.api.InertialFrameId;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.api.RuggedBuilder;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.LinearLineDatation;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.los.FixedRotation;
import org.orekit.rugged.los.LOSBuilder;
import org.orekit.rugged.los.TimeDependentLOS;
import org.orekit.rugged.refraction.AtmosphericRefraction;
import org.orekit.rugged.refraction.MultiLayerModel;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
import org.orekit.time.TimeScalesFactory;
import org.orekit.utils.AngularDerivativesFilter;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.IERSConventions;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.TimeStampedAngularCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
/** A simple example of how to use the atmospheric refraction correction.
*/
public class AtmosphericRefractionExamples {
public static void main(String[] args) throws URISyntaxException {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Sensor's definition
// ===================
// Line of sight
// -------------
// The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
List<Vector3D> rawDirs = new ArrayList<Vector3D>();
for (int i = 0; i < 2000; i++) {
// 20° field of view, 2000 pixels
rawDirs.add(new Vector3D(0., i*FastMath.toRadians(20.)/2000., 1.));
}
// The instrument is oriented 10° off nadir around the X-axis, we need to rotate the viewing
// direction to obtain the line of sight in the satellite frame
LOSBuilder losBuilder = new LOSBuilder(rawDirs);
losBuilder.addTransform(new FixedRotation("10-degrees-rotation", Vector3D.PLUS_I, FastMath.toRadians(10.)));
TimeDependentLOS lineOfSight = losBuilder.build();
// Datation model
// --------------
// We use Orekit for handling time and dates, and Rugged for defining the datation model:
TimeScale gps = TimeScalesFactory.getGPS();
AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1., 20.);
// Line sensor
// -----------
// With the LOS and the datation now define, we can initialize a line sensor object in Rugged:
LineSensor lineSensor = new LineSensor("mySensor", lineDatation, Vector3D.ZERO, lineOfSight);
// Satellite position, velocity and attitude
// =========================================
// Reference frames
// ----------------
// In our application, we simply need to know the name of the frames we are working with. Positions and
// velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
// inertial frame.
Frame eme2000 = FramesFactory.getEME2000();
boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
// Satellite attitude
// ------------------
ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236, 0.333952, -0.844012, -0.245684);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773, 0.329336, -0.837871, -0.252281);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:30.592937", -0.369237, 0.324612, -0.831445, -0.258824);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:54.592937", -0.3836, 0.319792, -0.824743, -0.265299);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:18.592937", -0.397834, 0.314883, -0.817777, -0.271695);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:42.592937", -0.411912, 0.309895, -0.810561, -0.278001);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:06.592937", -0.42581, 0.304838, -0.803111, -0.284206);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:30.592937", -0.439505, 0.299722, -0.795442, -0.290301);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976, 0.294556, -0.787571, -0.296279);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207, 0.28935, -0.779516, -0.302131);
// Positions and velocities
// ------------------------
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466, -5411878.485, 4637549.599, -2463.635, -4447.634, -5576.736);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267, -5506500.533, 4515934.894, -2459.848, -4312.676, -5683.906);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368, -5598184.195, 4392036.13, -2454.395, -4175.564, -5788.201);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:47.392937", -885556.748, -5686883.696, 4265915.971, -2447.273, -4036.368, -5889.568);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:08.992937", -938326.32, -5772554.875, 4137638.207, -2438.478, -3895.166, -5987.957);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:30.592937", -990887.942, -5855155.21, 4007267.717, -2428.011, -3752.034, -6083.317);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:52.192937", -1043205.448, -5934643.836, 3874870.441, -2415.868, -3607.05, -6175.600);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:13.792937", -1095242.669, -6010981.571, 3740513.34, -2402.051, -3460.291, -6264.760);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:35.392937", -1146963.457, -6084130.93, 3604264.372, -2386.561, -3311.835, -6350.751);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706, -6154056.146, 3466192.446, -2369.401, -3161.764, -6433.531);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381, -6220723.191, 3326367.397, -2350.574, -3010.159, -6513.056);
// Rugged initialization
// ---------------------
RuggedBuilder builder = new RuggedBuilder().
setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID).
setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5. / lineSensor.getRate(0.)).
setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor);
// Build Rugged without atmospheric refraction model
Rugged ruggedWithout = builder.build();
// Defines atmospheric refraction model (with the default multi layers model)
AtmosphericRefraction atmosphericRefraction = new MultiLayerModel(ruggedWithout.getEllipsoid());
// One can use its own atmospheric model that must extend the abstract refraction.AtmosphericRefraction class.
// Set the optional grid steps, for the inverse location computation. Useless for direct location computation.
// This setting is optional as default values exist. But can be useful for instance to improve results by given smaller steps
// or to speed up the computation bigger steps.
int pixelStep = 100;
int lineStep = 100;
atmosphericRefraction.setGridSteps(pixelStep, lineStep);
// To compute the inverse location grid with atmospheric refraction, a default margin is available:
// atmosphericRefraction.getComputationParameters().getDefaultInverseLocMargin();
// but can be modified with:
// atmosphericRefraction.setInverseLocMargin(margin);
// Build Rugged with atmospheric refraction model
builder.setRefractionCorrection(atmosphericRefraction);
Rugged ruggedWith = builder.build();
// Direct location on a line WITHOUT and WITH atmospheric correction
// -----------------------------------------------------------------
double chosenLine = 200.;
// Without atmosphere
GeodeticPoint[] gpWithoutAtmosphericRefractionCorrection = ruggedWithout.directLocation("mySensor", chosenLine);
// With atmosphere
GeodeticPoint[] gpWithAtmosphericRefractionCorrection = ruggedWith.directLocation("mySensor", chosenLine);
double earthRadius = ruggedWithout.getEllipsoid().getEquatorialRadius();
DescriptiveStatistics statDistance = new DescriptiveStatistics();
for (int i = 0; i < gpWithAtmosphericRefractionCorrection.length; i++) {
double currentRadius = earthRadius + (gpWithAtmosphericRefractionCorrection[i].getAltitude()+ gpWithoutAtmosphericRefractionCorrection[i].getAltitude())/2.;
double distance = computeDistanceInMeter(currentRadius, gpWithAtmosphericRefractionCorrection[i], gpWithoutAtmosphericRefractionCorrection[i]);
statDistance.addValue(distance);
}
System.out.format("Distance must be > 0 and < 2m:" +
" Max = " + DFS.format(statDistance.getMax()) +
" Min = " + DFS.format(statDistance.getMin()) +
" Median = " + DFS.format(statDistance.getPercentile(50.)) +
" Mean = " + DFS.format(statDistance.getMean()) +
" Std deviation= " + DFS.format(statDistance.getStandardDeviation()) +
"\n");
// Inverse loc WITH atmospheric correction
// ==========================================================================
final double epsilonPixel = 1.e-3;
final double epsilonLine = 1.1e-2;
int minLine = (int) FastMath.floor(lineSensor.getLine(ruggedWithout.getMinDate()));
int maxLine = (int) FastMath.ceil(lineSensor.getLine(ruggedWithout.getMaxDate()));
for (int i = 0; i < gpWithAtmosphericRefractionCorrection.length; i++) {
// to check if we go back to the initial point when taking the geodetic point with atmospheric correction
GeodeticPoint gpWith = gpWithAtmosphericRefractionCorrection[i];
SensorPixel sensorPixelReverseWith = ruggedWith.inverseLocation("mySensor", gpWith, minLine, maxLine);
if (sensorPixelReverseWith != null) {
// Compare the computed pixel vs expected
if (FastMath.abs(i - sensorPixelReverseWith.getPixelNumber()) > epsilonPixel) {
System.out.format("Problem with pixel " + i + " . Delta pixel= " + DFS.format((i - sensorPixelReverseWith.getPixelNumber())) + "\n");
}
// Compare the computed line vs the expected
if (FastMath.abs(chosenLine - sensorPixelReverseWith.getLineNumber())> epsilonLine) {
System.out.format("Probem with line, for pixel " + i + ". Delta line= " + DFS.format((chosenLine - sensorPixelReverseWith.getLineNumber())) + "\n");
}
} else {
System.out.println("Inverse location failed for pixel " + i + " with atmospheric refraction correction for geodetic point computed with" );
}
} // end loop on pixel i
System.out.format("Inverse location gave same pixel and line as direct location input for" +
" epsilon pixel= " + DFS.format(epsilonPixel) +
" and epsilon line= " + DFS.format(epsilonLine) +
"\n");
}
private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz) {
AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
Vector3D position = new Vector3D(px, py, pz); // in ITRF, unit: m
Vector3D velocity = new Vector3D(vx, vy, vz); // in ITRF, unit: m/s
PVCoordinates pvITRF = new PVCoordinates(position, velocity);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pvEME2000.getPosition(), pvEME2000.getVelocity(), Vector3D.ZERO));
}
private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
double q0, double q1, double q2, double q3) {
AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
Rotation rotation = new Rotation(q0, q1, q2, q3, true); // q0 is the scalar term
TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
}
private static double computeDistanceInMeter(double earthRadius, final GeodeticPoint gp1, final GeodeticPoint gp2) {
// get vectors on unit sphere from angular coordinates
final Vector3D p1 = new Vector3D(gp1.getLongitude(), gp1.getLatitude());
final Vector3D p2 = new Vector3D(gp2.getLongitude(), gp2.getLatitude());
return earthRadius * Vector3D.angle(p1, p2);
}
/** Definition of print format. */
private static final DecimalFormatSymbols SYMBOLS = new DecimalFormatSymbols(Locale.US);
/** Defined of number of digit after the point. */
private static final DecimalFormat DFS = new DecimalFormat("#.#####", SYMBOLS);
}
src/tutorials/java/fr/cs/examples/DirectLocation.java
View file @ acf902ea
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
......@@ -16,16 +16,16 @@
*/
package fr.cs.examples;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import java.io.File;
import java.util.ArrayList;
import java.util.List;
import java.util.Locale;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataProvidersManager;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.frames.Frame;
......@@ -40,8 +40,8 @@ import org.orekit.rugged.api.RuggedBuilder;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.LinearLineDatation;
import org.orekit.rugged.los.LOSBuilder;
import org.orekit.rugged.los.FixedRotation;
import org.orekit.rugged.los.LOSBuilder;
import org.orekit.rugged.los.TimeDependentLOS;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
......@@ -62,12 +62,16 @@ public class DirectLocation {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Sensor's definition
// ===================
// Line of sight
// -------------
// The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
List<Vector3D> rawDirs = new ArrayList<Vector3D>();
for (int i = 0; i < 2000; i++) {
//20° field of view, 2000 pixels
// 20° field of view, 2000 pixels
rawDirs.add(new Vector3D(0d, i*FastMath.toRadians(20)/2000d, 1d));
}
......@@ -78,23 +82,33 @@ public class DirectLocation {
TimeDependentLOS lineOfSight = losBuilder.build();
// Datation model
// --------------
// We use Orekit for handling time and dates, and Rugged for defining the datation model:
TimeScale gps = TimeScalesFactory.getGPS();
AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
// With the LOS and the datation now defined , we can initialize a line sensor object in Rugged:
// Line sensor
// -----------
// With the LOS and the datation now defined, we can initialize a line sensor object in Rugged:
LineSensor lineSensor = new LineSensor("mySensor", lineDatation, Vector3D.ZERO, lineOfSight);
// Satellite position, velocity and attitude
// =========================================
// Reference frames
// ----------------
// In our application, we simply need to know the name of the frames we are working with. Positions and
// velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
// inertial frame.
// inertial frame.
