Package org.orekit.propagation.numerical

Interface Summary

AdditionalEquations	This interface allows users to add their own differential equations to a numerical propagator.
JacobianParametersProvider	Interface for classes that can provide parameters for computing jacobians.
ModeHandler	Common interface for all propagator mode handlers initialization.
TimeDerivativesEquations	Interface summing up the contribution of several forces into orbit and mass derivatives.

Class Summary

AdditionalStateInfo	Utility class that describes in a minimal fashion the structure of an additional state.
AttitudeEquation	This interface allows users to add their own attitude differential equations to a numerical propagator.
Jacobianizer	Class enabling basic ForceModel instances to be used when processing spacecraft state partial derivatives.
JacobiansMapper	Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
NumericalPropagator	This class propagates SpacecraftState using numerical integration.
ParameterConfiguration	Simple container associating a parameter name with a step to compute its jacobian and the provider thant manages it.
PartialDerivativesEquations	Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

Enum Summary

AttitudeEquation.AttitudeType