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Commit b33c9371 authored by noeljanes's avatar noeljanes
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HELLO

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src/main/java/fr/cs/examples/estimation/MeasurementsGeneration.java
+ 6
− 5
View file @ b33c9371
...@@ -146,7 +146,7 @@ public class MeasurementsGeneration { ...@@ -146,7 +146,7 @@ public class MeasurementsGeneration {
FastMath.toRadians(23.739), FastMath.toRadians(23.739),
119); 119);
final GroundStation station = new GroundStation(new TopocentricFrame(earth, location, "Apomahon")); final GroundStation station = new GroundStation(new TopocentricFrame(earth, location, "Apomahon"));
/*
final GeodeticPoint location = new GeodeticPoint(FastMath.toRadians(48.644), final GeodeticPoint location = new GeodeticPoint(FastMath.toRadians(48.644),
FastMath.toRadians(2.231), FastMath.toRadians(2.231),
110); 110);
...@@ -157,6 +157,7 @@ public class MeasurementsGeneration { ...@@ -157,6 +157,7 @@ public class MeasurementsGeneration {
401); 401);
final GroundStation station = new GroundStation(new TopocentricFrame(earth, location, "Kir-virt")); final GroundStation station = new GroundStation(new TopocentricFrame(earth, location, "Kir-virt"));
final GeodeticPoint location = new GeodeticPoint(FastMath.toRadians(43.562), final GeodeticPoint location = new GeodeticPoint(FastMath.toRadians(43.562),
FastMath.toRadians(1.469), FastMath.toRadians(1.469),
180); 180);
...@@ -167,7 +168,7 @@ public class MeasurementsGeneration { ...@@ -167,7 +168,7 @@ public class MeasurementsGeneration {
final double minElevation = FastMath.toRadians(1.0); final double minElevation = FastMath.toRadians(1.0);
final double timeStep = 5.0; final double timeStep = 5.0;
final TimeScale utc = TimeScalesFactory.getUTC(); final TimeScale utc = TimeScalesFactory.getUTC();
final AbsoluteDate t0 = new AbsoluteDate("2019-08-15T00:00:00.000", utc); final AbsoluteDate t0 = new AbsoluteDate("2019-08-13T00:00:00.000", utc);
final double duration = Constants.JULIAN_DAY; // Sets the duration to be the length of a Julian day final double duration = Constants.JULIAN_DAY; // Sets the duration to be the length of a Julian day
...@@ -182,10 +183,10 @@ public class MeasurementsGeneration { ...@@ -182,10 +183,10 @@ public class MeasurementsGeneration {
// this orbit is a dummy one, close to the first results from orbit determination from Max Valier satellite // this orbit is a dummy one, close to the first results from orbit determination from Max Valier satellite
final NormalizedSphericalHarmonicsProvider gravity = GravityFieldFactory.getNormalizedProvider(12, 12); final NormalizedSphericalHarmonicsProvider gravity = GravityFieldFactory.getNormalizedProvider(12, 12);
final AbsoluteDate tOrb = new AbsoluteDate("2019-08-15T13:55:04.172", utc); final AbsoluteDate tOrb = new AbsoluteDate("2019-08-12T03:52:20.580", utc);
final TimeStampedPVCoordinates pvt = new TimeStampedPVCoordinates(tOrb, final TimeStampedPVCoordinates pvt = new TimeStampedPVCoordinates(tOrb,
new Vector3D(1630586.0137295902, -6689236.123644499, 4656.431019124808), new Vector3D(1234146.2433587196, -6761913.188732109, -7188.547472578492),
new Vector3D(-930.7917732051654, -202.65450696096696, 7548.237934477402)); new Vector3D(-943.7363307457433, -169.23351996424876, 7560.364453528402));
final CartesianOrbit orbit = new CartesianOrbit(pvt, FramesFactory.getEME2000(), gravity.getMu()); final CartesianOrbit orbit = new CartesianOrbit(pvt, FramesFactory.getEME2000(), gravity.getMu());
final OrbitType type = OrbitType.CARTESIAN; final OrbitType type = OrbitType.CARTESIAN;
......
