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public interface IOrbitalParameters
Interface for orbital parameters.
Method Summary | |
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ApsisAltitudeParameters |
getApsisAltitudeParameters(double ae)
Convert current orbital parameters into apsis (using altitude) parameters. |
ApsisRadiusParameters |
getApsisRadiusParameters()
Convert current orbital parameters into apsis (using radius) parameters. |
CartesianParameters |
getCartesianParameters()
Convert current orbital parameters into cartesian parameters. |
CircularParameters |
getCircularParameters()
Convert current orbital parameters into circular parameters. |
EquatorialParameters |
getEquatorialParameters()
Convert current orbital parameters into equatorial parameters. |
EquinoctialParameters |
getEquinoctialParameters()
Convert current orbital parameters into equinoctial parameters. |
KeplerianParameters |
getKeplerianParameters()
Convert current orbital parameters into Keplerian parameters. |
double |
getMu()
Getter for the central acceleration constant. |
ReentryParameters |
getReentryParameters(double ae,
double f)
Convert current orbital parameters into reentry parameters. |
StelaEquinoctialParameters |
getStelaEquinoctialParameters()
Convert current orbital parameters into Stela equinoctial parameters. |
Method Detail |
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double getMu()
CartesianParameters getCartesianParameters()
CartesianParameters
KeplerianParameters getKeplerianParameters()
KeplerianParameters
CircularParameters getCircularParameters()
CircularParameters
EquatorialParameters getEquatorialParameters()
EquatorialParameters
EquinoctialParameters getEquinoctialParameters()
EquinoctialParameters
ApsisAltitudeParameters getApsisAltitudeParameters(double ae)
ae
- equatorial radius (m)
ApsisAltitudeParameters
ApsisRadiusParameters getApsisRadiusParameters()
ApsisRadiusParameters
ReentryParameters getReentryParameters(double ae, double f)
ae
- equatorial radius (m)f
- flattening (f = (a-b)/a)
ReentryParameters
StelaEquinoctialParameters getStelaEquinoctialParameters()
StelaEquinoctialParameters
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