Frame eme2000 = FramesFactory.getEME2000();
boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
// Satellite attitude
// ------------------
ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236d, 0.333952d, -0.844012d, -0.245684d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773d, 0.329336d, -0.837871d, -0.252281d);
......@@ -107,6 +121,10 @@ public class DirectLocation {
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976d, 0.294556d, -0.787571d, -0.296279d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207d, 0.28935d, -0.779516d, -0.302131d);
// Positions and velocities
// ------------------------
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466d, -5411878.485d, 4637549.599d, -2463.635d, -4447.634d, -5576.736d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267d, -5506500.533d, 4515934.894d, -2459.848d, -4312.676d, -5683.906d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368d, -5598184.195d, 4392036.13d, -2454.395d, -4175.564d, -5788.201d);
......@@ -119,16 +137,20 @@ public class DirectLocation {
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706d, -6154056.146d, 3466192.446d, -2369.401d, -3161.764d, -6433.531d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381d, -6220723.191d, 3326367.397d, -2350.574d, -3010.159d, -6513.056d);
// Rugged initialization
// ---------------------
Rugged rugged = new RuggedBuilder().
setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID).
setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID).
setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor).
build();
// Direct location of a single sensor pixel (first line, first pixel)
// ------------------------------------------------------------------
Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
AbsoluteDate firstLineDate = lineSensor.getDate(0);
Vector3D los = lineSensor.getLOS(firstLineDate, 0);
......@@ -151,21 +173,21 @@ public class DirectLocation {
private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz)
throws OrekitException {
double px, double py, double pz, double vx, double vy, double vz) {
AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
Vector3D position = new Vector3D(px, py, pz);
Vector3D velocity = new Vector3D(vx, vy, vz);
Vector3D position = new Vector3D(px, py, pz); // in ITRF, unit: m
Vector3D velocity = new Vector3D(vx, vy, vz); // in ITRF, unit: m/s
PVCoordinates pvITRF = new PVCoordinates(position, velocity);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pvEME2000.getPosition(), pvEME2000.getVelocity(), Vector3D.ZERO));
}
private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
double q0, double q1, double q2, double q3) {
AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
Rotation rotation = new Rotation(q0, q1, q2, q3, true);
Rotation rotation = new Rotation(q0, q1, q2, q3, true); // q0 is the scalar term
TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
......
src/tutorials/java/fr/cs/examples/DirectLocationWithDEM.java
View file @ acf902ea
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
......@@ -25,7 +25,7 @@ import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataProvidersManager;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.frames.Frame;
......@@ -65,12 +65,16 @@ public class DirectLocationWithDEM {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Sensor's definition
// ===================
// Line of sight
// -------------
// The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
List<Vector3D> rawDirs = new ArrayList<Vector3D>();
for (int i = 0; i < 2000; i++) {
//20° field of view, 2000 pixels
// 20° field of view, 2000 pixels
rawDirs.add(new Vector3D(0d, i*FastMath.toRadians(20)/2000d, 1d));
}
......@@ -81,23 +85,33 @@ public class DirectLocationWithDEM {
TimeDependentLOS lineOfSight = losBuilder.build();
// Datation model
// --------------
// We use Orekit for handling time and dates, and Rugged for defining the datation model:
TimeScale gps = TimeScalesFactory.getGPS();
AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
// With the LOS and the datation now defined , we can initialize a line sensor object in Rugged:
// Line sensor
// -----------
// With the LOS and the datation now defined, we can initialize a line sensor object in Rugged:
LineSensor lineSensor = new LineSensor("mySensor", lineDatation, Vector3D.ZERO, lineOfSight);
// Satellite position, velocity and attitude
// =========================================
// Reference frames
// ----------------
// In our application, we simply need to know the name of the frames we are working with. Positions and
// velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
// inertial frame.
// inertial frame.
Frame eme2000 = FramesFactory.getEME2000();
boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
// Satellite attitude
// ------------------
ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236d, 0.333952d, -0.844012d, -0.245684d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773d, 0.329336d, -0.837871d, -0.252281d);
......@@ -109,7 +123,10 @@ public class DirectLocationWithDEM {
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:30.592937", -0.439505d, 0.299722d, -0.795442d, -0.290301d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976d, 0.294556d, -0.787571d, -0.296279d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207d, 0.28935d, -0.779516d, -0.302131d);
// Positions and velocities
// ------------------------
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466d, -5411878.485d, 4637549.599d, -2463.635d, -4447.634d, -5576.736d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267d, -5506500.533d, 4515934.894d, -2459.848d, -4312.676d, -5683.906d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368d, -5598184.195d, 4392036.13d, -2454.395d, -4175.564d, -5788.201d);
......@@ -122,23 +139,27 @@ public class DirectLocationWithDEM {
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706d, -6154056.146d, 3466192.446d, -2369.401d, -3161.764d, -6433.531d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381d, -6220723.191d, 3326367.397d, -2350.574d, -3010.159d, -6513.056d);
// Rugged initialization
// ---------------------
Rugged rugged = new RuggedBuilder().
setAlgorithm(AlgorithmId.DUVENHAGE).
setDigitalElevationModel(new VolcanicConeElevationUpdater(new GeodeticPoint(FastMath.toRadians(37.58),
FastMath.toRadians(-96.95),
2463.0),
FastMath.toRadians(30.0), 16.0,
FastMath.toRadians(1.0), 1201),
8).
setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor).
build();
setAlgorithm(AlgorithmId.DUVENHAGE).
setDigitalElevationModel(new VolcanicConeElevationUpdater(new GeodeticPoint(FastMath.toRadians(37.58),
FastMath.toRadians(-96.95),
2463.0),
FastMath.toRadians(30.0), 16.0,
FastMath.toRadians(1.0), 1201),
8).
setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor).
build();
// Direct location of a single sensor pixel (first line, first pixel)
// ------------------------------------------------------------------
Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
AbsoluteDate firstLineDate = lineSensor.getDate(0);
Vector3D los = lineSensor.getLOS(firstLineDate, 0);
......@@ -159,16 +180,16 @@ public class DirectLocationWithDEM {
}
private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz)
throws OrekitException {
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz) {
AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
Vector3D position = new Vector3D(px, py, pz);
Vector3D velocity = new Vector3D(vx, vy, vz);
Vector3D position = new Vector3D(px, py, pz); // in ITRF, unit: m
Vector3D velocity = new Vector3D(vx, vy, vz); // in ITRF, unit: m/s
PVCoordinates pvITRF = new PVCoordinates(position, velocity);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pvEME2000.getPosition(), pvEME2000.getVelocity(), Vector3D.ZERO));
}
......@@ -176,9 +197,9 @@ public class DirectLocationWithDEM {
private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
double q0, double q1, double q2, double q3) {
AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
Rotation rotation = new Rotation(q0, q1, q2, q3, true);
Rotation rotation = new Rotation(q0, q1, q2, q3, true); // q0 is the scalar term
TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
}
......@@ -199,8 +220,9 @@ public class DirectLocationWithDEM {
this.n = n;
}
public void updateTile(double latitude, double longitude, UpdatableTile tile)
throws RuggedException {
@Override
public void updateTile(double latitude, double longitude, UpdatableTile tile) {
double step = size / (n - 1);
double minLatitude = size * FastMath.floor(latitude / size);
double minLongitude = size * FastMath.floor(longitude / size);
......@@ -211,8 +233,8 @@ public class DirectLocationWithDEM {
for (int j = 0; j < n; ++j) {
double cellLongitude = minLongitude + j * step;
double distance = Constants.WGS84_EARTH_EQUATORIAL_RADIUS *
FastMath.hypot(cellLatitude - summit.getLatitude(),
cellLongitude - summit.getLongitude());
FastMath.hypot(cellLatitude - summit.getLatitude(),
cellLongitude - summit.getLongitude());
double altitude = FastMath.max(summit.getAltitude() - distance * sinSlope,
base);
tile.setElevation(i, j, altitude);
......
src/tutorials/java/fr/cs/examples/InverseLocation.java
View file @ acf902ea
/* Copyright 2013-2016 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
......@@ -25,7 +25,8 @@ import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataProvidersManager;
import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.frames.Frame;
......@@ -44,6 +45,7 @@ import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.los.FixedRotation;
import org.orekit.rugged.los.LOSBuilder;
import org.orekit.rugged.los.TimeDependentLOS;
import org.orekit.rugged.utils.RoughVisibilityEstimator;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
import org.orekit.time.TimeScalesFactory;
......@@ -63,12 +65,16 @@ public class InverseLocation {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Sensor's definition
// ===================
// Line of sight
// -------------
// The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
List<Vector3D> rawDirs = new ArrayList<Vector3D>();
for (int i = 0; i < 2000; i++) {
//20° field of view, 2000 pixels
// 20° field of view, 2000 pixels
rawDirs.add(new Vector3D(0d, i*FastMath.toRadians(20)/2000d, 1d));
}
......@@ -79,26 +85,34 @@ public class InverseLocation {
TimeDependentLOS lineOfSight = losBuilder.build();
// Datation model
// --------------
// We use Orekit for handling time and dates, and Rugged for defining the datation model:
TimeScale gps = TimeScalesFactory.getGPS();
AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
// Line sensor
// -----------
// With the LOS and the datation now defined , we can initialize a line sensor object in Rugged:
String sensorName = "mySensor";
LineSensor lineSensor = new LineSensor(sensorName, lineDatation, Vector3D.ZERO, lineOfSight);
// Satellite position, velocity and attitude
// =========================================
// Reference frames
// ----------------
// In our application, we simply need to know the name of the frames we are working with. Positions and
// velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
// inertial frame.
// inertial frame.
Frame eme2000 = FramesFactory.getEME2000();
boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
// Satellite attitude
// ------------------
ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236d, 0.333952d, -0.844012d, -0.245684d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773d, 0.329336d, -0.837871d, -0.252281d);
......@@ -111,6 +125,10 @@ public class InverseLocation {
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976d, 0.294556d, -0.787571d, -0.296279d);
addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207d, 0.28935d, -0.779516d, -0.302131d);
// Positions and velocities
// ------------------------
ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466d, -5411878.485d, 4637549.599d, -2463.635d, -4447.634d, -5576.736d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267d, -5506500.533d, 4515934.894d, -2459.848d, -4312.676d, -5683.906d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368d, -5598184.195d, 4392036.13d, -2454.395d, -4175.564d, -5788.201d);
......@@ -123,37 +141,77 @@ public class InverseLocation {
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706d, -6154056.146d, 3466192.446d, -2369.401d, -3161.764d, -6433.531d);
addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381d, -6220723.191d, 3326367.397d, -2350.574d, -3010.159d, -6513.056d);
Rugged rugged = new RuggedBuilder().
setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID).
setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor).
build();
// Rugged initialization
// ---------------------
RuggedBuilder ruggedBuilder = new RuggedBuilder();
ruggedBuilder.setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID);
ruggedBuilder.setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF);
ruggedBuilder.setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0));
ruggedBuilder.setTrajectory(InertialFrameId.EME2000,
satellitePVList, 4, CartesianDerivativesFilter.USE_P,
satelliteQList, 4, AngularDerivativesFilter.USE_R).
addLineSensor(lineSensor);
Rugged rugged = ruggedBuilder.build();
// Inverse location of a Geodetic Point
// ------------------------------------
// Point defined by its latitude, longitude and altitude
double latitude = FastMath.toRadians(37.585);
double longitude = FastMath.toRadians(-96.949);
double altitude = 0.0d;
// For a GeodeticPoint : angles are given in radians and altitude in meters
GeodeticPoint gp = new GeodeticPoint(latitude, longitude, altitude);
// Search the sensor pixel seeing point
// ....................................
// interval of lines where to search the point
int minLine = 0;
int maxLine = 100;
SensorPixel sensorPixel = rugged.inverseLocation(sensorName, gp, minLine, maxLine);
// we need to test if the sensor pixel is found in the prescribed lines otherwise the sensor pixel is null
// Be careful: no exception is thrown if the pixel is not found
if (sensorPixel != null){
// The pixel was found
System.out.format(Locale.US, "Sensor Pixel found : line = %5.3f, pixel = %5.3f %n", sensorPixel.getLineNumber(), sensorPixel.getPixelNumber());
} else {
// The pixel was not found: set to null
System.out.println("Sensor Pixel is null: point cannot be seen between the prescribed line numbers\n");
}
// Find the date at which the sensor sees the ground point
// .......................................................
