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.
ThrustPropulsionModel	Interface for a thrust-based propulsion model.
ThrustVectorProvider	Interface defining thrust vectors depending on date and mass only.

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.
PolynomialThrustSegment	Thrust vector given as polynomials for the Cartesian coordinates.
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.