Package org.orekit.forces.maneuvers.propulsion

This package provides propulsion models intended to be used with class Maneuver.

Interface Summary

Interface	Description
PropulsionModel	Generic interface for a propulsion model used in a Maneuver.
ThrustDirectionProvider	Interface to compute the thrust direction of a maneuver.
ThrustPropulsionModel	Interface for a thrust-based propulsion model.

Class Summary

Class	Description
AbstractConstantThrustPropulsionModel	This abstract class simply serve as a container for a constant thrust maneuver.
BasicConstantThrustPropulsionModel	Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.
ConstantThrustDirectionProvider	Simple implementation of VariableThrustDirectionVector, providing a constant direction.
PolynomialThrustSegment	One polynomial segment of a thrust profile.
ProfileThrustPropulsionModel	Thrust propulsion model based on segmented profile.
ScaledConstantThrustPropulsionModel	Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.
ThrustDirectionAndAttitudeProvider	This class is used in to both manage the attitude of the satellite and the direction of thrust.