AbsoluteDate dateLine = rugged.dateLocation(sensorName, gp, minLine, maxLine);
System.out.println("Date at which the sensor sees the ground point : " + dateLine);
// How to find min and max lines ? with the RoughVisibilityEstimator
// -------------------------------
// Create a RoughVisibilityEstimator for inverse location
OneAxisEllipsoid oneAxisEllipsoid = ruggedBuilder.getEllipsoid();
Frame pvFrame = ruggedBuilder.getInertialFrame();
// Initialize the RoughVisibilityEstimator
RoughVisibilityEstimator roughVisibilityEstimator = new RoughVisibilityEstimator(oneAxisEllipsoid, pvFrame, satellitePVList);
// Compute the approximated line with a rough estimator
AbsoluteDate roughLineDate = roughVisibilityEstimator.estimateVisibility(gp);
double roughLine = lineSensor.getLine(roughLineDate);
// Compute the min / max lines interval using a margin around the roughLine
int sensorMinLine= 0;
int sensorMaxLine = 1000;
int margin = 100;
int minLineRough = (int) FastMath.max(roughLine - margin, sensorMinLine);
int maxLineRough = (int) FastMath.min(roughLine + margin, sensorMaxLine);
SensorPixel sensorPixelRoughLine = rugged.inverseLocation(sensorName, gp, minLineRough, maxLineRough);
System.out.format(Locale.US, "Rough line found = %5.1f; InverseLocation gives (margin of %d around rough line): line = %5.3f, pixel = %5.3f %n", roughLine, margin, sensorPixelRoughLine.getLineNumber(), sensorPixel.getPixelNumber());
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
......@@ -165,25 +223,25 @@ public class InverseLocation {
}
private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz)
throws OrekitException {
ArrayList<TimeStampedPVCoordinates> satellitePVList,
String absDate,
double px, double py, double pz, double vx, double vy, double vz) {
AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
Vector3D position = new Vector3D(px, py, pz);
Vector3D velocity = new Vector3D(vx, vy, vz);
Vector3D position = new Vector3D(px, py, pz); // in ITRF, unit: m
Vector3D velocity = new Vector3D(vx, vy, vz); // in ITRF, unit: m/s
PVCoordinates pvITRF = new PVCoordinates(position, velocity);
Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
PVCoordinates pvEME2000 = transform.transformPVCoordinates(pvITRF);
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pvEME2000.getPosition(), pvEME2000.getVelocity(), Vector3D.ZERO));
}
private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
double q0, double q1, double q2, double q3) {
AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
Rotation rotation = new Rotation(q0, q1, q2, q3, true);
Rotation rotation = new Rotation(q0, q1, q2, q3, true); // q0 is the scalar term
TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
}
......
src/tutorials/java/fr/cs/examples/refiningPleiades/GroundRefining.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades;
import java.io.File;
import java.util.List;
import java.util.Locale;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
import org.orekit.orbits.Orbit;
import org.orekit.rugged.adjustment.measurements.SensorToGroundMapping;
import org.orekit.rugged.api.AlgorithmId;
import org.orekit.rugged.api.BodyRotatingFrameId;
import org.orekit.rugged.api.EllipsoidId;
import org.orekit.rugged.api.InertialFrameId;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.api.RuggedBuilder;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.AngularDerivativesFilter;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.TimeStampedAngularCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
import fr.cs.examples.refiningPleiades.generators.GroundMeasurementGenerator;
import fr.cs.examples.refiningPleiades.generators.Noise;
import fr.cs.examples.refiningPleiades.metrics.DistanceTools;
import fr.cs.examples.refiningPleiades.models.OrbitModel;
import fr.cs.examples.refiningPleiades.models.PleiadesViewingModel;
/**
* Class for testing refining (Ground Control Points GCP study)
* with or without noisy measurements
* @author Jonathan Guinet
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @see SensorToGroundMapping
* @see GroundMeasurementGenerator
* @since 2.0
*/
public class GroundRefining extends Refining {
/** Pleiades viewing model */
private static PleiadesViewingModel pleiadesViewingModel;
/** Sensor name */
private static String sensorName;
/** Main function
*/
public static void main(String[] args) {
try {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
// ---------------------------------------------------------------------------
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Initialize refining context
// ---------------------------
GroundRefining refining = new GroundRefining();
// Sensor's definition: create Pleiades viewing model
// --------------------------------------------------
System.out.format("**** Build Pleiades viewing model and orbit definition **** %n");
AbsoluteDate minDate = pleiadesViewingModel.getMinDate();
AbsoluteDate maxDate = pleiadesViewingModel.getMaxDate();
AbsoluteDate refDate = pleiadesViewingModel.getDatationReference();
LineSensor lineSensor = pleiadesViewingModel.getLineSensor();
// Satellite position, velocity and attitude: create an orbit model
// ----------------------------------------------------------------
OrbitModel orbitmodel = new OrbitModel();
BodyShape earth = orbitmodel.createEarth();
NormalizedSphericalHarmonicsProvider gravityField = orbitmodel.createGravityField();
Orbit orbit = orbitmodel.createOrbit(gravityField.getMu(), refDate);
// Nadir's pointing
final double [] rollPoly = {0.0,0.0,0.0};
double[] pitchPoly = {0.0,0.0};
double[] yawPoly = {0.0,0.0,0.0};
orbitmodel.setLOFTransform(rollPoly, pitchPoly, yawPoly, minDate);
// Satellite attitude
List<TimeStampedAngularCoordinates> satelliteQList =
orbitmodel.orbitToQ(orbit, earth, minDate.shiftedBy(-0.0), maxDate.shiftedBy(+0.0), 0.25);
int nbQPoints = 2;
// Position and velocities
PVCoordinates PV = orbit.getPVCoordinates(earth.getBodyFrame());
List<TimeStampedPVCoordinates> satellitePVList =
orbitmodel.orbitToPV(orbit, earth, minDate.shiftedBy(-0.0), maxDate.shiftedBy(+0.0), 0.25);
int nbPVPoints = 8;
// Convert frame and coordinates type in one call
GeodeticPoint gp = earth.transform(PV.getPosition(), earth.getBodyFrame(), orbit.getDate());
System.out.format(Locale.US, "Geodetic Point at date %s : φ = %8.10f °, λ = %8.10f %n",
orbit.getDate().toString(),
FastMath.toDegrees(gp.getLatitude()),
FastMath.toDegrees(gp.getLongitude()));
// Rugged initialization
// ---------------------
System.out.format("\n**** Rugged initialization **** %n");
RuggedBuilder ruggedBuilder = new RuggedBuilder();
ruggedBuilder.addLineSensor(lineSensor);
ruggedBuilder.setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID);
ruggedBuilder.setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF);
ruggedBuilder.setTimeSpan(minDate,maxDate, 0.001, 5.0);
ruggedBuilder.setTrajectory(InertialFrameId.EME2000, satellitePVList,nbPVPoints,
CartesianDerivativesFilter.USE_PV, satelliteQList,
nbQPoints, AngularDerivativesFilter.USE_R);
ruggedBuilder.setName("Rugged_refining");
Rugged rugged = ruggedBuilder.build();
// Compute ground sample distance (GSD)
// ------------------------------------
double [] gsd = refining.computeGSD(rugged, lineSensor);
System.out.format("GSD - X: %2.2f Y: %2.2f **** %n", gsd[0], gsd[1]);
// Initialize disruptions:
// -----------------------
// Introduce rotations around instrument axes (roll and pitch translations, scale factor)
System.out.format("\n**** Add disruptions: roll and pitch rotations, scale factor **** %n");
double rollValue = FastMath.toRadians(-0.01);
double pitchValue = FastMath.toRadians(0.02);
double factorValue = 1.05;
System.out.format("roll: %3.5f \tpitch: %3.5f \tfactor: %3.5f \n",rollValue, pitchValue, factorValue);
// Apply disruptions on physical model
refining.applyDisruptions(rugged, sensorName, rollValue, pitchValue, factorValue);
// Generate measurements (observations) from physical model disrupted
// ------------------------------------------------------------------
int lineSampling = 1000;
int pixelSampling = 1000;
// Noise definition
// distribution: gaussian(0), vector dimension:3
final Noise noise = new Noise(0,3);
// lat mean, long mean, alt mean
final double[] mean = {0.0,0.0,0.0};
// lat std, long std, alt std}
final double[] standardDeviation = {0.0,0.0,0.0};
noise.setMean(mean);
noise.setStandardDeviation(standardDeviation);
// Ground measurements
GroundMeasurementGenerator measurements = refining.generateNoisyPoints(lineSampling, pixelSampling,
rugged, sensorName,
pleiadesViewingModel.getDimension(),
noise);
// Compute ground truth residuals
// ------------------------------
System.out.format("\n**** Ground truth residuals **** %n");
refining.computeMetrics(measurements.getGroundMapping(), rugged, false);
// Initialize physical model without disruptions
// ---------------------------------------------
System.out.format("\n**** Initialize physical model without disruptions: reset Roll/Pitch/Factor **** %n");
refining.resetModel(rugged, sensorName, true);
// Compute initial residuals
// -------------------------
System.out.format("\n**** Initial Residuals **** %n");
refining.computeMetrics(measurements.getGroundMapping(), rugged, false);
// Start optimization
// ------------------
System.out.format("\n**** Start optimization **** %n");
int maxIterations = 100;
double convergenceThreshold = 1.e-11;
refining.optimization(maxIterations, convergenceThreshold, measurements.getObservables(), rugged);
// Check estimated values
// ----------------------
System.out.format("\n**** Check parameters ajustement **** %n");
refining.paramsEstimation(rugged, sensorName, rollValue, pitchValue, factorValue);
// Compute statistics
// ------------------
System.out.format("\n**** Compute Statistics **** %n");
// Residuals computed in meters
refining.computeMetrics(measurements.getGroundMapping(), rugged, false);
// Residuals computed in degrees
refining.computeMetrics(measurements.getGroundMapping(), rugged, true);
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
} catch (RuggedException re) {
System.err.println(re.getLocalizedMessage());
System.exit(1);
}
}
/** Constructor */
private GroundRefining() {
sensorName = "line";
pleiadesViewingModel = new PleiadesViewingModel(sensorName);
}
/** Estimate ground sample distance (GSD)
* @param LineSensor line sensor
* @return the GSD
*/
private double[] computeGSD(final Rugged rugged, final LineSensor lineSensor) {
// Get number of line
int dimension = pleiadesViewingModel.getDimension();
// Get position
Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
// Get upper left geodetic point
AbsoluteDate firstLineDate = lineSensor.getDate(0);
Vector3D los = lineSensor.getLOS(firstLineDate,0);
GeodeticPoint upLeftPoint = rugged.directLocation(firstLineDate, position, los);
los = lineSensor.getLOS(firstLineDate,dimension-1);
// Get center geodetic point
AbsoluteDate lineDate = lineSensor.getDate(dimension/2);
los = lineSensor.getLOS(lineDate,dimension/2);
// Get upper right geodetic point
int pixelPosition = dimension-1;
los = lineSensor.getLOS(firstLineDate,pixelPosition);
GeodeticPoint upperRight = rugged.directLocation(firstLineDate, position, los);
// Get lower left geodetic point
AbsoluteDate lineDate_y = lineSensor.getDate(dimension-1);
los = lineSensor.getLOS(lineDate_y,0);
GeodeticPoint lowerLeft = rugged.directLocation(lineDate_y, position, los);
double gsdX = DistanceTools.computeDistanceInMeter(upLeftPoint, upperRight)/dimension;
double gsdY = DistanceTools.computeDistanceInMeter(upLeftPoint, lowerLeft)/dimension;
double [] gsd = {gsdX, gsdY};
return gsd;
}
// /**
// * Get the Pleiades viewing model
// * @return the Pleiades viewing model
// */
// public PleiadesViewingModel getPleiadesViewingModel() {
// return pleiadesViewingModel;
// }
//
// /**
// * Set the Pleiades viewing model
// * @param pleiadesViewingModel Pleiades viewing model to set
// */
// public void setPleiadesViewingModel(final PleiadesViewingModel pleiadesViewingModel) {
// this.pleiadesViewingModel = pleiadesViewingModel;
// }
//
// /**
// * Get the orbit model
// * @return the orbit model
// */
// public OrbitModel getOrbitmodel() {
// return orbitmodel;
// }
//
// /**
// * Set the orbit model
// * @param orbitmodel the orbit model to set
// */
// public void setOrbitmodel(final OrbitModel orbitmodel) {
// this.orbitmodel = orbitmodel;
// }
//
// /**
// * Get the sensor name
// * @return the sensor name
// */
// public String getSensorName() {
// return sensorName;
// }
//
// /**
// * Get the Rugged instance
// * @return the rugged instance
// */
// public Rugged getRugged() {
// return rugged;
// }
//
// /**
// * Set the Rugged instance
// * @param rugged the Rugged instance to set
// */
// public void setRugged(final Rugged rugged) {
// this.rugged = rugged;
// }
}
src/tutorials/java/fr/cs/examples/refiningPleiades/InterRefining.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades;
import java.io.File;
import java.util.Arrays;
import java.util.List;
import java.util.Locale;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.data.DataContext;
import org.orekit.data.DirectoryCrawler;
import org.orekit.errors.OrekitException;
import org.orekit.orbits.Orbit;
import org.orekit.rugged.adjustment.measurements.SensorToGroundMapping;
import org.orekit.rugged.api.AlgorithmId;
import org.orekit.rugged.api.BodyRotatingFrameId;
import org.orekit.rugged.api.EllipsoidId;
import org.orekit.rugged.api.InertialFrameId;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.api.RuggedBuilder;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.AngularDerivativesFilter;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.Constants;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.TimeStampedAngularCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
import fr.cs.examples.refiningPleiades.generators.GroundMeasurementGenerator;
import fr.cs.examples.refiningPleiades.generators.InterMeasurementGenerator;
import fr.cs.examples.refiningPleiades.generators.Noise;
import fr.cs.examples.refiningPleiades.metrics.DistanceTools;
import fr.cs.examples.refiningPleiades.models.OrbitModel;
import fr.cs.examples.refiningPleiades.models.PleiadesViewingModel;
/**
* Class for testing refining (tie points study)
* with or without noisy measurements
* @author Jonathan Guinet
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @see SensorToGroundMapping
