| Package | Description | 
|---|---|
| agi.foundation.access | 
 Contains types used in performing access calculations. 
 | 
| agi.foundation.access.constraints | 
 Contains types used in modeling constraints applied to the calculation of access. 
 | 
| agi.foundation.aircraftpropagation | 
 Contains types for propagating an aircraft through various maneuvers subject to 
 flight phase performance models and wind effects. 
 | 
| agi.foundation.ccsds | 
 Contains types for interoperating with data formats supported by 
 The Consultative Committee for Space Data Systems (CCSDS). 
 | 
| agi.foundation.celestial | 
 Contains types used in modeling characteristics of celestial objects and celestial phenomena. 
 | 
| agi.foundation.cesium | 
 Contains types used for defining graphical properties of definitional objects to be written out as CZML. 
 | 
| agi.foundation.communications | 
 Contains types for representing electromagnetic signals and propagating them along communication links. 
 | 
| agi.foundation.coverage | 
 Contains types for computing complex access calculations between many different objects simultaneously. 
 | 
| agi.foundation.geometry | 
 Contains types for expressing the motion of fundamental geometric objects such as points, axes, and reference frames; 
 the manner in which they are related; and transformations between representations. 
 | 
| agi.foundation.geometry.discrete | 
 Contains types which define discretization algorithms and metadata for analysis of spatial geometry. 
 | 
| agi.foundation.graphics | 
 Provides commonly used and instantiated graphics types related to 3D scene management, terrain and imagery, and more. 
 | 
| agi.foundation.navigation | 
 Contains types useful in modeling navigation processes which utilize the Global Positioning System (GPS). 
 | 
| agi.foundation.navigation.advanced | 
 Contains types used in GPS communications modeling. 
 | 
| agi.foundation.navigation.datareaders | 
 Contains types for reading various navigation-related data file formats. 
 | 
| agi.foundation.platforms | 
 Contains types used in modeling various mechanical platforms such as satellites, facilities, aircraft, etc. 
 | 
| agi.foundation.propagators | 
 Contains types used in producing the state of an object from a known element set. 
 | 
| agi.foundation.propagators.advanced | 
 Contains types used to create more specialized propagation scenarios. 
 | 
| agi.foundation.routedesign | 
 Contains types for creating simple routes by specifying procedures at points of interest, how to connect them, and what height and speed to use along the route. 
 | 
| agi.foundation.segmentpropagation | 
 Contains types for modeling a trajectory in segments, where the type of propagation varies for each segment. 
 | 
| agi.foundation.spice | 
 Contains types used in modeling the ephemeris of solar system bodies using JPL SPICE files. 
 | 
| agi.foundation.stk | 
 Contains types for interoperating with the STK desktop application and related data. 
 | 
| agi.foundation.tracking | 
 Contains types for acquiring, analyzing and archiving dynamic data, such as those found in real-time feeds or simulation environments. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
static Evaluator<JulianDate> | 
AccessConstraintSampling.getNextStepFromRelativeMotionEvaluator(ReferenceFrame observer,
                                      Point target,
                                      double maximumAngularMotion,
                                      EvaluatorGroup group)
Gets an evaluator that determines the next time at which to sample a constraint function
    based on the relative motion between two objects and a maximum relative motion per step. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
ThirdBodyElevationAngleConstraint.getThirdBodyPoint()
Gets the center of mass point for the third body. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
ThirdBodyElevationAngleConstraint.setThirdBodyPoint(Point value)
Sets the center of mass point for the third body. 
 | 
| Constructor and Description | 
|---|
ThirdBodyElevationAngleConstraint(CentralBody centralBody,
                                 Point thirdBodyPoint,
                                 double minimumValue)
Initializes a new instance with the specified central body, third body point, and minimum value. 
 | 
ThirdBodyElevationAngleConstraint(CentralBody centralBody,
                                 Point thirdBodyPoint,
                                 double minimumValue,
                                 double maximumValue)
Initializes a new instance with the specified central body, third body point, minimum value, and maximum value. 
 | 
ThirdBodyElevationAngleConstraint(IServiceProvider constrainedObject,
                                 CentralBody centralBody,
                                 Point thirdBodyPoint,
                                 double minimumValue)
Initializes a new instance with the specified constrained object, central body, third body point, and minimum value. 
 | 
ThirdBodyElevationAngleConstraint(IServiceProvider constrainedObject,
                                 CentralBody centralBody,
                                 Point thirdBodyPoint,
                                 double minimumValue,
                                 double maximumValue)
Initializes a new instance with the specified constrained object, central body, third body point,
    minimum value, and maximum value. 
 | 
ThirdBodyElevationAngleConstraint(IServiceProvider constrainedObject,
                                 Point thirdBodyPoint,
                                 double minimumValue)
Initializes a new instance with the specified constrained object, third body point, and minimum value. 
