Package | Description |
---|---|
org.orekit.estimation.iod |
This package provides initial orbit determination methods.
|
org.orekit.files.ccsds.ndm.odm.opm |
This package contains class managing CCSDS Orbit Parameter Message.
|
org.orekit.orbits |
This package provides classes to represent orbits.
|
org.orekit.propagation.analytical |
Top level package for analytical propagators.
|
Modifier and Type | Method and Description |
---|---|
CartesianOrbit |
IodLaplace.estimate(Frame frame,
PVCoordinates obsPva,
AbsoluteDate obsDate1,
Vector3D los1,
AbsoluteDate obsDate2,
Vector3D los2,
AbsoluteDate obsDate3,
Vector3D los3)
Estimate orbit from three line of sight angles from the same location.
|
CartesianOrbit |
IodLaplace.estimate(Frame frame,
PVCoordinates obsPva,
AngularRaDec raDec1,
AngularRaDec raDec2,
AngularRaDec raDec3)
Estimate the orbit from three angular observations at the same location.
|
Modifier and Type | Method and Description |
---|---|
CartesianOrbit |
Opm.generateCartesianOrbit()
Generate a Cartesian orbit.
|
Modifier and Type | Method and Description |
---|---|
CartesianOrbit |
CartesianOrbit.interpolate(AbsoluteDate date,
Stream<Orbit> sample)
Get an interpolated instance.
|
CartesianOrbit |
CartesianOrbit.shiftedBy(double dt)
Get a time-shifted orbit.
|
CartesianOrbit |
FieldCartesianOrbit.toOrbit() |
Modifier and Type | Method and Description |
---|---|
CartesianOrbit |
EcksteinHechlerPropagator.propagateOrbit(AbsoluteDate date)
Extrapolate an orbit up to a specific target date.
|
Copyright © 2002-2022 CS GROUP. All rights reserved.