public static interface AbstractIntegratedPropagator.MainStateEquations
Modifier and Type | Method | Description |
---|---|---|
double[] |
computeDerivatives(SpacecraftState state) |
Compute differential equations for main state.
|
default void |
init(SpacecraftState initialState,
AbsoluteDate target) |
Initialize the equations at the start of propagation.
|
default void init(SpacecraftState initialState, AbsoluteDate target)
computeDerivatives(SpacecraftState)
.
The default implementation of this method does nothing.
initialState
- initial state information at the start of propagation.target
- date of propagation. Not equal to
initialState.getDate()
.double[] computeDerivatives(SpacecraftState state)
state
- current stateCopyright © 2002-2019 CS Systèmes d'information. All rights reserved.