public class GtmLeoSimpleOrbit extends AbstractGtmSimpleOrbit
date, inc, orbit| Constructor and Description |
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GtmLeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date,
double hp,
double ha,
double inc)
Constructor
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| Modifier and Type | Method and Description |
|---|---|
protected void |
buildOrbit()
Method to build the initial ApsisOrbit orbit corresponding to the required hp/ha/inc.
|
double |
getHa()
Method to get the apogee altitude.
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double |
getHp()
Method to get the perigee altitude.
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getDate, getInc, getOrbitpublic GtmLeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date,
double hp,
double ha,
double inc)
throws GtmInitException
date - date of the orbithp - perigee altitude (m)ha - apogee altitude (m)inc - inclination (rad)GtmInitException - occured when building the orbitprotected void buildOrbit()
throws GtmInitException
buildOrbit in class AbstractGtmSimpleOrbitGtmInitException - occured when building frames or use frames conversionpublic double getHp()
public double getHa()
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