* @see GroundMeasurementGenerator
* @since 2.0
*/
public class InterRefining extends Refining {
/** Pleiades viewing model A */
private static PleiadesViewingModel pleiadesViewingModelA;
/** Pleiades viewing model B */
private static PleiadesViewingModel pleiadesViewingModelB;
/** Sensor name A corresponding to viewing model A */
private static String sensorNameA;
/** Sensor name A corresponding to viewing model B */
private static String sensorNameB;
/** Main function
*/
public static void main(String[] args) {
try {
// Initialize Orekit, assuming an orekit-data folder is in user home directory
// ---------------------------------------------------------------------------
File home = new File(System.getProperty("user.home"));
File orekitData = new File(home, "orekit-data");
DataContext.getDefault().getDataProvidersManager().addProvider(new DirectoryCrawler(orekitData));
// Initialize refining context
// ---------------------------
InterRefining refining = new InterRefining();
// Sensors's definition: creation of 2 Pleiades viewing models
// -----------------------------------------------------------
System.out.format("**** Build Pleiades viewing model A and its orbit definition **** %n");
// 1/- Create First Pleiades Viewing Model
final AbsoluteDate minDateA = pleiadesViewingModelA.getMinDate();
final AbsoluteDate maxDateA = pleiadesViewingModelA.getMaxDate();
final AbsoluteDate refDateA = pleiadesViewingModelA.getDatationReference();
LineSensor lineSensorA = pleiadesViewingModelA.getLineSensor();
System.out.format(Locale.US, "Viewing model A - date min: %s max: %s ref: %s %n", minDateA, maxDateA, refDateA);
// ----Satellite position, velocity and attitude: create orbit model A
OrbitModel orbitmodelA = new OrbitModel();
BodyShape earthA = orbitmodelA.createEarth();
Orbit orbitA = orbitmodelA.createOrbit(Constants.EIGEN5C_EARTH_MU, refDateA);
// ----If no LOF Transform Attitude Provider is Nadir Pointing Yaw Compensation
final double [] rollPoly = {0.0,0.0,0.0};
double[] pitchPoly = {0.025,0.0};
double[] yawPoly = {0.0,0.0,0.0};
orbitmodelA.setLOFTransform(rollPoly, pitchPoly, yawPoly, minDateA);
// ----Satellite attitude
List<TimeStampedAngularCoordinates> satelliteQListA = orbitmodelA.orbitToQ(orbitA, earthA, minDateA.shiftedBy(-0.0), maxDateA.shiftedBy(+0.0), 0.25);
int nbQPoints = 2;
// ----Position and velocities
PVCoordinates PVA = orbitA.getPVCoordinates(earthA.getBodyFrame());
List<TimeStampedPVCoordinates> satellitePVListA = orbitmodelA.orbitToPV(orbitA, earthA, minDateA.shiftedBy(-0.0), maxDateA.shiftedBy(+0.0), 0.25);
int nbPVPoints = 8;
// ----Convert frame and coordinates type in one call
GeodeticPoint gpA = earthA.transform(PVA.getPosition(), earthA.getBodyFrame(), orbitA.getDate());
System.out.format(Locale.US, "(A) Geodetic Point at date %s : φ = %8.10f °, λ = %8.10f %n",
orbitA.getDate().toString(),
FastMath.toDegrees(gpA.getLatitude()),
FastMath.toDegrees(gpA.getLongitude()));
// Rugged A initialization
// ---------------------
System.out.format("**** Rugged A initialization **** %n");
RuggedBuilder ruggedBuilderA = new RuggedBuilder();
ruggedBuilderA.addLineSensor(lineSensorA);
ruggedBuilderA.setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID);
ruggedBuilderA.setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF);
ruggedBuilderA.setTimeSpan(minDateA,maxDateA, 0.001, 5.0);
ruggedBuilderA.setTrajectory(InertialFrameId.EME2000, satellitePVListA, nbPVPoints,
CartesianDerivativesFilter.USE_PV, satelliteQListA,
nbQPoints, AngularDerivativesFilter.USE_R);
ruggedBuilderA.setLightTimeCorrection(false);
ruggedBuilderA.setAberrationOfLightCorrection(false);
ruggedBuilderA.setName("RuggedA");
Rugged ruggedA = ruggedBuilderA.build();
System.out.format("\n**** Build Pleiades viewing model B and its orbit definition **** %n");
// 2/- Create Second Pleiades Viewing Model
final AbsoluteDate minDateB = pleiadesViewingModelB.getMinDate();
final AbsoluteDate maxDateB = pleiadesViewingModelB.getMaxDate();
final AbsoluteDate refDateB = pleiadesViewingModelB.getDatationReference();
LineSensor lineSensorB = pleiadesViewingModelB.getLineSensor();
System.out.format(Locale.US, "Viewing model B - date min: %s max: %s ref: %s %n", minDateB, maxDateB, refDateB);
// ----Satellite position, velocity and attitude: create orbit model B
OrbitModel orbitmodelB = new OrbitModel();
BodyShape earthB = orbitmodelB.createEarth();
Orbit orbitB = orbitmodelB.createOrbit(Constants.EIGEN5C_EARTH_MU, refDateB);
// ----Satellite attitude
List<TimeStampedAngularCoordinates> satelliteQListB = orbitmodelB.orbitToQ(orbitB, earthB, minDateB.shiftedBy(-0.0), maxDateB.shiftedBy(+0.0), 0.25);
// ----Position and velocities
PVCoordinates PVB = orbitB.getPVCoordinates(earthB.getBodyFrame());
List<TimeStampedPVCoordinates> satellitePVListB = orbitmodelB.orbitToPV(orbitB, earthB, minDateB.shiftedBy(-0.0), maxDateB.shiftedBy(+0.0), 0.25);
GeodeticPoint gpB = earthB.transform(PVB.getPosition(), earthB.getBodyFrame(), orbitB.getDate());
System.out.format(Locale.US, "(B) Geodetic Point at date %s : φ = %8.10f °, λ = %8.10f %n",orbitA.getDate().toString(),
FastMath.toDegrees(gpB.getLatitude()),
FastMath.toDegrees(gpB.getLongitude()));
// Rugged B initialization
// ---------------------
System.out.format("**** Rugged B initialization **** %n");
RuggedBuilder ruggedBuilderB = new RuggedBuilder();
ruggedBuilderB.addLineSensor(lineSensorB);
ruggedBuilderB.setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID);
ruggedBuilderB.setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF);
ruggedBuilderB.setTimeSpan(minDateB,maxDateB, 0.001, 5.0);
ruggedBuilderB.setTrajectory(InertialFrameId.EME2000, satellitePVListB, nbPVPoints,
CartesianDerivativesFilter.USE_PV, satelliteQListB,
nbQPoints, AngularDerivativesFilter.USE_R);
ruggedBuilderB.setLightTimeCorrection(false);
ruggedBuilderB.setAberrationOfLightCorrection(false);
ruggedBuilderB.setName("RuggedB");
Rugged ruggedB = ruggedBuilderB.build();
// Compute distance between LOS
// -----------------------------
double distance = refining.computeDistanceBetweenLOS(ruggedA, lineSensorA, ruggedB, lineSensorB);
System.out.format("distance %f meters %n",distance);
// Initialize disruptions:
// -----------------------
// Introduce rotations around instrument axes (roll and pitch translations, scale factor)
System.out.format("\n**** Add disruptions on both acquisitions (A,B): roll and pitch rotations, scale factor **** %n");
double rollValueA = FastMath.toRadians(0.004);
double pitchValueA = FastMath.toRadians(0.0008);
double rollValueB = FastMath.toRadians(-0.004);
double pitchValueB = FastMath.toRadians(0.0008);
double factorValue = 1.0;
System.out.format("Acquisition A roll: %3.5f \tpitch: %3.5f \tfactor: %3.5f \n",rollValueA,pitchValueA,factorValue);
System.out.format("Acquisition B roll: %3.5f \tpitch: %3.5f \tfactor: %3.5f \n",rollValueB,pitchValueB,factorValue);
// Apply disruptions on physical model (acquisition A)
refining.applyDisruptions(ruggedA, sensorNameA, rollValueA, pitchValueA, factorValue);
// Apply disruptions on physical model (acquisition B)
refining.applyDisruptions(ruggedB, sensorNameB, rollValueB, pitchValueB, factorValue);
// Generate measurements (observations) from physical model disrupted
// ------------------------------------------------------------------
int lineSampling = 1000;
int pixelSampling = 1000;
// Noise definition
// distribution: gaussian(0), vector dimension: 2
final Noise noise = new Noise(0,2);
// {pixelA mean, pixelB mean}
final double[] mean = {5.0,0.0};
// {pixelB std, pixelB std}
final double[] standardDeviation = {0.1,0.1};
noise.setMean(mean);
noise.setStandardDeviation(standardDeviation);
System.out.format("\tSensor A mean: %f std %f %n",mean[0],standardDeviation[0]);
System.out.format("\tSensor B mean: %f std %f %n",mean[1],standardDeviation[1]);
// Inter-measurements (between both viewing models)
InterMeasurementGenerator measurements = refining.generateNoisyPoints(lineSampling, pixelSampling,
ruggedA, sensorNameA,
pleiadesViewingModelA.getDimension(),
ruggedB, sensorNameB,
pleiadesViewingModelB.getDimension(),
noise);
// Compute ground truth residuals
// ------------------------------
System.out.format("\n**** Ground truth residuals **** %n");
refining.computeMetrics(measurements.getInterMapping(), ruggedA, ruggedB, false);
// Initialize physical models without disruptions
// -----------------------------------------------
System.out.format("\n**** Initialize physical models (A,B) without disruptions: reset Roll/Pitch/Factor **** %n");
refining.resetModel(ruggedA, sensorNameA, false);
refining.resetModel(ruggedB, sensorNameB, false);
// Compute initial residuals
// -------------------------
System.out.format("\n**** Initial Residuals **** %n");
refining.computeMetrics(measurements.getInterMapping(), ruggedA, ruggedB, false);
// Start optimization
// ------------------
System.out.format("\n**** Start optimization **** %n");
final int maxIterations = 100;
final double convergenceThreshold = 1.e-7;
List<Rugged> ruggedList = Arrays.asList(ruggedA, ruggedB);
refining.optimization(maxIterations, convergenceThreshold,
measurements.getObservables(), ruggedList);
// Check estimated values
// ----------------------
System.out.format("\n**** Check parameters ajustement **** %n");
System.out.format("Acquisition A:%n");
refining.paramsEstimation(ruggedA, sensorNameA, rollValueA, pitchValueA, factorValue);
System.out.format("Acquisition B:%n");
refining.paramsEstimation(ruggedB, sensorNameB, rollValueB, pitchValueB, factorValue);
// Compute statistics
// ------------------
System.out.format("\n**** Compute Statistics **** %n");
refining.computeMetrics(measurements.getInterMapping(), ruggedA, ruggedB, false);
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
} catch (RuggedException re) {
System.err.println(re.getLocalizedMessage());
System.exit(1);
}
}
/** Constructor */
private InterRefining() {
sensorNameA = "SensorA";
final double incidenceAngleA = -5.0;
final String dateA = "2016-01-01T11:59:50.0";
pleiadesViewingModelA = new PleiadesViewingModel(sensorNameA, incidenceAngleA, dateA);
sensorNameB = "SensorB";
final double incidenceAngleB = 0.0;
final String dateB = "2016-01-01T12:02:50.0";
pleiadesViewingModelB = new PleiadesViewingModel(sensorNameB, incidenceAngleB, dateB);
}
/** Estimate distance between LOS
* @param lineSensorA line sensor A
* @param lineSensorB line sensor B
* @return GSD
*/
private double computeDistanceBetweenLOS(final Rugged ruggedA, final LineSensor lineSensorA,
final Rugged ruggedB, final LineSensor lineSensorB) {
// Get number of line of sensors
int dimensionA = pleiadesViewingModelA.getDimension();
int dimensionB = pleiadesViewingModelB.getDimension();
Vector3D positionA = lineSensorA.getPosition();
// This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
AbsoluteDate lineDateA = lineSensorA.getDate(dimensionA/2);
Vector3D losA = lineSensorA.getLOS(lineDateA,dimensionA/2);
GeodeticPoint centerPointA = ruggedA.directLocation(lineDateA, positionA, losA);
System.out.format(Locale.US, "\ncenter geodetic position A : φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(centerPointA.getLatitude()),
FastMath.toDegrees(centerPointA.getLongitude()),centerPointA.getAltitude());
Vector3D positionB = lineSensorB.getPosition();
// This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
AbsoluteDate lineDateB = lineSensorB.getDate(dimensionB/2);
Vector3D losB = lineSensorB.getLOS(lineDateB,dimensionB/2);
GeodeticPoint centerPointB = ruggedB.directLocation(lineDateB, positionB, losB);
System.out.format(Locale.US, "center geodetic position B : φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(centerPointB.getLatitude()),
FastMath.toDegrees(centerPointB.getLongitude()),centerPointB.getAltitude());
lineDateB = lineSensorB.getDate(0);
losB = lineSensorB.getLOS(lineDateB,0);
GeodeticPoint firstPointB = ruggedB.directLocation(lineDateB, positionB, losB);
System.out.format(Locale.US, "first geodetic position B : φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(firstPointB.getLatitude()),
FastMath.toDegrees(firstPointB.getLongitude()),firstPointB.getAltitude());
lineDateB = lineSensorB.getDate(dimensionB-1);
losB = lineSensorB.getLOS(lineDateB,dimensionB-1);
GeodeticPoint lastPointB = ruggedB.directLocation(lineDateB, positionB, losB);
System.out.format(Locale.US, "last geodetic position B : φ = %8.10f °, λ = %8.10f °, h = %8.3f m%n",
FastMath.toDegrees(lastPointB.getLatitude()),
FastMath.toDegrees(lastPointB.getLongitude()),lastPointB.getAltitude());
double distance = DistanceTools.computeDistanceInMeter(centerPointA, centerPointB);
return distance;
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/Refining.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades;
import java.util.ArrayList;
import java.util.Collection;
import java.util.Collections;
import java.util.List;
import org.hipparchus.optim.nonlinear.vector.leastsquares.LeastSquaresOptimizer.Optimum;
import org.orekit.rugged.adjustment.AdjustmentContext;
import org.orekit.rugged.adjustment.measurements.Observables;
import org.orekit.rugged.adjustment.measurements.SensorToGroundMapping;
import org.orekit.rugged.adjustment.measurements.SensorToSensorMapping;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.errors.RuggedMessages;
import fr.cs.examples.refiningPleiades.generators.GroundMeasurementGenerator;
import fr.cs.examples.refiningPleiades.generators.InterMeasurementGenerator;
import fr.cs.examples.refiningPleiades.generators.Noise;
import fr.cs.examples.refiningPleiades.metrics.LocalisationMetrics;
/**
* Class for refining problems common methods
* @author Jonathan Guinet
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @see SensorToGroundMapping
* @see SensorToSensorMapping
* @see GroundMeasurementGenerator
* @see InterMeasurementGenerator
* @since 2.0
*/
public class Refining {
/**
* Constructor
*/
public Refining() {
}
/** Apply disruptions on acquisition for roll, pitch and scale factor
* @param rugged Rugged instance
* @param sensorName line sensor name
* @param rollValue rotation on roll value
* @param pitchValue rotation on pitch value
* @param factorValue scale factor
*/
public void applyDisruptions(final Rugged rugged, final String sensorName,
final double rollValue, final double pitchValue, final double factorValue) {
rugged.
getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(sensorName + rollSuffix)).
findFirst().get().setValue(rollValue);
rugged.
getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(sensorName + pitchSuffix)).
findFirst().get().setValue(pitchValue);
rugged.
getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(factorName)).
findFirst().get().setValue(factorValue);
}
/** Generate measurements without noise (sensor to ground mapping)
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
* @param rugged Rugged instance
* @param sensorName line sensor name
* @param dimension number of line of the sensor
* @return ground measurements generator (sensor to ground mapping)
*/
public GroundMeasurementGenerator generatePoints(final int lineSampling, final int pixelSampling,
final Rugged rugged, final String sensorName,
final int dimension) {
GroundMeasurementGenerator measurements = new GroundMeasurementGenerator(rugged, sensorName, dimension);
System.out.format("\n**** Generate measurements (without noise; sensor to ground mapping) **** %n");
// Generation measurements without noise
measurements.createMeasurement(lineSampling, pixelSampling);
System.out.format("Number of tie points generated: %d %n", measurements.getMeasurementCount());
return measurements;
}
/** Generate measurements without noise (sensor to sensor mapping)
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
* @param ruggedA Rugged instance of acquisition A
* @param sensorNameA line sensor name A
* @param dimensionA dimension for acquisition A
* @param ruggedB Rugged instance of acquisition B
* @param sensorNameB line sensor name B
* @param dimensionB dimension for acquisition B
* @return inter measurements generator (sensor to sensor mapping)
*/
public InterMeasurementGenerator generatePoints(final int lineSampling, final int pixelSampling,
final Rugged ruggedA, final String sensorNameA, final int dimensionA,
final Rugged ruggedB, final String sensorNameB, final int dimensionB) {
// Outliers control
final double outlierValue = 1e+2;
// Earth constraint weight
final double earthConstraintWeight = 0.1;
// Generate measurements with constraints on outliers control and Earth distance
InterMeasurementGenerator measurements = new InterMeasurementGenerator(ruggedA, sensorNameA, dimensionA,
ruggedB, sensorNameB, dimensionB,
outlierValue,
earthConstraintWeight);
System.out.format("\n**** Generate measurements (without noise; sensor to sensor mapping) **** %n");
// Generation measurements without noise
measurements.createMeasurement(lineSampling, pixelSampling);
System.out.format("Number of tie points generated: %d %n", measurements.getMeasurementCount());
return measurements;
}
/** Generate noisy measurements (sensor to ground mapping)
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
* @param rugged Rugged instance
* @param sensorName line sensor name
* @param dimension dimension
* @param noise Noise structure to generate noisy measurements
* @return ground measurements generator (sensor to ground mapping)
*/
public GroundMeasurementGenerator generateNoisyPoints(final int lineSampling, final int pixelSampling,
final Rugged rugged, final String sensorName, final int dimension,
final Noise noise) {
// Generate ground measurements
GroundMeasurementGenerator measurements = new GroundMeasurementGenerator(rugged, sensorName, dimension);
System.out.format("\n**** Generate noisy measurements (sensor to ground mapping) **** %n");
// Generate noisy measurements
measurements.createNoisyMeasurement(lineSampling, pixelSampling, noise);
System.out.format("Number of tie points generated: %d %n", measurements.getMeasurementCount());
return measurements;
}
/** Generate noisy measurements (sensor to sensor mapping)
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
* @param ruggedA Rugged instance of acquisition A
* @param sensorNameA line sensor name A
* @param dimensionA dimension for acquisition A
* @param ruggedB Rugged instance of acquisition B
* @param sensorNameB line sensor name B
* @param dimensionB dimension for acquisition B
* @param noise noise structure to generate noisy measurements
* @return inter-measurements generator (sensor to sensor mapping)
*/
public InterMeasurementGenerator generateNoisyPoints(final int lineSampling, final int pixelSampling,
final Rugged ruggedA, final String sensorNameA, final int dimensionA,
final Rugged ruggedB, final String sensorNameB, final int dimensionB,
final Noise noise) {
// Outliers control
final double outlierValue = 1.e+2;
// Earth constraint weight
final double earthConstraintWeight = 0.1;
// Generate measurements with constraints on Earth distance and outliers control
InterMeasurementGenerator measurements = new InterMeasurementGenerator(ruggedA, sensorNameA, dimensionA,
ruggedB, sensorNameB, dimensionB,
outlierValue,
earthConstraintWeight);
System.out.format("\n**** Generate noisy measurements (sensor to sensor mapping) **** %n");
// Generation noisy measurements
measurements.createNoisyMeasurement(lineSampling, pixelSampling, noise);
System.out.format("Number of tie points generated: %d %n", measurements.getMeasurementCount());
return measurements;
}
/** Compute metrics to evaluate geometric performances in location,
* for Ground Control Points GCP study.
* @param groundMapping sensor to ground mapping
* @param rugged Rugged instance
* @param unit flag to know if distance is computed in meters (false) or with angular (true)
*/
public void computeMetrics(final SensorToGroundMapping groundMapping,
final Rugged rugged, final boolean unit) {
String stUnit = null;
if(unit) {
stUnit="degrees";
} else {
stUnit="meters";
}
LocalisationMetrics residuals = new LocalisationMetrics(groundMapping, rugged, unit);
System.out.format("Max: %3.4e Mean: %3.4e %s%n",residuals.getMaxResidual(),residuals.getMeanResidual(), stUnit);
}
/** Compute metrics to evaluate geometric performances in location,
* for tie points study.
* @param interMapping sensor to sensor mapping
* @param ruggedA Rugged instance A
* @param ruggedB Rugged instance B
* @param unit flag to know if distance is computed in meters (false) or with angular (true)
*/
public void computeMetrics(final SensorToSensorMapping interMapping,
final Rugged ruggedA, final Rugged ruggedB,
final boolean unit) {
String stUnit = null;
if(unit) stUnit="degrees";
else stUnit="meters";
LocalisationMetrics residuals = new LocalisationMetrics(interMapping, ruggedA, ruggedB, unit);
System.out.format("Max: %1.4e Mean: %1.4e %s%n",residuals.getMaxResidual(),residuals.getMeanResidual(), stUnit);
System.out.format("LOS distance Max: %1.4e Mean: %1.4e %s%n",residuals.getLosMaxDistance(),residuals.getLosMeanDistance(), stUnit);
System.out.format("Earth distance Max: %1.4e Mean: %1.4e %s%n",residuals.getEarthMaxDistance(),residuals.getEarthMeanDistance(), stUnit);
}
/** Reset a model
* @param rugged Rugged instance
* @param sensorName line sensor name
* @param isSelected flag to known if factor parameter is selected or not
*/
public void resetModel(final Rugged rugged, final String sensorName, final boolean isSelected) {
rugged.
getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(sensorName + rollSuffix)
|| driver.getName().equals(sensorName + pitchSuffix)).
forEach(driver -> {
driver.setSelected(true);
driver.setValue(0.0);
});
rugged.
getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(factorName)).
forEach(driver -> {
driver.setSelected(isSelected);
// default value: no Z scale factor applied
driver.setValue(1.0);
});
}
/** Start optimization to adjust parameters (Ground Control Points GCP study).
* @param maxIterations iterations max
* @param convergenceThreshold threshold of convergence
* @param measurements ground measurements
* @param rugged Rugged instance
*/
public void optimization(final int maxIterations, final double convergenceThreshold,
final Observables measurements, final Rugged rugged) {
System.out.format("Iterations max: %d\tconvergence threshold: %3.6e \n", maxIterations, convergenceThreshold);
AdjustmentContext adjustmentContext = new AdjustmentContext(Collections.singletonList(rugged), measurements);
Optimum optimum = adjustmentContext.estimateFreeParameters(Collections.singletonList(rugged.getName()), maxIterations, convergenceThreshold);
// Print statistics
System.out.format("Max value: %3.6e %n", optimum.getResiduals().getMaxValue());
System.out.format("Optimization performed in %d iterations \n", optimum.getIterations());
System.out.format("Optimization performed with %d evaluations of model (objective) function \n", optimum.getEvaluations());
System.out.format("RMSE: %f \n", optimum.getRMS());
}
/** Start optimization to adjust parameters (tie points study).
* @param maxIterations iterations max
* @param convergenceThreshold threshold of convergence
* @param measurements measurements
* @param ruggeds Rugged instances A and B
*/
public void optimization(final int maxIterations, final double convergenceThreshold,
final Observables measurements,
final Collection<Rugged> ruggeds) {
System.out.format("Iterations max: %d\tconvergence threshold: %3.6e \n", maxIterations, convergenceThreshold);
if(ruggeds.size()!= 2 ) {
throw new RuggedException(RuggedMessages.UNSUPPORTED_REFINING_CONTEXT,ruggeds.size());
}
AdjustmentContext adjustmentContext = new AdjustmentContext(ruggeds, measurements);
List<String> ruggedNameList = new ArrayList<String>();
for(Rugged rugged : ruggeds) {
ruggedNameList.add(rugged.getName());
}
Optimum optimum = adjustmentContext.estimateFreeParameters(ruggedNameList, maxIterations, convergenceThreshold);
// Print statistics
System.out.format("Max value: %3.6e %n", optimum.getResiduals().getMaxValue());
System.out.format("Optimization performed in %d iterations \n", optimum.getIterations());
System.out.format("Optimization performed with %d evaluations of model (objective) function \n", optimum.getEvaluations());
System.out.format("RMSE: %f \n", optimum.getRMS());
}
/** Check adjusted parameters of an acquisition
* @param rugged Rugged instance
* @param sensorName line sensor name
* @param rollValue rotation on roll value
* @param pitchValue rotation on pitch value
* @param factorValue scale factor
*/
public void paramsEstimation(final Rugged rugged, final String sensorName,
final double rollValue, final double pitchValue, final double factorValue) {
// Estimate Roll
double estimatedRoll = rugged.getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(sensorName + rollSuffix)).
findFirst().get().getValue();
double rollError = (estimatedRoll - rollValue);
System.out.format("Estimated roll: %3.5f\troll error: %3.6e %n", estimatedRoll, rollError);
// Estimate pitch
double estimatedPitch = rugged.getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(sensorName + pitchSuffix)).
findFirst().get().getValue();
double pitchError = (estimatedPitch - pitchValue);
System.out.format("Estimated pitch: %3.5f\tpitch error: %3.6e %n", estimatedPitch, pitchError);
// Estimate scale factor
double estimatedFactor = rugged.getLineSensor(sensorName).
getParametersDrivers().
filter(driver -> driver.getName().equals(factorName)).
findFirst().get().getValue();
double factorError = (estimatedFactor - factorValue);
System.out.format("Estimated factor: %3.5f\tfactor error: %3.6e %n", estimatedFactor, factorError);
}
/**
* Part of the name of parameter drivers
*/
static final String rollSuffix = "_roll";
static final String pitchSuffix = "_pitch";
static final String factorName = "factor";
public static String getRollsuffix() {
return rollSuffix;
}
public static String getPitchsuffix() {
return pitchSuffix;
}
public static String getFactorname() {
return factorName;
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/generators/GroundMeasurementGenerator.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.generators;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.random.GaussianRandomGenerator;
import org.hipparchus.random.UncorrelatedRandomVectorGenerator;
import org.hipparchus.random.Well19937a;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.rugged.adjustment.measurements.Observables;
import org.orekit.rugged.adjustment.measurements.SensorToGroundMapping;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.time.AbsoluteDate;
/** Ground measurements generator (sensor to ground mapping).
