public static interface AbstractIntegratedPropagator.MainStateEquations
|Modifier and Type||Method and Description|
Compute differential equations for main state.
Initialize the equations at the start of propagation.
default void init(SpacecraftState initialState, AbsoluteDate target)
The default implementation of this method does nothing.
initialState- initial state information at the start of propagation.
target- date of propagation. Not equal to
double computeDerivatives(SpacecraftState state)
state- current state
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