|
Kalman model/estimator usage suggestions
|
|
10
|
221
|
November 18, 2020
|
|
Map Latitud, Longitud and altitud, help
|
|
4
|
104
|
November 18, 2020
|
|
Orbital Elements of a Sun Synchronous Orbit
|
|
2
|
104
|
November 18, 2020
|
|
EcksteinHechler Propagator Exception
|
|
1
|
85
|
November 17, 2020
|
|
Ambiguity resolving
|
|
2
|
112
|
November 16, 2020
|
|
Station to satellite distance
|
|
2
|
81
|
November 16, 2020
|
|
ImpulseManeuver on PositionAngle with Python wrapper
|
|
6
|
116
|
November 13, 2020
|
|
Measurement types for estimation
|
|
2
|
91
|
November 12, 2020
|
|
GNSS attitude by GenericGNSS
|
|
3
|
129
|
November 5, 2020
|
|
Prime meridian angle
|
|
1
|
63
|
November 5, 2020
|
|
InvalidArgError for addNewSegment into OrekitEphemerisFile.OrekitSatelliteEphemeris
|
|
1
|
74
|
November 2, 2020
|
|
Simulating topocentric right ascension/declination measurements
|
|
26
|
339
|
October 30, 2020
|
|
Access to AngularAzEl values
|
|
4
|
78
|
October 30, 2020
|
|
Endless loop in a multi-handler case
|
|
13
|
245
|
October 27, 2020
|
|
Transforming Angles
|
|
6
|
386
|
October 22, 2020
|
|
Help with local orbital frames
|
|
4
|
138
|
October 21, 2020
|
|
Ephemeris based estimation
|
|
2
|
83
|
October 21, 2020
|
|
Satellite clock offset
|
|
8
|
218
|
October 15, 2020
|
|
Problem with CCSDS Export
|
|
3
|
139
|
October 14, 2020
|
|
TLE file to azimuth and elevation
|
|
3
|
137
|
October 14, 2020
|
|
Java Propagator Parallelizer
|
|
6
|
193
|
October 14, 2020
|
|
PVCoordinatesProvider in OneWayGNSSPhase
|
|
4
|
84
|
October 14, 2020
|
|
PropagatorsParallelizer
|
|
11
|
453
|
October 13, 2020
|
|
Error in Orekit-Python Examples
|
|
3
|
154
|
October 9, 2020
|
|
Covariance matrix frame
|
|
2
|
138
|
October 9, 2020
|
|
Electric Thrust to GEO
|
|
1
|
129
|
October 9, 2020
|
|
Loading Earth Orientation Parameters from finals files
|
|
2
|
94
|
October 1, 2020
|
|
Issue with DSST propagator setup
|
|
7
|
154
|
September 28, 2020
|
|
Performance of numerical propagator with hundreds of finite maneuvers in sequence
|
|
3
|
135
|
September 28, 2020
|
|
DSST orbit determination with osculating propagation fails depending on initial epoch
|
|
3
|
100
|
September 25, 2020
|
