Uses of Interface
fr.cnes.sirius.patrius.bodies.EllipsoidBodyShape

Packages that use EllipsoidBodyShape

Package	Description
fr.cnes.sirius.patrius.assembly.models.aerocoeffs
fr.cnes.sirius.patrius.attitudes
fr.cnes.sirius.patrius.attitudes.directions
fr.cnes.sirius.patrius.bodies
fr.cnes.sirius.patrius.projections

Uses of EllipsoidBodyShape in fr.cnes.sirius.patrius.assembly.models.aerocoeffs

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

Modifier and Type	Method and Description
static double	AeroCoeffByAoA.angleOfAttackFromSpacecraftState(SpacecraftState state, EllipsoidBodyShape earthShape) Computes the angle of attack from the spacecraft state and the Earth shape.

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

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

Uses of EllipsoidBodyShape in fr.cnes.sirius.patrius.attitudes

Constructors in fr.cnes.sirius.patrius.attitudes with parameters of type EllipsoidBodyShape

Constructor and Description
AeroAttitudeLaw(double angleofattack, double sideslip, double rollVel, EllipsoidBodyShape earthShape) Constructor.
AeroAttitudeLaw(double angleofattack, double sideslip, double rollVel, EllipsoidBodyShape earthShape, double dtSpin, double dtAcc) Constructor with parameterizable delta-time for spin and acceleration computation.
AeroAttitudeLaw(IParameterizableFunction angleofattack, IParameterizableFunction sideslip, IParameterizableFunction rollVel, EllipsoidBodyShape earthShape) Constructor.
AeroAttitudeLaw(IParameterizableFunction angleofattack, IParameterizableFunction sideslip, IParameterizableFunction rollVel, EllipsoidBodyShape earthShape, double dtSpin, double dtAcc) Constructor with parameterizable delta-time for spin and acceleration computation.

Uses of EllipsoidBodyShape in fr.cnes.sirius.patrius.attitudes.directions

Constructors in fr.cnes.sirius.patrius.attitudes.directions with parameters of type EllipsoidBodyShape

Constructor and Description
GlintApproximatePointingDirection(EllipsoidBodyShape shape, PVCoordinatesProvider sunPV) Constructor with default solver ( BisectionSolver.BisectionSolver(double, double)).
GlintApproximatePointingDirection(EllipsoidBodyShape shape, PVCoordinatesProvider sunPV, UnivariateSolver univariateSolver) Constructor.

Uses of EllipsoidBodyShape in fr.cnes.sirius.patrius.bodies

Classes in fr.cnes.sirius.patrius.bodies that implement EllipsoidBodyShape

Modifier and Type	Class and Description
class	ExtendedOneAxisEllipsoid Implementation of the EllipsoidBodyShape interface : this an extended spheroid model to represent celestial bodies shapes.

Uses of EllipsoidBodyShape in fr.cnes.sirius.patrius.projections

Classes in fr.cnes.sirius.patrius.projections that implement EllipsoidBodyShape

Modifier and Type	Class and Description
class	ProjectionEllipsoid Deprecated. as of 4.3. This class is replaced by ProjectionEllipsoidUtils

Methods in fr.cnes.sirius.patrius.projections that return EllipsoidBodyShape

Modifier and Type	Method and Description
EllipsoidBodyShape	AbstractProjection.getReference() Get the system of reference used.

Methods in fr.cnes.sirius.patrius.projections with parameters of type EllipsoidBodyShape

