org.orekit.tutorials.maneuvers

Class StationKeeping.TutorialStationKeeping

java.lang.Object

org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping

Enclosing class:

StationKeeping

public static class StationKeeping.TutorialStationKeeping
extends Object

Input data for this station-keeping tutorial.

Data are read from a YAML file.

Constructor Summary

Constructors

Constructor and Description
TutorialStationKeeping()

Method Summary

Modifier and Type	Method and Description
double	getCycleDuration() Get the SK cycle duration.
int	getCyclesNumber() Get the number of SK cycles to simulate.
double	getDeltaVMax() Get the DV max.
double	getEasternBoundary() Get the eastern boundary for longitude window.
double	getInitialMass() Get the initial mass of the spacecraft.
double	getIsp() Get the ISP.
int	getNbMaxManeuvers() Get the max number of maneuvers per cycle.
TutorialOrbit	getOrbit() Get the orbit data.
int	getOrbitsSeparation() Get the number of orbits between maneuvers.
double	getOutputStep() Get the time step between printed elements.
double	getWesternBoundary() Get the western boundary for longitude window.
boolean	isPrintToFile() Get the flag for printing results to a file.
void	setCycleDuration(double cycleDuration) Set the SK cycle duration.
void	setCyclesNumber(int cyclesNumber) Set the number of SK cycles to simulate.
void	setDeltaVMax(double deltaVMax) Set the DV max.
void	setEasternBoundary(double easternBoundary) Set the eastern boundary for longitude window.
void	setInitialMass(double initialMass) Set the initial mass of the spacecraft.
void	setIsp(double isp) Set the ISP.
void	setNbMaxManeuvers(int nbMaxManeuvers) Set the max number of maneuvers per cycle.
void	setOrbit(TutorialOrbit orbit) Set the orbit data.
void	setOrbitsSeparation(int orbitsSeparation) Set the number of orbits between maneuvers.
void	setOutputStep(double outputStep) Set the time step between printed elements.
void	setPrintToFile(boolean printToFile) Set the flag for printing results to a file.
void	setWesternBoundary(double westernBoundary) Set the western boundary for longitude window.

Methods inherited from class java.lang.Object

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

Constructor Detail

TutorialStationKeeping

public TutorialStationKeeping()

Method Detail

getOrbit

public TutorialOrbit getOrbit()

Get the orbit data.

Returns:

the orbit data

setOrbit

public void setOrbit(TutorialOrbit orbit)

Set the orbit data.

Parameters:

orbit - orbit data

getEasternBoundary

public double getEasternBoundary()

Get the eastern boundary for longitude window.

Returns:

the eastern boundary (degrees in [-180, 180])

setEasternBoundary

public void setEasternBoundary(double easternBoundary)

Set the eastern boundary for longitude window.

Parameters:

easternBoundary - the eastern boundary (degrees in [-180, 180])

getWesternBoundary

public double getWesternBoundary()

Get the western boundary for longitude window.

Returns:

the western boundary (degrees in [-180, 180])

setWesternBoundary

public void setWesternBoundary(double westernBoundary)

Set the western boundary for longitude window.

Parameters:

westernBoundary - the western boundary (degrees in [-180, 180])

getDeltaVMax

public double getDeltaVMax()

Get the DV max.

Returns:

the DV max (m/s)

setDeltaVMax

public void setDeltaVMax(double deltaVMax)

Set the DV max.

Parameters:

deltaVMax - DV max (m/s)

getIsp

public double getIsp()

Get the ISP.

Returns:

the ISP (s)

setIsp

public void setIsp(double isp)

Set the ISP.

Parameters:

isp - ISP (s)

getInitialMass

public double getInitialMass()

Get the initial mass of the spacecraft.

Returns:

the initial mass (kg)

setInitialMass

public void setInitialMass(double initialMass)

Set the initial mass of the spacecraft.

Parameters:

initialMass - the initial mass (kg)

getNbMaxManeuvers

public int getNbMaxManeuvers()

Get the max number of maneuvers per cycle.

Returns:

the max number of maneuvers per cycle

setNbMaxManeuvers

public void setNbMaxManeuvers(int nbMaxManeuvers)

Set the max number of maneuvers per cycle.

Parameters:

nbMaxManeuvers - the max number of maneuvers per cycle

getOrbitsSeparation

public int getOrbitsSeparation()

Get the number of orbits between maneuvers.

Returns:

the number of orbits between maneuvers

setOrbitsSeparation

public void setOrbitsSeparation(int orbitsSeparation)

Set the number of orbits between maneuvers.

Parameters:

orbitsSeparation - the number of orbits between maneuvers

getCycleDuration

public double getCycleDuration()

Get the SK cycle duration.

Returns:

the cycle duration (days)

setCycleDuration

public void setCycleDuration(double cycleDuration)

Set the SK cycle duration.

Parameters:

cycleDuration - cycle duration (days)

getCyclesNumber

public int getCyclesNumber()

Get the number of SK cycles to simulate.

Returns:

the number of SK cycles to simulate

setCyclesNumber

public void setCyclesNumber(int cyclesNumber)

Set the number of SK cycles to simulate.

Parameters:

cyclesNumber - the number of SK cycles to simulate

isPrintToFile

public boolean isPrintToFile()

Get the flag for printing results to a file.

Returns:

if true, results are printed to a file

setPrintToFile

public void setPrintToFile(boolean printToFile)

Set the flag for printing results to a file.

Parameters:

printToFile - if true, results are are printed to a file

getOutputStep

public double getOutputStep()

Get the time step between printed elements.

Returns:

the time step between printed elements (s)

setOutputStep

public void setOutputStep(double outputStep)

Set the time step between printed elements.

Parameters:

outputStep - time step between printed elements (s)