Package | Description |
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org.orekit.propagation |
Propagation
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org.orekit.propagation.analytical.gnss |
This package provides classes to propagate GNSS orbits.
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org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
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Modifier and Type | Method | Description |
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List<AdditionalStateProvider> |
AbstractPropagator.getAdditionalStateProviders() |
Get an unmodifiable list of providers for additional state.
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List<AdditionalStateProvider> |
Propagator.getAdditionalStateProviders() |
Get an unmodifiable list of providers for additional state.
|
Modifier and Type | Method | Description |
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void |
AbstractPropagator.addAdditionalStateProvider(AdditionalStateProvider additionalStateProvider) |
Add a set of user-specified state parameters to be computed along with the orbit propagation.
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void |
Propagator.addAdditionalStateProvider(AdditionalStateProvider additionalStateProvider) |
Add a set of user-specified state parameters to be computed along with the orbit propagation.
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Modifier and Type | Class | Description |
---|---|---|
class |
ClockCorrectionsProvider |
Provider for clock corrections as additional states.
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Constructor | Description |
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IntegratedEphemeris(AbsoluteDate startDate,
AbsoluteDate minDate,
AbsoluteDate maxDate,
StateMapper mapper,
boolean meanOrbit,
org.hipparchus.ode.DenseOutputModel model,
Map<String,double[]> unmanaged,
List<AdditionalStateProvider> providers,
String[] equations) |
Creates a new instance of IntegratedEphemeris.
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