org.orekit.forces.maneuvers

Class Maneuver

java.lang.Object

org.orekit.forces.AbstractForceModel

org.orekit.forces.maneuvers.Maneuver

All Implemented Interfaces:

ForceModel

Direct Known Subclasses:

ConfigurableLowThrustManeuver, ConstantThrustManeuver

public class Maneuver
extends AbstractForceModel

A generic model for maneuvers. It contains: - An attitude override, this is the attitude used during the maneuver, it can be different than the one used for propagation; - A maneuver triggers object from the trigger sub-package. It defines the triggers used to start and stop the maneuvers (dates or events for example). - A propulsion model from sub-package propulsion. It defines the thrust or ΔV, isp, flow rate etc.. Both the propulsion model and the maneuver triggers can contain parameter drivers (for estimation). The convention here is that the propulsion model drivers are given before the maneuver triggers when calling the method getParametersDrivers()

Since:

10.2

Author:

Maxime Journot

Constructor Summary

Constructors

Constructor and Description
Maneuver(AttitudeProvider attitudeOverride, ManeuverTriggers maneuverTriggers, PropulsionModel propulsionModel) Generic maneuver constructor.

Method Summary

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldVector3D<T>	acceleration(FieldSpacecraftState<T> s, T[] parameters) Compute acceleration.
Vector3D	acceleration(SpacecraftState s, double[] parameters) Compute acceleration.
<T extends RealFieldElement<T>> void	addContribution(FieldSpacecraftState<T> s, FieldTimeDerivativesEquations<T> adder) Compute the contribution of the force model to the perturbing acceleration.
void	addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
boolean	dependsOnPositionOnly() Check if force models depends on position only.
AttitudeProvider	getAttitudeOverride() Get the attitude override used for the maneuver.
Stream<EventDetector>	getEventsDetectors() Get the discrete events related to the model.
<T extends RealFieldElement<T>> Stream<FieldEventDetector<T>>	getFieldEventsDetectors(Field<T> field) Get the discrete events related to the model.
ManeuverTriggers	getManeuverTriggers() Get the maneuver triggers.
String	getName() Get the name of the maneuver.
ParameterDriver[]	getParametersDrivers() Get the drivers for force model parameters.
PropulsionModel	getPropulsionModel() Get the propulsion model.
void	init(SpacecraftState initialState, AbsoluteDate target) Initialize the force model at the start of propagation.

Methods inherited from class org.orekit.forces.AbstractForceModel

complainIfNotSupported, getParameterDriver, isSupported

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.forces.ForceModel

getParameters, getParameters

Constructor Detail

Maneuver

public Maneuver(AttitudeProvider attitudeOverride,
                ManeuverTriggers maneuverTriggers,
                PropulsionModel propulsionModel)

Generic maneuver constructor.

Parameters:

attitudeOverride - attitude provider for the attitude during the maneuver

maneuverTriggers - maneuver triggers

propulsionModel - propulsion model

Method Detail

getName

public String getName()

Get the name of the maneuver. The name can be in the propulsion model, in the maneuver triggers or both. If it is in both it should be the same since it refers to the same maneuver. The name is inferred from the propulsion model first, then from the maneuver triggers if the propulsion model had an empty name.

Returns:

the name

getAttitudeOverride

public AttitudeProvider getAttitudeOverride()

Get the attitude override used for the maneuver.

Returns:

the attitude override

getPropulsionModel

public PropulsionModel getPropulsionModel()

Get the propulsion model.

Returns:

the propulsion model

getManeuverTriggers

public ManeuverTriggers getManeuverTriggers()

Get the maneuver triggers.

Returns:

the maneuver triggers

dependsOnPositionOnly

public boolean dependsOnPositionOnly()

Check if force models depends on position only.

Returns:

true if force model depends on position only, false if it depends on velocity, either directly or due to a dependency on attitude

init

public void init(SpacecraftState initialState,
                 AbsoluteDate target)

Initialize the force model at the start of propagation. This method will be called before any calls to ForceModel.addContribution(SpacecraftState, TimeDerivativesEquations), ForceModel.addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations), ForceModel.acceleration(SpacecraftState, double[]) or ForceModel.acceleration(FieldSpacecraftState, RealFieldElement[])

The default implementation of this method does nothing.

Parameters:

initialState - spacecraft state at the start of propagation.

target - date of propagation. Not equal to initialState.getDate().

addContribution

public void addContribution(SpacecraftState s,
                            TimeDerivativesEquations adder)

Compute the contribution of the force model to the perturbing acceleration.

The default implementation simply adds the acceleration as a non-Keplerian acceleration.

Parameters:

s - current state information: date, kinematics, attitude

adder - object where the contribution should be added

addContribution

public <T extends RealFieldElement<T>> void addContribution(FieldSpacecraftState<T> s,
                                                            FieldTimeDerivativesEquations<T> adder)

Compute the contribution of the force model to the perturbing acceleration.

Type Parameters:

T - type of the elements

Parameters:

s - current state information: date, kinematics, attitude

adder - object where the contribution should be added

acceleration

public Vector3D acceleration(SpacecraftState s,
                             double[] parameters)

Description copied from interface: ForceModel

Compute acceleration.

Parameters:

s - current state information: date, kinematics, attitude

parameters - values of the force model parameters

Returns:

acceleration in same frame as state

acceleration

public <T extends RealFieldElement<T>> FieldVector3D<T> acceleration(FieldSpacecraftState<T> s,
                                                                     T[] parameters)

Description copied from interface: ForceModel

Compute acceleration.

Type Parameters:

T - type of the elements

Parameters:

s - current state information: date, kinematics, attitude

parameters - values of the force model parameters

Returns:

acceleration in same frame as state

getEventsDetectors

public Stream<EventDetector> getEventsDetectors()

Get the discrete events related to the model.

Returns:

stream of events detectors

getFieldEventsDetectors

public <T extends RealFieldElement<T>> Stream<FieldEventDetector<T>> getFieldEventsDetectors(Field<T> field)

Get the discrete events related to the model.

Type Parameters:

T - extends RealFieldElement<T>

Parameters:

field - field to which the state belongs

Returns:

stream of events detectors

getParametersDrivers

public ParameterDriver[] getParametersDrivers()

Description copied from interface: ForceModel

Get the drivers for force model parameters.

Returns:

drivers for force model parameters