fr.cnes.sirius.patrius.orbits.orbitalparameters

Interface IOrbitalParameters

All Known Implementing Classes:

AbstractOrbitalParameters, AlternateEquinoctialParameters, ApsisAltitudeParameters, ApsisRadiusParameters, CartesianParameters, CircularParameters, EquatorialParameters, EquinoctialParameters, KeplerianParameters, ReentryParameters, StelaEquinoctialParameters

public interface IOrbitalParameters

Interface for orbital parameters.

Since:

3.0

Version:

$Id: IOrbitalParameters.java 18071 2017-10-02 16:46:39Z bignon $

Author:

Emmanuel Bignon

Method Summary

Modifier and Type	Method and Description
boolean	equals(Object object) Test for the equality of two orbits.
AlternateEquinoctialParameters	getAlternateEquinoctialParameters() Convert current orbital parameters into alternate equinoctial parameters.
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.
int	hashCode() Get a hashCode for the orbit.

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

getAlternateEquinoctialParameters

AlternateEquinoctialParameters getAlternateEquinoctialParameters()

Convert current orbital parameters into alternate equinoctial parameters.

Returns:

current orbital parameters converted into alternate equinoctial parameters

See Also:

AlternateEquinoctialParameters

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

equals

boolean equals(Object object)

Test for the equality of two orbits.

Orbits are considered equals if they have the same type and all their attributes are equals. In particular, the orbits frame are considered equals if they represent the same instance. If they have the same attributes but are not the same instance, the method will return false.

Overrides:

equals in class Object

Parameters:

object - Object to test for equality to this

Returns:

true if two orbits are equal

hashCode

int hashCode()

Get a hashCode for the orbit.

Overrides:

hashCode in class Object

Returns:

a hash code value for this object