Package org.orekit.forces.maneuvers.propulsion
package org.orekit.forces.maneuvers.propulsion
This package provides propulsion models intended to be used with class
Maneuver.-
ClassDescriptionThis abstract class simply serve as a container for a constant thrust maneuver.Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.Thrust vector given as polynomials for the Cartesian coordinates.Thrust propulsion model based on segmented profile.Generic interface for a propulsion model used in a
Maneuver.Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust vector in spherical coordinates.Interface for a thrust-based propulsion model.Interface defining thrust vectors depending on date and mass only.