* @author Jonathan Guinet
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @since 2.0
*/
public class GroundMeasurementGenerator implements Measurable {
/** Sensor to ground mapping. */
private SensorToGroundMapping groundMapping;
/** Observables which contains ground mapping. */
private Observables observables;
/** Rugged instance */
private Rugged rugged;
/** Line sensor */
private LineSensor sensor;
/** Number of lines of the sensor */
private int dimension;
/** Number of measurements */
private int measurementCount;
/** Simple constructor.
* @param rugged Rugged instance
* @param sensorName sensor name
* @param dimension number of line of the sensor
*/
public GroundMeasurementGenerator(final Rugged rugged, final String sensorName, final int dimension) {
// Generate reference mapping
this.groundMapping = new SensorToGroundMapping(rugged.getName(), sensorName);
// Create observables for one model
this.observables = new Observables(1);
this.rugged = rugged;
this.sensor = rugged.getLineSensor(groundMapping.getSensorName());
this.dimension = dimension;
this.measurementCount = 0;
}
/** Get the sensor to ground mapping
* @return the sensor to ground mapping
*/
public SensorToGroundMapping getGroundMapping() {
return groundMapping;
}
/** Get the observables which contains the ground mapping
* @return the observables which contains the ground mapping
*/
public Observables getObservables() {
return observables;
}
@Override
public int getMeasurementCount() {
return measurementCount;
}
@Override
public void createMeasurement(final int lineSampling, final int pixelSampling) {
for (double line = 0; line < dimension; line += lineSampling) {
final AbsoluteDate date = sensor.getDate(line);
for (int pixel = 0; pixel < sensor.getNbPixels(); pixel += pixelSampling) {
final GeodeticPoint gp2 = rugged.directLocation(date, sensor.getPosition(),
sensor.getLOS(date, pixel));
groundMapping.addMapping(new SensorPixel(line, pixel), gp2);
// increment the number of measurements
measurementCount++;
}
}
observables.addGroundMapping(groundMapping);
}
@Override
public void createNoisyMeasurement(final int lineSampling, final int pixelSampling, final Noise noise) {
// Estimate latitude and longitude errors (rad)
final Vector3D latLongError = estimateLatLongError();
// Get noise features
final double[] mean = noise.getMean(); // [latitude, longitude, altitude] mean
final double[] std = noise.getStandardDeviation(); // [latitude, longitude, altitude] standard deviation
final double latErrorMean = mean[0] * latLongError.getX();
final double lonErrorMean = mean[1] * latLongError.getY();
final double latErrorStd = std[0] * latLongError.getX();
final double lonErrorStd = std[1] * latLongError.getY();
// Gaussian random generator
// Build a null mean random uncorrelated vector generator with standard deviation corresponding to the estimated error on ground
final double meanGenerator[] = {latErrorMean, lonErrorMean, mean[2]};
final double stdGenerator[] = {latErrorStd, lonErrorStd, std[2]};
// seed has been fixed for tests purpose
final GaussianRandomGenerator rng = new GaussianRandomGenerator(new Well19937a(0xefac03d9be4d24b9l));
final UncorrelatedRandomVectorGenerator rvg = new UncorrelatedRandomVectorGenerator(meanGenerator, stdGenerator, rng);
for (double line = 0; line < dimension; line += lineSampling) {
final AbsoluteDate date = sensor.getDate(line);
for (int pixel = 0; pixel < sensor.getNbPixels(); pixel += pixelSampling) {
// Components of generated vector follow (independent) Gaussian distribution
final Vector3D vecRandom = new Vector3D(rvg.nextVector());
final GeodeticPoint gp2 = rugged.directLocation(date, sensor.getPosition(),
sensor.getLOS(date, pixel));
final GeodeticPoint gpNoisy = new GeodeticPoint(gp2.getLatitude() + vecRandom.getX(),
gp2.getLongitude() + vecRandom.getY(),
gp2.getAltitude() + vecRandom.getZ());
groundMapping.addMapping(new SensorPixel(line, pixel), gpNoisy);
// increment the number of measurements
measurementCount++;
}
}
this.observables.addGroundMapping(groundMapping);
}
/** Compute latitude and longitude errors
* @return the latitude and longitude errors (rad)
*/
private Vector3D estimateLatLongError() {
final int pix = sensor.getNbPixels() / 2;
final int line = (int) FastMath.floor(pix); // assumption : same number of line and pixels;
final AbsoluteDate date = sensor.getDate(line);
final GeodeticPoint gp_pix0 = rugged.directLocation(date, sensor.getPosition(), sensor.getLOS(date, pix));
final AbsoluteDate date1 = sensor.getDate(line + 1);
final GeodeticPoint gp_pix1 = rugged.directLocation(date1, sensor.getPosition(), sensor.getLOS(date1, pix + 1));
final double latErr = FastMath.abs(gp_pix0.getLatitude() - gp_pix1.getLatitude());
final double lonErr = FastMath.abs(gp_pix0.getLongitude() - gp_pix1.getLongitude());
return new Vector3D(latErr, lonErr, 0.0);
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/generators/InterMeasurementGenerator.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.generators;
import org.hipparchus.random.GaussianRandomGenerator;
import org.hipparchus.random.UncorrelatedRandomVectorGenerator;
import org.hipparchus.random.Well19937a;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.errors.RuggedMessages;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.adjustment.measurements.Observables;
import org.orekit.rugged.adjustment.measurements.SensorToSensorMapping;
import org.orekit.rugged.utils.SpacecraftToObservedBody;
import org.orekit.time.AbsoluteDate;
import fr.cs.examples.refiningPleiades.metrics.DistanceTools;
/**
* Inter-measurements generator (sensor to sensor mapping).
* @author Jonathan Guinet
* @author Lucie Labatallee
* @author Guylaine Prat
* @since 2.0
*/
public class InterMeasurementGenerator implements Measurable {
/** Mapping from sensor A to sensor B. */
private SensorToSensorMapping interMapping;
/** Observables which contains sensor to sensor mapping.*/
private Observables observables;
/** Rugged instance corresponding to the viewing model A */
private Rugged ruggedA;
/** Rugged instance corresponding to the viewing model B */
private Rugged ruggedB;
/** Sensor A */
private LineSensor sensorA;
/** Sensor B */
private LineSensor sensorB;
/** Number of measurements */
private int measurementCount;
/** Sensor name B */
private String sensorNameB;
/** Number of line for acquisition A */
private int dimensionA;
/** Number of line for acquisition B */
private int dimensionB;
/** Limit value for outlier points */
private double outlier;
/** Default constructor: measurements generation without outlier points control
* and without Earth distance constraint.
* @param ruggedA Rugged instance corresponding to the viewing model A
* @param sensorNameA sensor name A
* @param dimensionA number of line for acquisition A
* @param ruggedB Rugged instance corresponding to the viewing model B
* @param sensorNameB sensor name B
* @param dimensionB number of line for acquisition B
*/
public InterMeasurementGenerator(final Rugged ruggedA, final String sensorNameA, final int dimensionA,
final Rugged ruggedB, final String sensorNameB, final int dimensionB) {
// Initialize parameters
initParams(ruggedA, sensorNameA, dimensionA, ruggedB, sensorNameB, dimensionB);
// Generate reference mapping, without Earth distance constraint
interMapping = new SensorToSensorMapping(sensorNameA, sensorNameB);
// Create observables for two models
observables = new Observables(2);
}
/** Constructor for measurements generation taking into account outlier points control,
* without Earth distance constraint.
* @param ruggedA Rugged instance corresponding to the viewing model A
* @param sensorNameA sensor name A
* @param dimensionA dimension for acquisition A
* @param ruggedB Rugged instance corresponding to the viewing model B
* @param sensorNameB sensor name B
* @param dimensionB dimension for acquisition B
* @param outlier limit value for outlier points
*/
public InterMeasurementGenerator(final Rugged ruggedA, final String sensorNameA, final int dimensionA,
final Rugged ruggedB, final String sensorNameB, final int dimensionB,
final double outlier) {
this(ruggedA, sensorNameA, dimensionA, ruggedB, sensorNameB, dimensionB);
this.outlier = outlier;
}
/** Constructor for measurements generation taking into account outlier points control,
* and Earth distance constraint.
* @param ruggedA Rugged instance corresponding to the viewing model A
* @param sensorNameA sensor name A
* @param dimensionA dimension for acquisition A
* @param ruggedB Rugged instance corresponding to the viewing model B
* @param sensorNameB sensor name B
* @param dimensionB dimension for acquisition B
* @param outlier limit value for outlier points
* @param earthConstraintWeight weight given to the Earth distance constraint
* with respect to the LOS distance (between 0 and 1).
*/
public InterMeasurementGenerator(final Rugged ruggedA, final String sensorNameA, final int dimensionA,
final Rugged ruggedB, final String sensorNameB, final int dimensionB,
final double outlier, final double earthConstraintWeight) {
// Initialize parameters
initParams(ruggedA, sensorNameA, dimensionA, ruggedB, sensorNameB, dimensionB);
// Generate reference mapping, with Earth distance constraints.
