Uses of Interface
fr.cnes.sirius.patrius.forces.atmospheres.Atmosphere

Packages that use Atmosphere

Package	Description
fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.assembly.models.aerocoeffs
fr.cnes.sirius.patrius.forces.atmospheres
fr.cnes.sirius.patrius.forces.drag
fr.cnes.sirius.patrius.stela.forces.atmospheres
fr.cnes.sirius.patrius.stela.forces.drag
fr.cnes.sirius.patrius.wrenches

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

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

Constructor and Description
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.assembly.models.aerocoeffs

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

Modifier and Type	Method and Description
static double	AeroCoeffByMach.machFromSpacecraftState(SpacecraftState state, Atmosphere atmosphere) Computes the Mach number from the spacecraft state and an atmosphere model.

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

Constructor and Description
AeroCoeffByAoAAndMach(double[] anglesOfAttack, double[] machNumbers, double[][] coeffs, Atmosphere atmosphere, EllipsoidBodyShape earthShapeIn) Constructor.
AeroCoeffByMach(double[] xVariables, double[] yVariables, Atmosphere atmosphereIn) Constructor.

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

Subinterfaces of Atmosphere in fr.cnes.sirius.patrius.forces.atmospheres

Modifier and Type	Interface and Description
interface	ExtendedAtmosphere Interface for extended atmosphere.

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

Modifier and Type	Class and Description
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.

Methods in fr.cnes.sirius.patrius.forces.atmospheres that return Atmosphere

Modifier and Type	Method and Description
Atmosphere	HarrisPriester.copy() A copy of the atmosphere.
Atmosphere	DTM2000.copy() A copy of the atmosphere.
Atmosphere	US76.copy() A copy of the atmosphere.
Atmosphere	Atmosphere.copy() A copy of the atmosphere.
Atmosphere	MSISE2000.copy() A copy of the atmosphere.
Atmosphere	JB2006.copy() A copy of the atmosphere.
Atmosphere	SimpleExponentialAtmosphere.copy() A copy of the atmosphere.

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

Methods in fr.cnes.sirius.patrius.forces.drag that return Atmosphere

Modifier and Type	Method and Description
Atmosphere	DragForce.getAtmosphere() Get the atmosphere model.

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

Modifier and Type	Method and Description
static Vector3D	DragForce.computeAcceleration(PVCoordinates pv, Frame frame, Atmosphere atm, AbsoluteDate date, double kD, double mass) Method to compute the acceleration.

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

Constructor and Description
DragForce(Atmosphere atmosphereIn, DragSensitive spacecraftIn) Constructor with multiplicative factor k = 1.0.
DragForce(Atmosphere atmosphereIn, DragSensitive spacecraftIn, boolean computePDPos, boolean computePDVel) Constructor with multiplicative factor k = 1.0.
DragForce(double kIn, Atmosphere atmosphereIn, Assembly assembly) Creates a new instance.
DragForce(double kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn) Constructor with multiplicative factor k.
DragForce(double kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn, boolean computePDPos, boolean computePDVel) Constructor with multiplicative factor k.
DragForce(IParamDiffFunction kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn) Constructor with multiplicative factor k.
DragForce(IParamDiffFunction kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn, boolean computePDPos, boolean computePDVel) Constructor with multiplicative factor k.
DragForce(Parameter kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn) Constructor with multiplicative factor k.
DragForce(Parameter kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn, boolean computePDPos, boolean computePDVel) Constructor with multiplicative factor k.

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

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

Modifier and Type	Class and Description
class	MSIS00Adapter This class implements the MSIS00 atmospheric model.

Methods in fr.cnes.sirius.patrius.stela.forces.atmospheres that return Atmosphere

Modifier and Type	Method and Description
Atmosphere	MSIS00Adapter.copy() A copy of the atmosphere.

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

Constructor and Description
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

Constructor and Description
DragWrench(Atmosphere atmosphere, DragWrenchSensitive spacecraft) Simple constructor.