|
||||||||||
PREV CLASS NEXT CLASS | FRAMES NO FRAMES | |||||||||
SUMMARY: NESTED | FIELD | CONSTR | METHOD | DETAIL: FIELD | CONSTR | METHOD |
java.lang.Object fr.cnes.sirius.patrius.stela.forces.AbstractStelaLagrangeContribution fr.cnes.sirius.patrius.stela.forces.gravity.SolidTidesAcc
public class SolidTidesAcc
Class representing the tidal contribution.
Field Summary |
---|
Fields inherited from class fr.cnes.sirius.patrius.stela.forces.AbstractStelaLagrangeContribution |
---|
dPot |
Constructor Summary | |
---|---|
SolidTidesAcc(boolean computeSunContributionFlag,
boolean computeMoonContributionFlag,
CelestialBody sunBody,
CelestialBody moonBody)
Advanced constructor: the user can choose if the sun or the moon contribution has to be deactivated. |
|
SolidTidesAcc(CelestialBody sunBody,
CelestialBody moonBody)
Default constructor: both sun and moon contributions have to be computed. |
Method Summary | |
---|---|
double[][] |
computePartialDerivatives(StelaEquinoctialOrbit orbit)
Compute the partial derivatives for a given spacecraft state. |
double[] |
computePerturbation(StelaEquinoctialOrbit orbit)
Compute the dE/dt force derivatives for a given spacecraft state. |
double[] |
computeShortPeriods(StelaEquinoctialOrbit orbit)
Compute the short periodic variations for a given spacecraft state. |
CelestialBody |
getMoon()
Get the Moon. |
CelestialBody |
getSun()
Get the Sun. |
Methods inherited from class fr.cnes.sirius.patrius.stela.forces.AbstractStelaLagrangeContribution |
---|
getdPot, getType |
Methods inherited from class java.lang.Object |
---|
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait |
Constructor Detail |
---|
public SolidTidesAcc(CelestialBody sunBody, CelestialBody moonBody)
sunBody
- SunmoonBody
- Moonpublic SolidTidesAcc(boolean computeSunContributionFlag, boolean computeMoonContributionFlag, CelestialBody sunBody, CelestialBody moonBody)
computeSunContributionFlag
- true if sun contribution to be taken into accountcomputeMoonContributionFlag
- true if moon contribution to be taken into accountsunBody
- Sun (may be null if Sun contribution is not taken into account)moonBody
- Moon (may be null if Moon contribution is not taken into account)Method Detail |
---|
public double[] computePerturbation(StelaEquinoctialOrbit orbit) throws OrekitException
computePerturbation
in class AbstractStelaLagrangeContribution
orbit
- current orbit information: date, kinematics
OrekitException
- if perturbation computation failspublic CelestialBody getSun()
public CelestialBody getMoon()
public double[] computeShortPeriods(StelaEquinoctialOrbit orbit) throws OrekitException
orbit
- current orbit information: date, kinematics
OrekitException
- if short periods computation failspublic double[][] computePartialDerivatives(StelaEquinoctialOrbit orbit) throws OrekitException
orbit
- current orbit information: date, kinematics
OrekitException
- if partial derivatives computation fails
|
||||||||||
PREV CLASS NEXT CLASS | FRAMES NO FRAMES | |||||||||
SUMMARY: NESTED | FIELD | CONSTR | METHOD | DETAIL: FIELD | CONSTR | METHOD |