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Uses of Atmosphere in fr.cnes.sirius.patrius.stela.forces.atmospheres |
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Classes in fr.cnes.sirius.patrius.stela.forces.atmospheres that implement Atmosphere | |
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class |
MSIS00Adapter
This class implements the MSIS00 atmospheric model. |
Uses of Atmosphere in fr.cnes.sirius.patrius.stela.forces.drag |
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Constructors in fr.cnes.sirius.patrius.stela.forces.drag with parameters of type Atmosphere | |
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StelaAeroModel(double inMass,
StelaCd inCd,
double inSurface,
Atmosphere inAtmosphere,
double atmosDX)
Constructor to be used when partial derivatives are computed using the full finite differences method. |
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StelaAeroModel(double inMass,
StelaCd inCd,
double inSurface,
Atmosphere inAtmosphere,
double atmosDH,
GeodPosition inGeodPosition)
Constructor to be used when partial derivatives are computed using the altitude finite differences method. |
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StelaAtmosphericDrag(DragSensitive inSpacecraft,
Atmosphere inAtmosphere,
int inSquaringPoints,
double inEarthRadius,
double inAtmoThreshold,
int inDragRecomputeStep)
Constructor. |
Uses of Atmosphere in fr.cnes.sirius.patrius.wrenches |
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Constructors in fr.cnes.sirius.patrius.wrenches with parameters of type Atmosphere | |
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DragWrench(Atmosphere atmosphere,
DragWrenchSensitive spacecraft)
Simple constructor. |
Uses of Atmosphere in org.orekit.forces.atmospheres |
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Subinterfaces of Atmosphere in org.orekit.forces.atmospheres | |
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interface |
ExtendedAtmosphere
Interface for extended atmosphere. |
Classes in org.orekit.forces.atmospheres that implement Atmosphere | |
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class |
DTM2000
This atmosphere model is the realization of the DTM-2000 model. |
class |
HarrisPriester
This atmosphere model is the realization of the Modified Harris-Priester model. |
class |
JB2006
This is the realization of the Jacchia-Bowman 2006 atmospheric model. |
class |
MSISE2000
This class implements the MSIS00 atmospheric model. |
class |
SimpleExponentialAtmosphere
Simple exponential atmospheric model. |
class |
US76
This class implements the US76 atmospheric model. |
Uses of Atmosphere in org.orekit.forces.drag |
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Methods in org.orekit.forces.drag with parameters of type Atmosphere | |
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static Vector3D |
DragForce.computeAcceleration(PVCoordinates pv,
Frame frame,
Atmosphere atm,
AbsoluteDate date,
double kD,
double mass)
Method to compute the acceleration. |
Constructors in org.orekit.forces.drag with parameters of type Atmosphere | |
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DragForce(Atmosphere atmosphere,
DragSensitive spacecraft)
Constructor with multiplicative factor k = 1.0. |
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DragForce(Atmosphere atmosphere,
DragSensitive spacecraft,
boolean computePDPos,
boolean computePDVel)
Constructor with multiplicative factor k = 1.0. |
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DragForce(double k,
Atmosphere atmosphere,
DragSensitive spacecraft)
Constructor with multiplicative factor k. |
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DragForce(double k,
Atmosphere atmosphere,
DragSensitive spacecraft,
boolean computePDPos,
boolean computePDVel)
Constructor with multiplicative factor k. |
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DragForce(IParamDiffFunction k,
Atmosphere atmosphere,
DragSensitive spacecraft)
Constructor with multiplicative factor k. |
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DragForce(IParamDiffFunction k,
Atmosphere atmosphere,
DragSensitive spacecraft,
boolean computePDPos,
boolean computePDVel)
Constructor with multiplicative factor k. |
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DragForce(Parameter k,
Atmosphere atmosphere,
DragSensitive spacecraft)
Constructor with multiplicative factor k. |
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DragForce(Parameter k,
Atmosphere atmosphere,
DragSensitive spacecraft,
boolean computePDPos,
boolean computePDVel)
Constructor with multiplicative factor k. |
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