Package | Description |
---|---|
org.orekit.estimation.iod | |
org.orekit.files.ccsds |
This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
|
org.orekit.orbits |
This package provides classes to represent orbits.
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
IodLambert.estimate(Frame frame,
boolean posigrade,
int nRev,
Vector3D p1,
AbsoluteDate t1,
Vector3D p2,
AbsoluteDate t2)
Estimate a Keplerian orbit given two position vectors and a duration.
|
KeplerianOrbit |
IodGibbs.estimate(Frame frame,
PV pv1,
PV pv2,
PV pv3)
Give an initial orbit estimation, assuming Keplerian motion.
|
KeplerianOrbit |
IodGibbs.estimate(Frame frame,
Vector3D r1,
AbsoluteDate date1,
Vector3D r2,
AbsoluteDate date2,
Vector3D r3,
AbsoluteDate date3)
Give an initial orbit estimation, assuming Keplerian motion.
|
KeplerianOrbit |
IodGooding.estimate(Vector3D O1,
Vector3D O2,
Vector3D O3,
Vector3D lineOfSight1,
AbsoluteDate dateObs1,
Vector3D lineOfSight2,
AbsoluteDate dateObs2,
Vector3D lineOfSight3,
AbsoluteDate dateObs3,
double rho1init,
double rho3init)
Orbit got from Observed Three Lines of Sight (angles only).
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
OPMFile.generateKeplerianOrbit()
Generate a
KeplerianOrbit from the OPM Keplerian elements if hasKeplerianElements is true,
or from the state vector data otherwise. |
KeplerianOrbit |
OMMFile.generateKeplerianOrbit()
Generate a
KeplerianOrbit based on the OMM mean Keplerian elements. |
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
KeplerianOrbit.interpolate(AbsoluteDate date,
Stream<Orbit> sample)
Get an interpolated instance.
|
KeplerianOrbit |
KeplerianOrbit.shiftedBy(double dt)
Get a time-shifted orbit.
|
KeplerianOrbit |
FieldKeplerianOrbit.toOrbit() |
Copyright © 2002-2019 CS Systèmes d'information. All rights reserved.