fr.cnes.sirius.patrius.attitudes

Class AbstractIsisSpinBiasSlew

java.lang.Object

fr.cnes.sirius.patrius.attitudes.AbstractSlew

fr.cnes.sirius.patrius.attitudes.AbstractIsisSpinBiasSlew

All Implemented Interfaces:

AttitudeLeg, AttitudeProvider, Slew, Serializable

Direct Known Subclasses:

IsisAnalyticalSpinBiasSlew, IsisNumericalSpinBiasSlew

public abstract class AbstractIsisSpinBiasSlew
extends AbstractSlew

Abstract class for ISIS spin bias slew: slew with trapezoidal angular velocity profile calculated in GCRF.

Since:

3.3

Version:

$Id: AbstractIsisSpinBiasSlew.java 17582 2017-05-10 12:58:16Z bignon $

Author:

Emmanuel Bignon

See Also:

Serialized Form

Concurrency :

not thread safe

Nested Class Summary

Nested Classes

Modifier and Type	Class and Description
static class	AbstractIsisSpinBiasSlew.TypeOfDate Type of provided date.

Field Summary

Fields

Modifier and Type	Field and Description
protected double	accelDuration Duration of the acceleration phase.
protected double	accelMax Value of the acceleration step during the first phase.
protected double	decelDuration Duration of the deceleration phase.
protected double	decelMax Value of the deceleration step during the last phase (assumed > 0).
protected double	dtSCAO Time step.
protected double	durationWoTranq Duration of the spin bias slew, excluding the tranquillisation phase.
protected TabulatedAttitude	ephem Attitude ephemerides of the slew, including the tranquillisation phase.
protected AbsoluteDate	initialOrFinalDate Initial or final date of the slew.
protected Frame	refFrame Reference frame.
protected double	slewAngle Angle of the rotation associated to the spin bias slew.
protected Vector3D	slewAxis Axis of the rotation associated to the spin bias slew.
protected boolean	spinDerivativesComputation Flag to indicate if spin derivation computation is activated.
protected AbstractIsisSpinBiasSlew.TypeOfDate	typeOfDate Type of reference date: initial date or final date.

Fields inherited from class fr.cnes.sirius.patrius.attitudes.AbstractSlew

computed, currentProvider, fLaw, iLaw, intervalOfValidity

Constructor Summary

Constructors

Constructor and Description
AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialOrFinalDateIn, AbstractIsisSpinBiasSlew.TypeOfDate typeOfDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn) Constructor with default maximum number of iterations allowed for slew duration computation's convergence.
AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialOrFinalDateIn, AbstractIsisSpinBiasSlew.TypeOfDate typeOfDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn, int maxIterationsNumberIn) Constructor.

Method Summary

Methods

Modifier and Type	Method and Description
double	computeDuration(PVCoordinatesProvider pvProv) Computes the slew duration.
Attitude	getAttitude(AbsoluteDate date, Frame frame) Compute the attitude.
TabulatedAttitude	getEphemeris() Get the attitude ephemeris representing the slew.
void	setSpinDerivativesComputation(boolean computeSpinDerivatives) Method to activate spin derivative computation.

Methods inherited from class fr.cnes.sirius.patrius.attitudes.AbstractSlew

getAttitude, getAttitude, getDuration, getTimeInterval

Methods inherited from class java.lang.Object

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

Methods inherited from interface fr.cnes.sirius.patrius.attitudes.Slew

compute

Field Detail

initialOrFinalDate

protected final AbsoluteDate initialOrFinalDate

Initial or final date of the slew.

typeOfDate

protected final AbstractIsisSpinBiasSlew.TypeOfDate typeOfDate

Type of reference date: initial date or final date.

refFrame

protected final Frame refFrame

Reference frame.

dtSCAO

protected final double dtSCAO

Time step.

spinDerivativesComputation

protected boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

slewAngle

protected double slewAngle

Angle of the rotation associated to the spin bias slew.

slewAxis

protected Vector3D slewAxis

Axis of the rotation associated to the spin bias slew.

durationWoTranq

protected double durationWoTranq

Duration of the spin bias slew, excluding the tranquillisation phase.

accelMax

protected double accelMax

Value of the acceleration step during the first phase.

decelMax

protected double decelMax

Value of the deceleration step during the last phase (assumed > 0).

accelDuration

protected double accelDuration

Duration of the acceleration phase.

decelDuration

protected double decelDuration

Duration of the deceleration phase.

ephem

protected TabulatedAttitude ephem

Attitude ephemerides of the slew, including the tranquillisation phase.