Modifier and Type	Method and Description
static double	ProjectionEllipsoidUtils.computeBearing(GeodeticPoint gv1, GeodeticPoint gv2, EllipsoidBodyShape shape) Compute the bearing (azimuth) between two geodetic Points.
static GeodeticPoint	ProjectionEllipsoidUtils.computeCenterPointAlongLoxodrome(GeodeticPoint p1, GeodeticPoint p2, EllipsoidBodyShape body) Compute center point between two points along a loxodrome.
static double	ProjectionEllipsoidUtils.computeInverseMeridionalDistance(double distance, EllipsoidBodyShape shape) Compute the geodetic latitude, from a distance from the equator.
static double	ProjectionEllipsoidUtils.computeInverseRectifyingLatitude(double rectifyingLat, EllipsoidBodyShape shape) compute geodetic latitude at a given rectifying latitude. rectifying latitude -> giving sphere that has correct distances along the meridians
static double	ProjectionEllipsoidUtils.computeLoxodromicDistance(GeodeticPoint p1, GeodeticPoint p2, EllipsoidBodyShape shape) Loxodromic distance between P1 and P2.This is the distance of constant bearing (or along a line in Mercator).
static double	ProjectionEllipsoidUtils.computeMercatorLatitude(double geodeticLat, EllipsoidBodyShape shape) Compute crescent latitude (Le) at a given geodetic latitude. also called Mercator latitude.
static double	ProjectionEllipsoidUtils.computeMeridionalDistance(double geodeticLat, EllipsoidBodyShape shape) Compute the distance from a given geodetic latitude to the equator, along a meridian.
static double	ProjectionEllipsoidUtils.computeOrthodromicDistance(double lat1, double lon1, double lat2, double lon2, EllipsoidBodyShape shape) Compute the orthodromic distance.
static double	ProjectionEllipsoidUtils.computeOrthodromicDistance(GeodeticPoint p1, GeodeticPoint p2, EllipsoidBodyShape shape) Compute the orthodromic distance between two points.
static GeodeticPoint	ProjectionEllipsoidUtils.computePointAlongLoxodrome(GeodeticPoint p1, double distance, double azimuth, EllipsoidBodyShape shape) Compute the point coordinates from an origin point, an azimuth and a distance along the rhumb line (Loxodrome).
static GeodeticPoint	ProjectionEllipsoidUtils.computePointAlongOrthodrome(GeodeticPoint p1, double distance, double azimuthDirection, EllipsoidBodyShape shape) Compute a geodetic point along orthodrome, from a point p1, at a distance d, in a direction defined from an azimuth.
static double	ProjectionEllipsoidUtils.computeRadiusEastWest(double geodeticLat, EllipsoidBodyShape shape) Compute radius of curvature section East/West (also called M or Re).
static List<GeodeticPoint>	ProjectionEllipsoidUtils.discretizeGreatCircle(GeodeticPoint from, GeodeticPoint to, double maxLength, EllipsoidBodyShape shape) Discretize a great circle into N segments, between two points.
static List<GeodeticPoint>	ProjectionEllipsoidUtils.discretizeRhumbLine(GeodeticPoint from, GeodeticPoint to, double maxLength, EllipsoidBodyShape shape) Discretize a rhumb line into N segments, between two points.
static double	ProjectionEllipsoidUtils.getEccentricity(EllipsoidBodyShape shape) Get the eccentricity.
static double[]	ProjectionEllipsoidUtils.getSeries(EllipsoidBodyShape shape) Getter for series.

Constructors in fr.cnes.sirius.patrius.projections with parameters of type EllipsoidBodyShape

Constructor and Description
AbstractProjection(GeodeticPoint pivotIn, EllipsoidBodyShape shape) Constructor.
GeneralizedFlamsteedSamson(GeodeticPoint pivotPoint, EllipsoidBodyShape shape, double cap) Constructor : Mercator constructor is used with : a pivot point a reference shape a cap parameter centered set to true parameter series set to false indicating that inverse transformation is done with iterations : slower but more accurate
IdentityProjection(EllipsoidBodyShape ellipsoid) Constructor with EllipsoidBodyShape object.
Mercator(double centralMeridian, EllipsoidBodyShape ref) Constructor with default values : The latitude of pivot is 0 azimuth is null (no rotation) centered is false.
Mercator(GeodeticPoint pivotIn, EllipsoidBodyShape shape, double azimuthIn, boolean centeredIn, boolean seriesIn) Complete constructor.