src/main/java/fr/cs/examples/estimation/OrbitDetermination.java
+ 60
− 42
View file @ b33c9371
...@@ -146,48 +146,66 @@ public class OrbitDetermination { // Class 1 ...@@ -146,48 +146,66 @@ public class OrbitDetermination { // Class 1
* @param args program arguments (unused here) * @param args program arguments (unused here)
*/ */
public static void main(String[] args) { public static void main(String[] args) {
try { // configure Orekit
File home = new File(System.getProperty("user.home"));
// configure Orekit File orekitData = new File(home, "orekit-data");
File home = new File(System.getProperty("user.home")); if (!orekitData.exists()) {
File orekitData = new File(home, "orekit-data"); System.err.format(Locale.US, "Failed to find %s folder%n",
if (!orekitData.exists()) { orekitData.getAbsolutePath());
System.err.format(Locale.US, "Failed to find %s folder%n", System.err.format(Locale.US, "You need to download %s from %s, unzip it in %s and rename it 'orekit-data' for this tutorial to work%n",
orekitData.getAbsolutePath()); "orekit-data-master.zip", "https://gitlab.orekit.org/orekit/orekit-data/-/archive/master/orekit-data-master.zip",
System.err.format(Locale.US, "You need to download %s from %s, unzip it in %s and rename it 'orekit-data' for this tutorial to work%n", home.getAbsolutePath());
"orekit-data-master.zip", "https://gitlab.orekit.org/orekit/orekit-data/-/archive/master/orekit-data-master.zip",
home.getAbsolutePath());
System.exit(1);
}
DataProvidersManager manager = DataProvidersManager.getInstance();
manager.addProvider(new DirectoryCrawler(orekitData));
// input in tutorial resources directory/output (in user's home directory)
final String inputPath = OrbitDetermination.class.getClassLoader().getResource("maxvalier.in").toURI().getPath(); // Brings in input file with orbit data
final File input = new File(inputPath);
long t0 = System.currentTimeMillis(); // Returns current time in milliseconds
new OrbitDetermination().run(input, home);
long t1 = System.currentTimeMillis();
System.out.println("wall clock run time (s): " + (0.001 * (t1 - t0)));
} catch (URISyntaxException urise) {
System.err.println(urise.getLocalizedMessage());
System.exit(1);
} catch (IOException ioe) {
System.err.println(ioe.getLocalizedMessage());
System.exit(1);
} catch (IllegalArgumentException iae) {
iae.printStackTrace(System.err);
System.err.println(iae.getLocalizedMessage());
System.exit(1);
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
} catch (ParseException pe) {
System.err.println(pe.getLocalizedMessage());
System.exit(1); System.exit(1);
} }
DataProvidersManager manager = DataProvidersManager.getInstance();
manager.addProvider(new DirectoryCrawler(orekitData));
File inputs = new File(home, "Documents\\ESA Socis\\Orbit Determination\\orbitdetermination\\satnogs-orbit-determination\\src\\main\\resources\\Generated-Measurements\\13-8");
String[] folderlist = inputs.list();
//boolean exists = inputs.exists();
//System.out.println(exists);
for(String inputfolders : folderlist) {
System.out.println(inputfolders);
final File filelistF = new File(inputs + "\\" + inputfolders);
String[] filelist = filelistF.list();
for (String inputfile : filelist) {
System.out.println(inputfile);
if (inputfile.endsWith(".in")) {
System.out.println(inputfile);
try {
// input in tutorial resources directory/output (in user's home directory)
//final String inputPath = OrbitDetermination.class.getClassLoader().getResource("maxvalier.in").toURI().getPath(); // Brings in input file with orbit data
