org.orekit.orbits.orbitalparameters
Interface IOrbitalParameters

All Known Implementing Classes:
AbstractOrbitalParameters, ApsisAltitudeParameters, ApsisRadiusParameters, CartesianParameters, CircularParameters, EquatorialParameters, EquinoctialParameters, KeplerianParameters, ReentryParameters, StelaEquinoctialParameters

public interface IOrbitalParameters

Interface for orbital parameters.

Since:
3.0
Version:
$Id: IOrbitalParameters.java 13121 2015-05-04 12:28:58Z maggiorani $
Author:
Emmanuel Bignon

Method Summary
 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

getMu

double getMu()
Getter for the central acceleration constant.

Returns:
central acceleration constant

getCartesianParameters

CartesianParameters getCartesianParameters()
Convert current orbital parameters into cartesian parameters.

Returns:
current orbital parameters converted into cartesian parameters
See Also:
CartesianParameters

getKeplerianParameters

KeplerianParameters getKeplerianParameters()
Convert current orbital parameters into Keplerian parameters.

Returns:
current orbital parameters converted into Keplerian parameters
See Also:
KeplerianParameters

getCircularParameters

CircularParameters getCircularParameters()
Convert current orbital parameters into circular parameters.

Returns:
current orbital parameters converted into circular parameters
See Also:
CircularParameters

getEquatorialParameters

EquatorialParameters getEquatorialParameters()
Convert current orbital parameters into equatorial parameters.

Returns:
current orbital parameters converted into equatorial parameters
See Also:
EquatorialParameters

getEquinoctialParameters

EquinoctialParameters getEquinoctialParameters()
Convert current orbital parameters into equinoctial parameters.

Returns:
current orbital parameters converted into equinoctial parameters
See Also:
EquinoctialParameters

getApsisAltitudeParameters

ApsisAltitudeParameters getApsisAltitudeParameters(double ae)
Convert current orbital parameters into apsis (using altitude) parameters.

Parameters:
ae - equatorial radius (m)
Returns:
current orbital parameters converted into apsis (using altitude) parameters
See Also:
ApsisAltitudeParameters

getApsisRadiusParameters

ApsisRadiusParameters getApsisRadiusParameters()
Convert current orbital parameters into apsis (using radius) parameters.

Returns:
current orbital parameters converted into apsis (using radius) parameters
See Also:
ApsisRadiusParameters

getReentryParameters

ReentryParameters getReentryParameters(double ae,
                                       double f)
Convert current orbital parameters into reentry parameters.

Parameters:
ae - equatorial radius (m)
f - flattening (f = (a-b)/a)
Returns:
current orbital parameters converted into reentry parameters
See Also:
ReentryParameters

getStelaEquinoctialParameters

StelaEquinoctialParameters getStelaEquinoctialParameters()
Convert current orbital parameters into Stela equinoctial parameters.

Returns:
current orbital parameters converted into Stela equinoctial parameters
See Also:
StelaEquinoctialParameters


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