Uses of Interface
org.orekit.forces.atmospheres.Atmosphere

Packages that use Atmosphere

fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.stela.forces.atmospheres
fr.cnes.sirius.patrius.stela.forces.drag
fr.cnes.sirius.patrius.wrenches
org.orekit.forces.atmospheres
org.orekit.forces.drag

Uses of Atmosphere in fr.cnes.sirius.patrius.assembly.models

Constructors in fr.cnes.sirius.patrius.assembly.models with parameters of type Atmosphere

AeroModel(Assembly inAssembly, Atmosphere inAtmosphere, OneAxisEllipsoid inGeodPos)
Aero model (the acceleration is computed from all the sub parts of the vehicle) with default step for finite differences computation.

AeroModel(Assembly inAssembly, Atmosphere inAtmosphere, OneAxisEllipsoid earthShapeIn, double altStep)
Aero model (the acceleration is computed from all the sub parts of the vehicle) with an Atmosphere model and a OneAxisEllipsoid for acceleration partial derivatives computation with respect to state by finite differences(including density partial derivatives).

Uses of Atmosphere in fr.cnes.sirius.patrius.stela.forces.atmospheres

Classes in fr.cnes.sirius.patrius.stela.forces.atmospheres that implement Atmosphere

class

MSIS00Adapter This class implements the MSIS00 atmospheric model.

Uses of Atmosphere in fr.cnes.sirius.patrius.stela.forces.drag

Constructors in fr.cnes.sirius.patrius.stela.forces.drag with parameters of type Atmosphere

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.

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.

StelaAtmosphericDrag(DragSensitive inSpacecraft, Atmosphere inAtmosphere, int inSquaringPoints, double inEarthRadius, double inAtmoThreshold, int inDragRecomputeStep)
Constructor.

Uses of Atmosphere in fr.cnes.sirius.patrius.wrenches

Constructors in fr.cnes.sirius.patrius.wrenches with parameters of type Atmosphere

DragWrench(Atmosphere atmosphere, DragWrenchSensitive spacecraft)
Simple constructor.

Uses of Atmosphere in org.orekit.forces.atmospheres

Subinterfaces of Atmosphere in org.orekit.forces.atmospheres

interface

ExtendedAtmosphere Interface for extended atmosphere.

Classes in org.orekit.forces.atmospheres that implement Atmosphere

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

Methods in org.orekit.forces.drag with parameters of type Atmosphere

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

DragForce(Atmosphere atmosphere, DragSensitive spacecraft)
Constructor with multiplicative factor k = 1.0.

DragForce(Atmosphere atmosphere, DragSensitive spacecraft, boolean computePDPos, boolean computePDVel)
Constructor with multiplicative factor k = 1.0.

DragForce(double k, Atmosphere atmosphere, DragSensitive spacecraft)
Constructor with multiplicative factor k.

DragForce(double k, Atmosphere atmosphere, DragSensitive spacecraft, boolean computePDPos, boolean computePDVel)
Constructor with multiplicative factor k.

DragForce(IParamDiffFunction k, Atmosphere atmosphere, DragSensitive spacecraft)
Constructor with multiplicative factor k.

DragForce(IParamDiffFunction k, Atmosphere atmosphere, DragSensitive spacecraft, boolean computePDPos, boolean computePDVel)
Constructor with multiplicative factor k.

DragForce(Parameter k, Atmosphere atmosphere, DragSensitive spacecraft)
Constructor with multiplicative factor k.

DragForce(Parameter k, Atmosphere atmosphere, DragSensitive spacecraft, boolean computePDPos, boolean computePDVel)
Constructor with multiplicative factor k.