//final File input = new File(inputPath);
//final File input = new File(inputPath);
final File input = new File(inputs + "\\" + inputfolders + "\\" + inputfile);
long t0 = System.currentTimeMillis(); // Returns current time in milliseconds
new OrbitDetermination().run(input, home);
long t1 = System.currentTimeMillis();
System.out.println("wall clock run time (s): " + (0.001 * (t1 - t0)));
} //catch (URISyntaxException urise) {
//System.err.println(urise.getLocalizedMessage());
//System.exit(1);
catch (IOException ioe) {
System.err.println(ioe.getLocalizedMessage());
System.exit(1);
} catch (IllegalArgumentException iae) {
iae.printStackTrace(System.err);
System.err.println(iae.getLocalizedMessage());
System.exit(1);
} catch (OrekitException oe) {
System.err.println(oe.getLocalizedMessage());
System.exit(1);
} catch (ParseException pe) {
System.err.println(pe.getLocalizedMessage());
System.exit(1);
}
}
}
}
} }
private void run(final File input, final File home) // Starts an initial guess and then propagates that private void run(final File input, final File home) // Starts an initial guess and then propagates that
...@@ -205,7 +223,7 @@ public class OrbitDetermination { // Class 1 ...@@ -205,7 +223,7 @@ public class OrbitDetermination { // Class 1
if (parser.containsKey(ParameterKey.OUTPUT_BASE_NAME) && if (parser.containsKey(ParameterKey.OUTPUT_BASE_NAME) &&
parser.getString(ParameterKey.OUTPUT_BASE_NAME).length() > 0) { parser.getString(ParameterKey.OUTPUT_BASE_NAME).length() > 0) {
baseName = parser.getString(ParameterKey.OUTPUT_BASE_NAME); baseName = parser.getString(ParameterKey.OUTPUT_BASE_NAME);
logStream = new PrintStream(new File(home, baseName + "-log.out"), "UTF-8"); logStream = new PrintStream(new File(home, "\\Documents\\ESA Socis\\Orbit Determination\\Python plotting\\20190813\\"+ baseName + "-log.out"), "UTF-8");
} else { } else {
baseName = null; baseName = null;
logStream = null; logStream = null;
...@@ -1970,7 +1988,7 @@ public class OrbitDetermination { // Class 1 ...@@ -1970,7 +1988,7 @@ public class OrbitDetermination { // Class 1
this.file = null; this.file = null;
this.stream = null; this.stream = null;
} else { } else {
this.file = new File(home, baseName + "-" + name + "-residuals.out"); this.file = new File(home, "\\Documents\\ESA Socis\\Orbit Determination\\Python plotting\\20190813\\" + baseName + "-" + name + "-residuals.out");
this.stream = new PrintStream(file, "UTF-8"); this.stream = new PrintStream(file, "UTF-8");
} }
} }
......
src/main/resources/2019-08-13T18_00_54_145.961_4171_42778.dat deleted 100644 → 0
+ 0
− 173
View file @ b3ffd4eb
2019-08-13T17:58:24.355 RANGE_RATE 39-CGBSAT-VHF-P1 -2.834483183864183
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2019-08-13T17:58:27.466 RANGE_RATE 39-CGBSAT-VHF-P1 -2.793403717431369
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2019-08-13T18:02:27.226 RANGE_RATE 39-CGBSAT-VHF-P1 2.6701653181329257
2019-08-13T18:02:28.262 RANGE_RATE 39-CGBSAT-VHF-P1 2.7112447845657397
2019-08-13T18:02:29.299 RANGE_RATE 39-CGBSAT-VHF-P1 2.7112447845657397
2019-08-13T18:02:30.336 RANGE_RATE 39-CGBSAT-VHF-P1 2.7523242509985546
2019-08-13T18:02:31.286 RANGE_RATE 39-CGBSAT-VHF-P1 2.7523242509985546
2019-08-13T18:02:33.360 RANGE_RATE 39-CGBSAT-VHF-P1 2.793403717431369
2019-08-13T18:02:34.310 RANGE_RATE 39-CGBSAT-VHF-P1 2.834483183864183
2019-08-13T18:02:35.347 RANGE_RATE 39-CGBSAT-VHF-P1 2.834483183864183
