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SatNOGS Orbit Determination
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SatNOGS Orbit Determination
Commits
eb4d7c92
Commit
eb4d7c92
authored
5 years ago
by
noeljanes
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Added config parameters for estimated cd
parent
82771635
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src/main/java/fr/cs/examples/estimation/OrbitDetermination.java
+13
-0
13 additions, 0 deletions
...in/java/fr/cs/examples/estimation/OrbitDetermination.java
src/main/resources/maxvalier.in
+6
-3
6 additions, 3 deletions
src/main/resources/maxvalier.in
with
19 additions
and
3 deletions
src/main/java/fr/cs/examples/estimation/OrbitDetermination.java
+
13
−
0
View file @
eb4d7c92
...
...
@@ -619,6 +619,7 @@ public class OrbitDetermination { // Class 1
final
double
area
=
parser
.
getDouble
(
ParameterKey
.
DRAG_AREA
);
final
boolean
cdEstimated
=
parser
.
getBoolean
(
ParameterKey
.
DRAG_CD_ESTIMATED
);
System
.
out
.
println
(
cd
);
System
.
out
.
println
(
parser
.
getDouble
(
ParameterKey
.
DRAG_CD_MAX
));
MarshallSolarActivityFutureEstimation
msafe
=
new
MarshallSolarActivityFutureEstimation
(
MarshallSolarActivityFutureEstimation
.
DEFAULT_SUPPORTED_NAMES
,
MarshallSolarActivityFutureEstimation
.
StrengthLevel
.
AVERAGE
);
...
...
@@ -627,13 +628,23 @@ public class OrbitDetermination { // Class 1
//Atmosphere atmosphere = new DTM2000(msafe, CelestialBodyFactory.getSun(), body);
Atmosphere
atmosphere
=
new
NRLMSISE00
(
msafe
,
CelestialBodyFactory
.
getSun
(),
body
);
propagatorBuilder
.
addForceModel
(
new
DragForce
(
atmosphere
,
new
IsotropicDrag
(
area
,
cd
)));
if
(
cdEstimated
)
{
for
(
final
ParameterDriver
driver
:
propagatorBuilder
.
getPropagationParametersDrivers
().
getDrivers
())
{
if
(
driver
.
getName
().
equals
(
DragSensitive
.
DRAG_COEFFICIENT
))
{
driver
.
setSelected
(
true
);
}
if
(
parser
.
containsKey
(
ParameterKey
.
DRAG_CD_MIN
))
{
driver
.
setMinValue
(
parser
.
getDouble
(
ParameterKey
.
DRAG_CD_MIN
));
}
if
(
parser
.
containsKey
(
ParameterKey
.
DRAG_CD_MAX
))
{
driver
.
setMinValue
(
parser
.
getDouble
(
ParameterKey
.
DRAG_CD_MAX
));
}
}
}
}
// solar radiation pressure
...
...
@@ -2240,6 +2251,8 @@ public class OrbitDetermination { // Class 1
DRAG_CD
,
DRAG_CD_ESTIMATED
,
DRAG_AREA
,
DRAG_CD_MIN
,
DRAG_CD_MAX
,
SOLAR_RADIATION_PRESSURE
,
SOLAR_RADIATION_PRESSURE_CR
,
SOLAR_RADIATION_PRESSURE_CR_ESTIMATED
,
...
...
This diff is collapsed.
Click to expand it.
src/main/resources/maxvalier.in
+
6
−
3
View file @
eb4d7c92
...
...
@@ -133,6 +133,9 @@ drag.cd = 2
drag.cd.estimated = true
## Drag area (m^2)
drag.area = 0.25
## Maximum and minimum values of the drag coefficient
drag.cd.min = 0
drag.cd.max = 20
## Solar Radiation Pressure (true/false) [false]
solar.radiation.pressure = false
...
...
@@ -588,11 +591,11 @@ estimator.max.iterations = 600
estimator.max.evaluations = 600
# comma-separated list of measurements files (in the same directory as this file)
measurements.files =
generated-doppler-39-CGBSAT-VHF
.dat
measurements.files =
2019-06-11T19_58_49_145.961_4171_42778
.dat
# generated-doppler-F4KLD-UNIVERSITE-PAUL-SABATIER-Toulouse-III.dat
#
#
generated-doppler-39-CGBSAT-VHF.dat
# generated-doppler-39-CGBSAT-VHF-fixeddrag.dat
# generated-doppler-Marcs.dat
# generated-doppler-ZL1WJQ.dat
...
...
@@ -619,7 +622,7 @@ measurements.files = generated-doppler-39-CGBSAT-VHF.dat
#Measured Data
# 2019-06-12T07_20_42_145.961_4171_42778.dat
#
2019-06-11T19_58_49_145.961_4171_42778.dat
, 2019-06-11T21_32_55_145.961_4171_42778.dat
# , 2019-06-11T21_32_55_145.961_4171_42778.dat
#
# base name of the output files (log and residuals), no files created if empty
...
...
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