Constructor Detail

AbstractIsisSpinBiasSlew

public AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn,
                        AttitudeProvider finalLawIn,
                        AbsoluteDate initialOrFinalDateIn,
                        AbstractIsisSpinBiasSlew.TypeOfDate typeOfDateIn,
                        double dtSCAOIn,
                        double thetaMaxAllowedIn,
                        double durationMaxIn,
                        double dtConvergenceThresholdIn,
                        double[][] inertiaMatrixIn,
                        double rwTorqueAllocAccelIn,
                        double rwTorqueAllocDecelIn,
                        double rwDeltaMomentumAllocIn,
                        double[][] rwMatrixIn,
                        double tranquillisationTimeIn)

Constructor with default maximum number of iterations allowed for slew duration computation's convergence.

Parameters:

initialLawIn - attitude law before the slew

finalLawIn - attitude law after the slew

initialOrFinalDateIn - slew initial or final date (choice given by TypeOfDate argument)

typeOfDateIn - defines type of provided date AbstractIsisSpinBiasSlew.TypeOfDate (initial date or final date)

dtSCAOIn - time step (s)

thetaMaxAllowedIn - maximum slew angular amplitude allowed (rad)

durationMaxIn - maximum duration expected for the slew, including the tranquilisation phase (s)

dtConvergenceThresholdIn - convergence threshold for the iterative computation of the slew duration (s)

inertiaMatrixIn - satellite inertia matrix in satellite reference frame (kg.m^2)

rwTorqueAllocAccelIn - torque allocation for each RW during the acceleration phase (N.m)

rwTorqueAllocDecelIn - torque allocation for each RW during the deceleration phase (assumed > 0) (N.m)

rwDeltaMomentumAllocIn - angular momentum allocation for each RW during the manoeuvre (N.m.s)

rwMatrixIn - cosine directors matrix of the reaction wheels in the satellite reference frame. Matrix 3xN_RW with N_RW wheels (Reaction wheels spin axes written in column in the satellite reference frame).

tranquillisationTimeIn - tranquilisation time after the end of the slew (s)

AbstractIsisSpinBiasSlew

public AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn,
                        AttitudeProvider finalLawIn,
                        AbsoluteDate initialOrFinalDateIn,
                        AbstractIsisSpinBiasSlew.TypeOfDate typeOfDateIn,
                        double dtSCAOIn,
                        double thetaMaxAllowedIn,
                        double durationMaxIn,
                        double dtConvergenceThresholdIn,
                        double[][] inertiaMatrixIn,
                        double rwTorqueAllocAccelIn,
                        double rwTorqueAllocDecelIn,
                        double rwDeltaMomentumAllocIn,
                        double[][] rwMatrixIn,
                        double tranquillisationTimeIn,
                        int maxIterationsNumberIn)

Constructor.

Parameters:

initialLawIn - attitude law before the slew

finalLawIn - attitude law after the slew

initialOrFinalDateIn - initial or final date of the slew (choice given by TypeOfDate argument)

typeOfDateIn - defines type of provided date AbstractIsisSpinBiasSlew.TypeOfDate (initial date or final date)

dtSCAOIn - time step (s)

thetaMaxAllowedIn - maximum slew angular amplitude allowed (rad)

durationMaxIn - maximum duration expected for the slew, including the tranquilisation phase (s)

dtConvergenceThresholdIn - convergence threshold for the iterative computation of the slew duration (s)

inertiaMatrixIn - satellite inertia matrix in satellite reference frame (kg.m^2)

rwTorqueAllocAccelIn - torque allocation for each RW during the acceleration phase (N.m)

rwTorqueAllocDecelIn - torque allocation for each RW during the deceleration phase (assumed > 0) (N.m)

rwDeltaMomentumAllocIn - angular momentum allocation for each RW during the manoeuvre (N.m.s)

rwMatrixIn - cosine directors matrix of the reaction wheels in the satellite reference frame. Matrix 3xN_RW with N_RW wheels (Reaction wheels spin axes written in column in the satellite reference frame).

tranquillisationTimeIn - tranquilisation time after the end of the slew (s)

maxIterationsNumberIn - maximum number of iterations allowed for slew duration computation's convergence

Method Detail

computeDuration

public double computeDuration(PVCoordinatesProvider pvProv)
                       throws PatriusException

Computes the slew duration.

Parameters:

pvProv - PV coordinates provider

Returns:

slew duration

Throws:

PatriusException - thrown if an error occurs during attitudes computation

getAttitude

public Attitude getAttitude(AbsoluteDate date,
                   Frame frame)
                     throws PatriusException

Compute the attitude.

Parameters:

date - : current date

frame - : reference frame from which attitude is computed

Returns:

attitude : attitude at the specified date

Throws:

PatriusException - orekit exception

getEphemeris

public TabulatedAttitude getEphemeris()

Get the attitude ephemeris representing the slew.

Returns:

the ephemeris

setSpinDerivativesComputation

public void setSpinDerivativesComputation(boolean computeSpinDerivatives)

Method to activate spin derivative computation.

Parameters:

computeSpinDerivatives - true if spin derivatives should be computed