Package | Description |
---|---|
org.orekit.estimation.iod |
This package provides initial orbit determination methods.
|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.estimation.measurements.generation |
This package provides Orbit Determination measurements generation.
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
IodGooding.estimate(Frame frame,
AngularRaDec raDec1,
AngularRaDec raDec2,
AngularRaDec raDec3,
double rho1init,
double rho3init)
Orbit got from three angular observations.
|
KeplerianOrbit |
IodGooding.estimate(Frame frame,
AngularRaDec raDec1,
AngularRaDec raDec2,
AngularRaDec raDec3,
double rho1init,
double rho3init,
int nRev,
boolean direction)
Orbit got from three angular observations.
|
CartesianOrbit |
IodLaplace.estimate(Frame frame,
PVCoordinates obsPva,
AngularRaDec raDec1,
AngularRaDec raDec2,
AngularRaDec raDec3)
Estimate the orbit from three angular observations at the same location.
|
static Vector3D |
IodGooding.lineOfSight(AngularRaDec raDec)
Calculate the line of sight vector from an AngularRaDec measurement.
|
static Vector3D |
IodLaplace.lineOfSight(AngularRaDec raDec)
Calculate the line of sight vector from an AngularRaDec measurement.
|
Modifier and Type | Method and Description |
---|---|
protected EstimatedMeasurement<AngularRaDec> |
AngularRaDec.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
Modifier and Type | Method and Description |
---|---|
AngularRaDec |
AngularRaDecBuilder.build(SpacecraftState[] states)
Generate a single measurement.
|
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