// Weighting will be applied as follow :
// (1-earthConstraintWeight) for losDistance weighting
// earthConstraintWeight for earthDistance weighting
interMapping = new SensorToSensorMapping(sensorNameA, ruggedA.getName(), sensorNameB, ruggedB.getName(), earthConstraintWeight);
// Outlier points control
this.outlier = outlier;
// Observables which contains sensor to sensor mapping
this.observables = new Observables(2);
}
/** Get the mapping from sensor A to sensor B
* @return the mapping from sensor A to sensor B
*/
public SensorToSensorMapping getInterMapping() {
return interMapping;
}
/** Get the observables which contains sensor to sensor mapping
* @return the observables which contains sensor to sensor mapping
*/
public Observables getObservables() {
return observables;
}
@Override
public int getMeasurementCount() {
return measurementCount;
}
@Override
public void createMeasurement(final int lineSampling, final int pixelSampling) {
// Search the sensor pixel seeing point
final int minLine = 0;
final int maxLine = dimensionB - 1;
for (double line = 0; line < dimensionA; line += lineSampling) {
final AbsoluteDate dateA = sensorA.getDate(line);
for (double pixelA = 0; pixelA < sensorA.getNbPixels(); pixelA += pixelSampling) {
final GeodeticPoint gpA = ruggedA.directLocation(dateA, sensorA.getPosition(),
sensorA.getLOS(dateA, pixelA));
final SensorPixel sensorPixelB = ruggedB.inverseLocation(sensorNameB, gpA, minLine, maxLine);
// We need to test if the sensor pixel is found in the prescribed lines
// otherwise the sensor pixel is null
if (sensorPixelB != null) {
final AbsoluteDate dateB = sensorB.getDate(sensorPixelB.getLineNumber());
final double pixelB = sensorPixelB.getPixelNumber();
final SpacecraftToObservedBody scToBodyA = ruggedA.getScToBody();
final GeodeticPoint gpB = ruggedB.directLocation(dateB, sensorB.getPosition(),
sensorB.getLOS(dateB, pixelB));
final double geoDistance = DistanceTools.computeDistanceInMeter(gpA, gpB);
if (geoDistance < this.outlier) {
final SensorPixel realPixelA = new SensorPixel(line, pixelA);
final SensorPixel realPixelB = new SensorPixel(sensorPixelB.getLineNumber(), sensorPixelB.getPixelNumber());
final AbsoluteDate realDateA = sensorA.getDate(realPixelA.getLineNumber());
final AbsoluteDate realDateB = sensorB.getDate(realPixelB.getLineNumber());
final double[] distanceLOSB = ruggedB.distanceBetweenLOS(sensorA, realDateA, realPixelA.getPixelNumber(), scToBodyA,
sensorB, realDateB, realPixelB.getPixelNumber());
final double losDistance = 0.0;
final double earthDistance = distanceLOSB[1];
interMapping.addMapping(realPixelA, realPixelB, losDistance, earthDistance);
// Increment the number of measurements
this.measurementCount++;
}
}
}
}
this.observables.addInterMapping(interMapping);
}
/** Tie point creation from direct 1ocation with Rugged A and inverse location with Rugged B
* @param lineSampling sampling along lines
* @param pixelSampling sampling along columns
* @param noise errors to apply to measure for pixel A and pixel B
*/
public void createNoisyMeasurement(final int lineSampling, final int pixelSampling, final Noise noise) {
// Get noise features (errors)
// [pixelA, pixelB] mean
final double[] mean = noise.getMean();
// [pixelA, pixelB] standard deviation
final double[] std = noise.getStandardDeviation();
// Search the sensor pixel seeing point
final int minLine = 0;
final int maxLine = dimensionB - 1;
final double meanA[] = { mean[0], mean[0] };
final double stdA[] = { std[0], std[0] };
final double meanB[] = { mean[1], mean[1] };
final double stdB[] = { std[1], std[1] };
// Seed has been fixed for tests purpose
final GaussianRandomGenerator rngA = new GaussianRandomGenerator(new Well19937a(0xefac03d9be4d24b9l));
final UncorrelatedRandomVectorGenerator rvgA = new UncorrelatedRandomVectorGenerator(meanA, stdA, rngA);
// Seed has been fixed for tests purpose
final GaussianRandomGenerator rngB = new GaussianRandomGenerator(new Well19937a(0xdf1c03d9be0b34b9l));
final UncorrelatedRandomVectorGenerator rvgB = new UncorrelatedRandomVectorGenerator(meanB, stdB, rngB);
for (double line = 0; line < dimensionA; line += lineSampling) {
final AbsoluteDate dateA = sensorA.getDate(line);
for (double pixelA = 0; pixelA < sensorA.getNbPixels(); pixelA += pixelSampling) {
final GeodeticPoint gpA = ruggedA.directLocation(dateA, sensorA.getPosition(),
sensorA.getLOS(dateA, pixelA));
final SensorPixel sensorPixelB = ruggedB.inverseLocation(sensorNameB, gpA, minLine, maxLine);
// We need to test if the sensor pixel is found in the prescribed lines
// otherwise the sensor pixel is null
if (sensorPixelB != null) {
final AbsoluteDate dateB = sensorB.getDate(sensorPixelB.getLineNumber());
final double pixelB = sensorPixelB.getPixelNumber();
// Get spacecraft to body transform of Rugged instance A
final SpacecraftToObservedBody scToBodyA = ruggedA.getScToBody();
final GeodeticPoint gpB = ruggedB.directLocation(dateB, sensorB.getPosition(),
sensorB.getLOS(dateB, pixelB));
final double geoDistance = DistanceTools.computeDistanceInMeter(gpA, gpB);
// Create the inter mapping if distance is below outlier value
if (geoDistance < outlier) {
final double[] vecRandomA = rvgA.nextVector();
final double[] vecRandomB = rvgB.nextVector();
final SensorPixel realPixelA = new SensorPixel(line + vecRandomA[0], pixelA + vecRandomA[1]);
final SensorPixel realPixelB = new SensorPixel(sensorPixelB.getLineNumber() + vecRandomB[0],
sensorPixelB.getPixelNumber() + vecRandomB[1]);
final AbsoluteDate realDateA = sensorA.getDate(realPixelA.getLineNumber());
final AbsoluteDate realDateB = sensorB.getDate(realPixelB.getLineNumber());
final double[] distanceLOSB = ruggedB.distanceBetweenLOS(sensorA, realDateA, realPixelA.getPixelNumber(), scToBodyA,
sensorB, realDateB, realPixelB.getPixelNumber());
final Double losDistance = 0.0;
final Double earthDistance = distanceLOSB[1];
interMapping.addMapping(realPixelA, realPixelB, losDistance, earthDistance);
// Increment the number of measurements
this.measurementCount++;
} // end test if geoDistance < outlier
} // end test if sensorPixelB != null
} // end loop on pixel of sensorA
} // end loop on line of sensorA
this.observables.addInterMapping(interMapping);
}
/** Default constructor: measurements generation without outlier points control
* and Earth distances constraint.
* @param rA Rugged instance A
* @param sNameA sensor name A
* @param dimA dimension for acquisition A
* @param rB Rugged instance B
* @param sNameB sensor name B
* @param dimB dimension for acquisition B
*/
private void initParams(final Rugged rA, final String sNameA, final int dimA,
final Rugged rB, final String sNameB, final int dimB) {
this.sensorNameB = sNameB;
// Check that sensors's name is different
if (sNameA.contains(sNameB)) {
throw new RuggedException(RuggedMessages.DUPLICATED_PARAMETER_NAME, sNameA);
}
this.ruggedA = rA;
this.ruggedB = rB;
this.sensorA = rA.getLineSensor(sNameA);
this.sensorB = rB.getLineSensor(sNameB);
this.dimensionA = dimA;
this.dimensionB = dimB;
this.measurementCount = 0;
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/generators/Measurable.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.generators;
/** For measurements generator.
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @since 2.0
*/
public interface Measurable {
/** Get the number of measurements
* @return the number of measurements
*/
int getMeasurementCount();
/** Create measurements (without noise)
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
*/
void createMeasurement(int lineSampling, int pixelSampling);
/** Create noisy measurements
* @param lineSampling line sampling
* @param pixelSampling pixel sampling
* @param noise the noise to add to the measurements
*/
void createNoisyMeasurement(int lineSampling, int pixelSampling, Noise noise);
}
src/tutorials/java/fr/cs/examples/refiningPleiades/generators/Noise.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.generators;
/** Class for adding a noise to measurements.
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @since 2.0
*/
public class Noise {
/** Type of distribution. */
private static final int GAUSSIAN = 0;
/** Dimension. */
private int dimension;
/** Mean. */
private double[] mean;
/** Standard deviation. */
private double[] standardDeviation;
/** Distribution. */
private int distribution = GAUSSIAN;
/** Build a new instance.
* @param distribution noise type
* @param dimension noise dimension
*/
public Noise(final int distribution, final int dimension) {
this.mean = new double[dimension];
this.standardDeviation = new double[dimension];
this.dimension = dimension;
this.distribution = distribution;
}
/** Get the mean.
* @return the mean
*/
public double[] getMean() {
return mean.clone();
}
/** Set the mean.
* @param meanValue the mean to set
*/
public void setMean(final double[] meanValue) {
this.mean = meanValue.clone();
}
/** Get the standard deviation.
* @return the standard deviation
*/
public double[] getStandardDeviation() {
return standardDeviation.clone();
}
/** Set the standard deviation.
* @param standardDeviationValue the standard deviation to set
*/
public void setStandardDeviation(final double[] standardDeviationValue) {
this.standardDeviation = standardDeviationValue.clone();
}
/** Get the distribution.
* @return the distribution
*/
public int getDistribution() {
return distribution;
}
/** Get the dimension.
* @return the dimension
*/
public int getDimension() {
return dimension;
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/metrics/DistanceTools.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.metrics;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.utils.Constants;
/**
* Class for computing geodetic and anguler distance between two geodetic points.
* @author Jonathan Guinet
* @author Guylaine Prat
* @since 2.0
*/
public class DistanceTools {
/** Private constructor for utility class.
*/
private DistanceTools() {
}
/** Choice the method for computing geodetic distance between two points.
* @param geoPoint1 first geodetic point (rad)
* @param geoPoint2 second geodetic point (rad)
* @param computeAngular if true, distance will be angular, otherwise will be in meters
* @return distance in meters or radians if flag computeAngular is true
*/
public static double computeDistance(final GeodeticPoint geoPoint1, final GeodeticPoint geoPoint2,
final boolean computeAngular) {
if (computeAngular == true) {
return computeDistanceAngular(geoPoint1, geoPoint2);
} else {
return computeDistanceInMeter(geoPoint1, geoPoint2);
}
}
/** Compute a geodetic distance in meters between two geodetic points..
* @param geoPoint1 first geodetic point (rad)
* @param geoPoint2 second geodetic point (rad)
* @return distance in meters
*/
public static double computeDistanceInMeter(final GeodeticPoint geoPoint1, final GeodeticPoint geoPoint2) {
// get vectors on unit sphere from angular coordinates
final Vector3D p1 = new Vector3D(geoPoint1.getLatitude(), geoPoint1.getLongitude()); //
final Vector3D p2 = new Vector3D(geoPoint2.getLatitude(), geoPoint2.getLongitude());
final double distance = Constants.WGS84_EARTH_EQUATORIAL_RADIUS * Vector3D.angle(p1, p2);
return distance;
}
/** Compute an angular distance between two geodetic points.
* @param geoPoint1 first geodetic point (rad)
* @param geoPoint2 second geodetic point (rad)
* @return angular distance in radians
*/
public static double computeDistanceAngular(final GeodeticPoint geoPoint1, final GeodeticPoint geoPoint2) {
final double lonDiff = geoPoint1.getLongitude() - geoPoint2.getLongitude();
final double latDiff = geoPoint1.getLatitude() - geoPoint2.getLatitude();
return FastMath.hypot(lonDiff, latDiff);
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/metrics/LocalisationMetrics.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.metrics;
import java.util.Iterator;
import java.util.Map;
import java.util.Set;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.rugged.adjustment.measurements.SensorToGroundMapping;
import org.orekit.rugged.adjustment.measurements.SensorToSensorMapping;
import org.orekit.rugged.api.Rugged;
import org.orekit.rugged.linesensor.LineSensor;
import org.orekit.rugged.linesensor.SensorPixel;
import org.orekit.rugged.utils.SpacecraftToObservedBody;
import org.orekit.time.AbsoluteDate;
/**
* Class for testing geometric performances in absolute location.
* Metrics are computed for two scenarios: ground control points and tie points.
* @see SensorToSensorMapping
* @see SensorToGroundMapping
* @author Jonathan Guinet
* @author Lucie Labat-Allee
* @author Guylaine Prat
* @since 2.0
*/
public class LocalisationMetrics {
/** Maximum residual distance. */
private double resMax;
/** Mean residual distance. */
private double resMean;
/** LOS distance max. */
private double losDistanceMax;
/** LOS distance mean. */
private double losDistanceMean;
/** Earth distance max. */
private double earthDistanceMax;
/** Earth distance mean.*/
private double earthDistanceMean;
/** Compute metrics corresponding to the Ground Control Points (GCP) study.
* @param measMapping Mapping of observations/measurements = the ground truth
* @param rugged Rugged instance
* @param computeAngular flag to know if distance is computed in meters (false) or with angular (true)
*/
public LocalisationMetrics(final SensorToGroundMapping measMapping, final Rugged rugged, final boolean computeAngular) {
// Initialization
this.resMax = 0.0;
this.resMean = 0.0;
// Compute metrics - Case of Sensor to Ground mapping (Ground Control Points GCP study)
computeGCPmetrics(measMapping, rugged, computeAngular);
}
/** Compute metrics corresponding to the tie points study.
* @param measMapping Mapping of observations/measurements = the ground truth
* @param ruggedA Rugged instance corresponding to viewing model A
* @param ruggedB Rugged instance corresponding to viewing model B
* @param computeAngular flag to know if distance is computed in meters (false) or with angular (true)
*/
public LocalisationMetrics(final SensorToSensorMapping measMapping, final Rugged ruggedA, final Rugged ruggedB,
final boolean computeAngular) {
// Initialization
this.resMax = 0.0;
this.resMean = 0.0;
this.losDistanceMax = 0.0;
this.losDistanceMean = 0.0;
this.earthDistanceMax = 0.0;
this.earthDistanceMean = 0.0;
// Compute metrics - Case of Sensor to Sensor mapping (tie points study)
computeTiePointsMetrics(measMapping, ruggedA, ruggedB, computeAngular);
}
/**
* Compute metrics: case of ground control points (GCP).
* @param measMapping Mapping of observations/measurements = the ground truth
* @param rugged Rugged instance
* @param computeAngular flag to know if distance is computed in meters (false) or with angular (true)
*/
public void computeGCPmetrics(final SensorToGroundMapping measMapping, final Rugged rugged, final boolean computeAngular) {
// Mapping of observations/measurements = the ground truth
final Set<Map.Entry<SensorPixel, GeodeticPoint>> measurementsMapping;
final LineSensor lineSensor;
// counter for compute mean distance
double count = 0;
// Initialization
measurementsMapping = measMapping.getMapping();
lineSensor = rugged.getLineSensor(measMapping.getSensorName());
// number of measurements
int nbMeas = measurementsMapping.size();
final Iterator<Map.Entry<SensorPixel, GeodeticPoint>> gtIt = measurementsMapping.iterator();
// Browse map of measurements
while (gtIt.hasNext()) {
final Map.Entry<SensorPixel, GeodeticPoint> gtMeas = gtIt.next();
final SensorPixel gtSP = gtMeas.getKey();
final GeodeticPoint gtGP = gtMeas.getValue();
final AbsoluteDate date = lineSensor.getDate(gtSP.getLineNumber());
final GeodeticPoint esGP = rugged.directLocation(date, lineSensor.getPosition(),
lineSensor.getLOS(date,
(int) gtSP.getPixelNumber()));
// Compute distance
double distance = DistanceTools.computeDistance(esGP, gtGP, computeAngular);
count += distance;
if (distance > resMax) {
resMax = distance;
}
}
// Mean of residuals
resMean = count / nbMeas;
}
/**
* Compute metrics: case of tie points.