 | 
ThirdBodyElevationAngleConstraint(IServiceProvider constrainedObject,
                                 Point thirdBodyPoint,
                                 double minimumValue,
                                 double maximumValue)
Initializes a new instance with the specified constrained object, third body point, minimum value, and maximum value. 
 | 
ThirdBodyElevationAngleConstraint(Point thirdBodyPoint,
                                 double minimumValue)
Initializes a new instance with the specified third body point and minimum value. 
 | 
ThirdBodyElevationAngleConstraint(Point thirdBodyPoint,
                                 double minimumValue,
                                 double maximumValue)
Initializes a new instance with the specified third body point, minimum value, and maximum value. 
 | 
| Modifier and Type | Class and Description | 
|---|---|
class  | 
AircraftMotionIntegrationPoint
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
AircraftMotionElement.getIntegrationPoint()
Gets a  
Point which is parameterized on the position and velocity in the state
    during integration. | 
Point | 
SimpleForwardFlightPropellerPropulsion.getReferencePoint()
Gets the point at which the propulsion model is to be applied. 
 | 
Point | 
SimpleForwardFlightJetPropulsion.getReferencePoint()
Gets the point at which the propulsion model is to be applied. 
 | 
Point | 
SimpleFixedWingCoordinatedFlight.getReferencePoint()
Gets the point at which the coordinated flight condition is imposed. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
protected boolean | 
AircraftMotionIntegrationPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
void | 
SimpleForwardFlightPropellerPropulsion.setReferencePoint(Point value)
Sets the point at which the propulsion model is to be applied. 
 | 
void | 
SimpleForwardFlightJetPropulsion.setReferencePoint(Point value)
Sets the point at which the propulsion model is to be applied. 
 | 
void | 
SimpleFixedWingCoordinatedFlight.setReferencePoint(Point value)
Sets the point at which the coordinated flight condition is imposed. 
 | 
| Constructor and Description | 
|---|
SimpleFixedWingCoordinatedFlight(Point referencePoint,
                                WindModel windModel,
                                SimpleFixedWingForwardFlightAerodynamics aerodynamicModel,
                                Scalar mass,
                                Scalar gravityModel)
Initializes a new instance with the specified parameters. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
CcsdsOrbitEphemerisMessageSegment.createPoint()
    Creates a  
Point whose time-varying position is computed by interpolating
    over the ephemeris data held by this instance. | 
| Modifier and Type | Method and Description | 
|---|---|
static Point | 
EarthMoonBarycenter.computeEarthMoonBarycenterPoint(Point earthCenterOfMassPoint,
                               Point moonCenterOfMassPoint,
                               double earthMoonMassRatio)
Computes the position of the Earth-Moon barycenter using the
    Earth-Moon mass ratio and the positions of the
    Earth and Moon. 
 | 
Point | 
JplDE.createEarthMoonBarycenterPoint()
Creates a  
Point that represents the position of
    the Earth-Moon barycenter calculated from the data in this class. | 
static Point | 
UranianMoonsAnalyticEphemeris.getAriel()
Gets a point describing the motion of Ariel. 
 | 
Point | 
GravityGradientTorque.getBodyCenterOfMass()
Gets the center of mass point of the gravity-gradient satellite. 
 | 
static Point | 
JovianMoonsAnalyticEphemeris.getCallisto()
Gets a point describing the motion of Callisto. 
 | 
Point | 
VestaCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
VenusCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
UranusCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
TritonCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
TitaniaCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
TitanCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
TethysCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
SunCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
SolarSystemBarycenter.getCenterOfMassPoint()
Gets a point describing the center of mass of this solar system. 
 | 
Point | 
SaturnCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
RheaCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
PlutoCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
PlanetarySystemBarycenter.getCenterOfMassPoint()
Gets a point describing the center of mass of this planetary system. 
 | 
Point | 
PhoebeCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
PhobosCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
NeptuneCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
MoonCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
MimasCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
MercuryCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
MarsCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
JupiterCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
IoCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
IapetusCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
HyperionCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
GanymedeCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
EuropaCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
EnceladusCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
EarthCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
DioneCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
DeimosCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
CharonCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
CeresCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
abstract Point | 
CentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
CallistoCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
Point | 
ArielCentralBody.getCenterOfMassPoint()
Gets a point describing the center of mass of this central body. 
 | 
static Point | 
SmallSolarSystemBodyAnalyticEphemeris.getCeres()
Gets a point describing the motion of Ceres. 
 | 
static Point | 
PlutonianMoonsAnalyticEphemeris.getCharon()
Gets a point describing the motion of Charon. 
 | 
static Point | 
MartianMoonsAnalyticEphemeris.getDeimos()
Gets a point describing the motion of Deimos. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getDione()
Gets a point describing the motion of Dione. 
