T
- the type of the field elementspublic interface FieldBoundedPropagator<T extends CalculusFieldElement<T>> extends FieldPropagator<T>
This interface provides a mean to retrieve orbital parameters at any time within a given range. It should be implemented by orbit readers based on external data files and by continuous models built after numerical integration has been completed and dense output data as been gathered.
DEFAULT_MASS
Modifier and Type | Method and Description |
---|---|
FieldAbsoluteDate<T> |
getMaxDate()
Get the last date of the range.
|
FieldAbsoluteDate<T> |
getMinDate()
Get the first date of the range.
|
addAdditionalStateProvider, addEventDetector, clearEventsDetectors, clearStepHandlers, getAdditionalStateProviders, getAttitudeProvider, getEphemerisGenerator, getEventsDetectors, getFrame, getInitialState, getManagedAdditionalStates, getMultiplexer, isAdditionalStateManaged, propagate, propagate, resetInitialState, setAttitudeProvider, setStepHandler, setStepHandler
getPVCoordinates
FieldAbsoluteDate<T> getMinDate()
FieldAbsoluteDate<T> getMaxDate()
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