fr.cnes.dynvol.gentleman.calc.data.orbit

Class GtmGeoSimpleOrbit

java.lang.Object

fr.cnes.dynvol.gentleman.calc.data.orbit.AbstractGtmSimpleOrbit

fr.cnes.dynvol.gentleman.calc.data.orbit.GtmGeoSimpleOrbit

public class GtmGeoSimpleOrbit
extends AbstractGtmSimpleOrbit

Class to define simple GEO orbits data.

Author:

goesterjf

Field Summary

Fields inherited from class fr.cnes.dynvol.gentleman.calc.data.orbit.AbstractGtmSimpleOrbit

date, inc, orbit

Constructor Summary

Constructors

Constructor and Description
GtmGeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date, double dhp, double dha, double inc, double longi) Constructor

Method Summary

Modifier and Type	Method and Description
protected void	buildOrbit() Method to build the initial equinoctial orbit corresponding to the required hp/ha/inc and longitude.
double	getDha() Method to get the delta vs GEO orbit on the apogee altitude.
double	getDhp() Method to get the delta vs GEO orbit on the perigee altitude.
double	getLongi() Method to get the longitude vs ITRF of the orbit.

Methods inherited from class fr.cnes.dynvol.gentleman.calc.data.orbit.AbstractGtmSimpleOrbit

getDate, getInc, getOrbit

Methods inherited from class java.lang.Object

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

Constructor Detail

GtmGeoSimpleOrbit

public GtmGeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date,
                         double dhp,
                         double dha,
                         double inc,
                         double longi)
                  throws GtmInitException

Constructor

Parameters:

date - date of the orbit.

dhp - delta vs GEO orbit on the perigee altitude (m)

dha - delta on the apogee altitude (m)

inc - inclination (rad)

longi - longitude vs ITRF (rad)

Throws:

GtmInitException - occured when building the orbit

Method Detail

buildOrbit

protected void buildOrbit()
                   throws GtmInitException

Method to build the initial equinoctial orbit corresponding to the required hp/ha/inc and longitude.

Specified by:

buildOrbit in class AbstractGtmSimpleOrbit

Throws:

GtmInitException - occured when building frames or use frames conversion

getDhp

public double getDhp()

Method to get the delta vs GEO orbit on the perigee altitude.

Returns:

delta on the perigee altitude (m)

getDha

public double getDha()

Method to get the delta vs GEO orbit on the apogee altitude.

Returns:

delta on the apogee altitude (m)

getLongi

public double getLongi()

Method to get the longitude vs ITRF of the orbit.

Returns:

longitude vs ITRF (rad)