* @param measMapping Mapping of observations/measurements = the ground truth
* @param ruggedA Rugged instance corresponding to viewing model A
* @param ruggedB Rugged instance corresponding to viewing model B
* @param computeAngular Flag to know if distance is computed in meters (false) or with angular (true)
*/
public void computeTiePointsMetrics(final SensorToSensorMapping measMapping, final Rugged ruggedA, final Rugged ruggedB,
final boolean computeAngular) {
// Mapping of observations/measurements = the ground truth
final Set<Map.Entry<SensorPixel, SensorPixel>> measurementsMapping;
final LineSensor lineSensorA; // line sensor corresponding to rugged A
final LineSensor lineSensorB; // line sensor corresponding to rugged B
double count = 0; // counter for computing remaining mean distance
double losDistanceCount = 0; // counter for computing LOS distance mean
double earthDistanceCount = 0; // counter for computing Earth distance mean
int i = 0; // increment of measurements
// Initialization
measurementsMapping = measMapping.getMapping();
lineSensorA = ruggedA.getLineSensor(measMapping.getSensorNameA());
lineSensorB = ruggedB.getLineSensor(measMapping.getSensorNameB());
int nbMeas = measurementsMapping.size(); // number of measurements
// Browse map of measurements
for (Iterator<Map.Entry<SensorPixel, SensorPixel>> gtIt = measurementsMapping.iterator();
gtIt.hasNext();
i++) {
if (i == measurementsMapping.size()) {
break;
}
final Map.Entry<SensorPixel, SensorPixel> gtMapping = gtIt.next();
final SensorPixel spA = gtMapping.getKey();
final SensorPixel spB = gtMapping.getValue();
final AbsoluteDate dateA = lineSensorA.getDate(spA.getLineNumber());
final AbsoluteDate dateB = lineSensorB.getDate(spB.getLineNumber());
final double pixelA = spA.getPixelNumber();
final double pixelB = spB.getPixelNumber();
final Vector3D losA = lineSensorA.getLOS(dateA, pixelA);
final Vector3D losB = lineSensorB.getLOS(dateB, pixelB);
final GeodeticPoint gpA = ruggedA.directLocation(dateA, lineSensorA.getPosition(), losA);
final GeodeticPoint gpB = ruggedB.directLocation(dateB, lineSensorB.getPosition(), losB);
final SpacecraftToObservedBody scToBodyA = ruggedA.getScToBody();
// Estimated distances (LOS / Earth)
final double[] distances = ruggedB.distanceBetweenLOS(lineSensorA, dateA, pixelA, scToBodyA, lineSensorB, dateB, pixelB);
// LOS distance control
final double estLosDistance = distances[0]; // LOS distance estimation
if (estLosDistance > losDistanceMax) {
losDistanceMax = estLosDistance;
}
losDistanceCount += estLosDistance;
// Earth distance control
final double estEarthDistance = distances[1]; // Earth distance estimation
final double measEarthDistance = measMapping.getBodyDistance(i).doubleValue(); // Earth measurement distance
final double earthDistance = FastMath.abs(estEarthDistance - measEarthDistance);
if (earthDistance > earthDistanceMax) {
earthDistanceMax = earthDistance;
}
earthDistanceCount += earthDistance;
// Compute remaining distance
double distance = DistanceTools.computeDistance(gpB, gpA, computeAngular);
count += distance;
if (distance > resMax) {
resMax = distance;
}
}
resMean = count / nbMeas;
losDistanceMean = losDistanceCount / nbMeas;
earthDistanceMean = earthDistanceCount / nbMeas;
}
/** Get the max residual.
* @return maximum of residuals
*/
public double getMaxResidual() {
return resMax;
}
/** Get the mean of residuals.
* @return mean of residuals
*/
public double getMeanResidual() {
return resMean;
}
/** Get the LOS maximum distance.
* @return LOS maximum distance
*/
public double getLosMaxDistance() {
return losDistanceMax;
}
/** Get the LOS mean distance.
* @return LOS mean distance
*/
public double getLosMeanDistance() {
return losDistanceMean;
}
/** Get the Earth distance maximum residual.
* @return Earth distance max residual
*/
public double getEarthMaxDistance() {
return earthDistanceMax;
}
/** Get the Earth distance mean residual.
* @return Earth distance mean residual
*/
public double getEarthMeanDistance() {
return earthDistanceMean;
}
}
src/tutorials/java/fr/cs/examples/refiningPleiades/models/OrbitModel.java 0 → 100644
View file @ acf902ea
/* Copyright 2013-2022 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package fr.cs.examples.refiningPleiades.models;
import java.util.ArrayList;
import java.util.List;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.RotationConvention;
import org.hipparchus.geometry.euclidean.threed.RotationOrder;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.attitudes.LofOffset;
import org.orekit.attitudes.NadirPointing;
import org.orekit.attitudes.TabulatedLofOffset;
import org.orekit.attitudes.YawCompensation;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.forces.gravity.potential.GravityFieldFactory;
import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.frames.LOFType;
import org.orekit.frames.Transform;
import org.orekit.orbits.CircularOrbit;
import org.orekit.orbits.Orbit;
import org.orekit.orbits.PositionAngle;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.analytical.KeplerianPropagator;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
import org.orekit.utils.AngularDerivativesFilter;
import org.orekit.utils.Constants;
import org.orekit.utils.IERSConventions;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.TimeStampedAngularCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
/**
* Orbit Model class to generate positions-velocities and attitude quaternions.
* <p>
* the aim of this class is to simulate the orbit model of an LEO satellite
* </p>
* @author Jonathan Guinet
* @author Guylaine Prat
* @since 2.0
*/
public class OrbitModel {
/** Flag to change Attitude Law (by default Nadir Pointing Yaw Compensation). */
private boolean userDefinedLOFTransform;
/** User defined Roll law. */
private double[] lofTransformRollPoly;
/** User defined Pitch law. */
private double[] lofTransformPitchPoly;
/** User defined Yaw law. */
private double[] lofTransformYawPoly;
/** Reference date. */
private AbsoluteDate refDate;
/** Default constructor.
*/
public OrbitModel() {
userDefinedLOFTransform = false;
}
/** Generate satellite ephemeris.
*/
public static void addSatellitePV(final TimeScale gps, final Frame eme2000, final Frame itrf,
final List<TimeStampedPVCoordinates> satellitePVList,
final String absDate,
final double px, final double py, final double pz,
final double vx, final double vy, final double vz) {
final AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
final Vector3D position = new Vector3D(px, py, pz);
final Vector3D velocity = new Vector3D(vx, vy, vz);
final PVCoordinates pvITRF = new PVCoordinates(position, velocity);
final Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
final Vector3D pEME2000 = transform.transformPosition(pvITRF.getPosition());
final Vector3D vEME2000 = transform.transformVector(pvITRF.getVelocity());
satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pEME2000, vEME2000, Vector3D.ZERO));
}
/** Generate satellite attitude.
*/
public void addSatelliteQ(final TimeScale gps,
final List<TimeStampedAngularCoordinates> satelliteQList,
final String absDate,
final double q0, final double q1, final double q2, final double q3) {
final AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
final Rotation rotation = new Rotation(q0, q1, q2, q3, true);
final TimeStampedAngularCoordinates pair =
new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
satelliteQList.add(pair);
}
/** Create an Earth.
* @return the Earth as the WGS84 ellipsoid
*/
public BodyShape createEarth() {
return new OneAxisEllipsoid(Constants.WGS84_EARTH_EQUATORIAL_RADIUS,
Constants.WGS84_EARTH_FLATTENING,
FramesFactory.getITRF(IERSConventions.IERS_2010, true));
}
/** Created a gravity field.
* @return normalized spherical harmonics coefficients
*/
public NormalizedSphericalHarmonicsProvider createGravityField() {
return GravityFieldFactory.getNormalizedProvider(12, 12);
}
/** Create an orbit at a chosen date.
* @param mu Earth gravitational constant
* @return the orbit
*/
public Orbit createOrbit(final double mu, final AbsoluteDate date) {
// the following orbital parameters have been computed using
// Orekit tutorial about phasing, using the following configuration:
//
// orbit.date = 2012-01-01T00:00:00.000
// phasing.orbits.number = 143
// phasing.days.number = 10
// sun.synchronous.reference.latitude = 0
// sun.synchronous.reference.ascending = false
// sun.synchronous.mean.solar.time = 10:30:00
// gravity.field.degree = 12
// gravity.field.order = 12
final Frame eme2000 = FramesFactory.getEME2000();
return new CircularOrbit(694000.0 + Constants.WGS84_EARTH_EQUATORIAL_RADIUS,
-4.029194321683225E-4,
0.0013530362644647786,
FastMath.toRadians(98.2), // Pleiades inclination 98.2 deg
FastMath.toRadians(-86.47 + 180),
FastMath.toRadians(135.9 + 0.3),
PositionAngle.TRUE,
eme2000,
date,
mu);
}
/** Set the Local Orbital Frame characteristics.
*/
public void setLOFTransform(final double[] rollPoly, final double[] pitchPoly,
final double[] yawPoly, final AbsoluteDate date) {
this.userDefinedLOFTransform = true;
lofTransformRollPoly = rollPoly.clone();
lofTransformPitchPoly = pitchPoly.clone();
lofTransformYawPoly = yawPoly.clone();
this.refDate = date;
}
/** Recompute the polynom coefficients with shift.
*/
private double getPoly(final double[] poly, final double shift) {
double val = 0.0;
for (int coef = 0; coef < poly.length; coef++) {
val = val + poly[coef] * FastMath.pow(shift, coef);
}
return val;
}
/** Get the offset.
*/
private Rotation getOffset(final BodyShape earth, final Orbit orbit, final double shift){
final LOFType type = LOFType.VVLH;
final double roll = getPoly(lofTransformRollPoly, shift);
final double pitch = getPoly(lofTransformPitchPoly, shift);
final double yaw = getPoly(lofTransformYawPoly, shift);
final LofOffset law = new LofOffset(orbit.getFrame(), type, RotationOrder.XYZ,
roll, pitch, yaw);
final Rotation offsetAtt = law.
getAttitude(orbit, orbit.getDate().shiftedBy(shift), orbit.getFrame()).
getRotation();
final NadirPointing nadirPointing = new NadirPointing(orbit.getFrame(), earth);
final Rotation nadirAtt = nadirPointing.
getAttitude(orbit, orbit.getDate().getDate().shiftedBy(shift), orbit.getFrame()).
getRotation();
final Rotation offsetProper = offsetAtt.compose(nadirAtt.revert(), RotationConvention.VECTOR_OPERATOR);
return offsetProper;
}
/** Create the attitude provider.
*/
public AttitudeProvider createAttitudeProvider(final BodyShape earth, final Orbit orbit) {
if (userDefinedLOFTransform) {
final LOFType type = LOFType.VVLH;
final List<TimeStampedAngularCoordinates> list = new ArrayList<TimeStampedAngularCoordinates>();
for (double shift = -10.0; shift < +10.0; shift += 1e-2) {
list.add(new TimeStampedAngularCoordinates(refDate
.shiftedBy(shift), getOffset(earth, orbit, shift),
Vector3D.ZERO,
Vector3D.ZERO));
}
final TabulatedLofOffset tabulated = new TabulatedLofOffset(orbit.getFrame(), type, list,
2, AngularDerivativesFilter.USE_R);
return tabulated;
} else {
return new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth));
}
}
/** Generate the orbit.
*/
public List<TimeStampedPVCoordinates> orbitToPV(final Orbit orbit, final BodyShape earth,
final AbsoluteDate minDate, final AbsoluteDate maxDate,
final double step) {
final Propagator propagator = new KeplerianPropagator(orbit);
propagator.setAttitudeProvider(createAttitudeProvider(earth, orbit));
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
propagator.getMultiplexer().add(step,
currentState ->
list.add(new TimeStampedPVCoordinates(currentState.getDate(),
currentState.getPVCoordinates().getPosition(),
currentState.getPVCoordinates().getVelocity(),
Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
/** Generate the attitude.
*/
public List<TimeStampedAngularCoordinates> orbitToQ(final Orbit orbit, final BodyShape earth,
final AbsoluteDate minDate, final AbsoluteDate maxDate,
final double step) {
final Propagator propagator = new KeplerianPropagator(orbit);
propagator.setAttitudeProvider(createAttitudeProvider(earth, orbit));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<>();
propagator.getMultiplexer().add(step,
currentState ->
list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
currentState.getAttitude().getRotation(),
Vector3D.ZERO,
Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
}