public interface StelaForceModel extends Serializable
StelaGTOPropagator.
Objects implementing this interface are intended to be added to a
semianalytical Stela GTO propagator before the
propagation is started.
ForceModel| Modifier and Type | Method and Description |
|---|---|
double[][] |
computePartialDerivatives(StelaEquinoctialOrbit orbit)
Compute the partial derivatives for a given spacecraft state.
|
double[] |
computeShortPeriods(StelaEquinoctialOrbit orbit,
OrbitNatureConverter converter)
Compute the short periodic variations for a given spacecraft state.
|
String |
getType() |
double[] computeShortPeriods(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) throws PatriusException
orbit - current orbit information: date, kinematicsconverter - converter necessary in some specific case (drag short periods computation)PatriusException - if short periods computation failsdouble[][] computePartialDerivatives(StelaEquinoctialOrbit orbit) throws PatriusException
orbit - current orbit information: date, kinematicsPatriusException - if partial derivatives computation failsString getType()
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