2019-08-13T18:02:36.384 RANGE_RATE 39-CGBSAT-VHF-P1 2.875562650296997
2019-08-13T18:02:37.334 RANGE_RATE 39-CGBSAT-VHF-P1 2.9166421167298116
2019-08-13T18:02:38.371 RANGE_RATE 39-CGBSAT-VHF-P1 2.9166421167298116
2019-08-13T18:02:39.408 RANGE_RATE 39-CGBSAT-VHF-P1 2.957721583162626
2019-08-13T18:02:40.358 RANGE_RATE 39-CGBSAT-VHF-P1 2.957721583162626
2019-08-13T18:02:41.309 RANGE_RATE 39-CGBSAT-VHF-P1 2.957721583162626
2019-08-13T18:02:42.432 RANGE_RATE 39-CGBSAT-VHF-P1 2.99880104959544
2019-08-13T18:02:43.382 RANGE_RATE 39-CGBSAT-VHF-P1 2.99880104959544
2019-08-13T18:02:46.406 RANGE_RATE 39-CGBSAT-VHF-P1 3.0809599824610685
2019-08-13T18:02:47.357 RANGE_RATE 39-CGBSAT-VHF-P1 3.0809599824610685
2019-08-13T18:02:50.381 RANGE_RATE 39-CGBSAT-VHF-P1 3.163118915326697
2019-08-13T18:02:51.418 RANGE_RATE 39-CGBSAT-VHF-P1 3.163118915326697
2019-08-13T18:02:52.454 RANGE_RATE 39-CGBSAT-VHF-P1 3.204198381759511
2019-08-13T18:02:54.442 RANGE_RATE 39-CGBSAT-VHF-P1 3.2452778481923255
2019-08-13T18:02:55.392 RANGE_RATE 39-CGBSAT-VHF-P1 3.2452778481923255
2019-08-13T18:02:56.429 RANGE_RATE 39-CGBSAT-VHF-P1 3.2863573146251395
2019-08-13T18:02:57.466 RANGE_RATE 39-CGBSAT-VHF-P1 3.327436781057954
2019-08-13T18:02:58.502 RANGE_RATE 39-CGBSAT-VHF-P1 3.327436781057954
2019-08-13T18:02:59.453 RANGE_RATE 39-CGBSAT-VHF-P1 3.327436781057954
2019-08-13T18:03:00.490 RANGE_RATE 39-CGBSAT-VHF-P1 3.368516247490768
2019-08-13T18:03:01.526 RANGE_RATE 39-CGBSAT-VHF-P1 3.368516247490768
2019-08-13T18:03:02.477 RANGE_RATE 39-CGBSAT-VHF-P1 3.4095957139235824
2019-08-13T18:03:03.514 RANGE_RATE 39-CGBSAT-VHF-P1 3.4095957139235824
2019-08-13T18:03:05.501 RANGE_RATE 39-CGBSAT-VHF-P1 3.4506751803563964
2019-08-13T18:03:06.538 RANGE_RATE 39-CGBSAT-VHF-P1 3.491754646789211
2019-08-13T18:03:07.574 RANGE_RATE 39-CGBSAT-VHF-P1 3.491754646789211
2019-08-13T18:03:08.525 RANGE_RATE 39-CGBSAT-VHF-P1 3.491754646789211
2019-08-13T18:03:09.562 RANGE_RATE 39-CGBSAT-VHF-P1 3.532834113222025
2019-08-13T18:03:10.598 RANGE_RATE 39-CGBSAT-VHF-P1 3.532834113222025
2019-08-13T18:03:11.549 RANGE_RATE 39-CGBSAT-VHF-P1 3.5739135796548394
2019-08-13T18:03:12.499 RANGE_RATE 39-CGBSAT-VHF-P1 3.5739135796548394
2019-08-13T18:03:13.622 RANGE_RATE 39-CGBSAT-VHF-P1 3.6149930460876534
2019-08-13T18:03:14.573 RANGE_RATE 39-CGBSAT-VHF-P1 3.6149930460876534
2019-08-13T18:03:15.523 RANGE_RATE 39-CGBSAT-VHF-P1 3.656072512520468
2019-08-13T18:03:16.560 RANGE_RATE 39-CGBSAT-VHF-P1 3.656072512520468
2019-08-13T18:03:17.597 RANGE_RATE 39-CGBSAT-VHF-P1 3.656072512520468
2019-08-13T18:03:18.547 RANGE_RATE 39-CGBSAT-VHF-P1 3.697151978953282
2019-08-13T18:03:19.584 RANGE_RATE 39-CGBSAT-VHF-P1 3.697151978953282
2019-08-13T18:03:25.632 RANGE_RATE 39-CGBSAT-VHF-P1 3.8203903782517243
2019-08-13T18:03:30.816 RANGE_RATE 39-CGBSAT-VHF-P1 3.9025493111173537
2019-08-13T18:04:02.006 RANGE_RATE 39-CGBSAT-VHF-P1 4.395502908311124
2019-08-13T18:04:08.141 RANGE_RATE 39-CGBSAT-VHF-P1 4.477661841176753
src/main/resources/2019-08-13T19_33_33_145.961_4171_42778.dat deleted 100644 → 0
+ 0
− 370
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src/main/resources/2019-08-13T21_07_21_145.961_4171_42778.dat deleted 100644 → 0
+ 0
− 401
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src/main/resources/2019-08-13T22_42_22_145.961_4171_42778.dat deleted 100644 → 0
+ 0
− 2
View file @ b3ffd4eb
2019-08-13T22:41:56.774 RANGE_RATE 39-CGBSAT-VHF-P4 -0.0
2019-08-13T22:42:02.822 RANGE_RATE 39-CGBSAT-VHF-P4 0.12323839929844274
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