|
||||||||||
PREV NEXT | FRAMES NO FRAMES |
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela |
---|
Constructors in fr.cnes.sirius.patrius.stela with parameters of type OrbitNatureConverter | |
---|---|
PerigeeAltitudeDetector(double maxCheck,
double threshold,
double altitudeIn,
double earthRadiusIn,
OrbitNatureConverter orbitConverterIn)
Build a new altitude detector, with osculating perigee. |
|
PerigeeAltitudeDetector(double maxCheck,
double threshold,
double altitudeIn,
double earthRadiusIn,
OrbitNatureConverter orbitConverterIn,
EventDetector.Action ascending,
EventDetector.Action descending)
Build a new altitude detector, with osculating perigee. |
|
PerigeeAltitudeDetector(double maxCheck,
double threshold,
double altitudeIn,
double earthRadiusIn,
OrbitNatureConverter orbitConverterIn,
EventDetector.Action ascending,
EventDetector.Action descending,
boolean removeAscending,
boolean removeDescending)
Build a new altitude detector, with osculating perigee. |
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces |
---|
Methods in fr.cnes.sirius.patrius.stela.forces with parameters of type OrbitNatureConverter | |
---|---|
abstract double[] |
AbstractStelaGaussContribution.computePerturbation(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
Compute the dE/dt force derivatives for a given spacecraft state. |
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.drag |
---|
Methods in fr.cnes.sirius.patrius.stela.forces.drag with parameters of type OrbitNatureConverter | |
---|---|
double[] |
StelaAtmosphericDrag.computePerturbation(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
|
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.noninertial |
---|
Methods in fr.cnes.sirius.patrius.stela.forces.noninertial with parameters of type OrbitNatureConverter | |
---|---|
double[] |
NonInertialContribution.computePerturbation(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
|
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.radiation |
---|
Methods in fr.cnes.sirius.patrius.stela.forces.radiation with parameters of type OrbitNatureConverter | |
---|---|
double[] |
SRPSquaring.computePerturbation(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
Compute the dE/dt force derivatives for a given spacecraft state. |
double[] |
StelaSRPSquaring.computePerturbation(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
Compute the dE/dt force derivatives for a given spacecraft state. |
Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.propagation |
---|
Methods in fr.cnes.sirius.patrius.stela.propagation that return OrbitNatureConverter | |
---|---|
OrbitNatureConverter |
StelaGTOPropagator.getOrbitNatureConverter()
Get the mean/osculating orbit converter. |
Constructors in fr.cnes.sirius.patrius.stela.propagation with parameters of type OrbitNatureConverter | |
---|---|
ForcesStepHandler(OrbitNatureConverter converterIn,
NonInertialContribution nonInertialContributionIn)
Constructor. |
|
||||||||||
PREV NEXT | FRAMES NO FRAMES |