 | 
static Point | 
Simon1994PlanetaryPositions.getEarth()
Gets a point describing the motion of the Earth. 
 | 
static Point | 
Simon1994PlanetaryPositions.getEarthMoonBarycenter()
Gets a point describing the motion of the Earth-Moon barycenter according to the equations
    described in section 6. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getEnceladus()
Gets a point describing the motion of Enceladus. 
 | 
static Point | 
JovianMoonsAnalyticEphemeris.getEuropa()
Gets a point describing the motion of Europa. 
 | 
static Point | 
JovianMoonsAnalyticEphemeris.getGanymede()
Gets a point describing the motion of Ganymede. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getHyperion()
Gets a point describing the motion of Hyperion. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getIapetus()
Gets a point describing the motion of Iapetus. 
 | 
Point | 
ScalarVariableAreaArgumentLatitude.getIntegrationPoint()
Gets the  
Point used to determine the argument of latitude
    at a particular time. | 
static Point | 
JovianMoonsAnalyticEphemeris.getIo()
Gets a point describing the motion of Io. 
 | 
static Point | 
Simon1994PlanetaryPositions.getJupiter()
Gets a point describing the motion of Jupiter according to the equations
    described in section 6. 
 | 
Point | 
CentralBody.getLocationPoint()
Gets the point that describes the position of the object. 
 | 
static Point | 
Simon1994PlanetaryPositions.getMars()
Gets a point describing the motion of Mars according to the equations
    described in section 6. 
 | 
static Point | 
Simon1994PlanetaryPositions.getMercury()
Gets a point describing the motion of Mercury according to the equations
    described in section 6. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getMimas()
Gets a point describing the motion of Mimas. 
 | 
static Point | 
Simon1994PlanetaryPositions.getMoon()
Gets a point describing the position of the moon according to the equations described in
    section 4. 
 | 
static Point | 
Simon1994PlanetaryPositions.getNeptune()
Gets a point describing the motion of Neptune according to the equations
    described in section 6. 
 | 
static Point | 
MartianMoonsAnalyticEphemeris.getPhobos()
Gets a point describing the motion of Phobos. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getPhoebe()
Gets a point describing the motion of Phoebe. 
 | 
static Point | 
SmallSolarSystemBodyAnalyticEphemeris.getPluto()
Gets a point describing the motion of Pluto. 
 | 
Point | 
ThirdBodyGravity.ThirdBodyInfo.getPosition()
Gets the  
Point representing the position of the perturbing gravitational body. | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getRhea()
Gets a point describing the motion of Rhea. 
 | 
static Point | 
Simon1994PlanetaryPositions.getSaturn()
Gets a point describing the motion of Saturn according to the equations
    described in section 6. 
 | 
Point | 
TwoBodyGravity.getTargetPoint()
Gets the target point at which to measure the gravitational acceleration. 
 | 
Point | 
ThirdBodyGravity.getTargetPoint()
Gets the target point at which the gravity is measured. 
 | 
Point | 
SphericalHarmonicGravity.getTargetPoint()
Gets the target point at which to measure the gravitational acceleration. 
 | 
Point | 
SimpleSolarRadiationForce.getTargetPoint()
 | 
Point | 
ScalarAtmosphericDensity.getTargetPoint()
Gets the target point describing the time-varying position at which density is
    to be calculated. 
 | 
Point | 
NPlateSolarRadiationForce.getTargetPoint()
 | 
Point | 
NPlateAtmosphericDragForce.getTargetPoint()
 | 
Point | 
IersTechnicalNote36RelativisticCorrectionForce.getTargetPoint()
Gets the point at which the  
IersTechnicalNote36RelativisticCorrectionForce is applied. | 
Point | 
AtmosphericDragForce.getTargetPoint()
 | 
Point | 
ScalarOccultation.getTargetPoint()
Gets the  
Point representing the location at which
    the occultation factor is being calculated. | 
Point | 
MagneticFieldVector.getTargetPoint()
Gets the point where the magnetic field vector is calculated. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getTethys()
Gets a point describing the motion of Tethys. 
 | 
static Point | 
SaturnianMoonsAnalyticEphemeris.getTitan()
Gets a point describing the motion of Titan. 
 | 
static Point | 
UranianMoonsAnalyticEphemeris.getTitania()
Gets a point describing the motion of Titania. 
 | 
static Point | 
NeptunianMoonsAnalyticEphemeris.getTriton()
Gets a point describing the motion of Triton. 
 | 
static Point | 
Simon1994PlanetaryPositions.getUranus()
Gets a point describing the motion of Uranus according to the equations
    described in section 6. 
 | 
static Point | 
Simon1994PlanetaryPositions.getVenus()
Gets a point describing the motion of Venus according to the equations
    described in section 6. 
 | 
static Point | 
SmallSolarSystemBodyAnalyticEphemeris.getVesta()
Gets a point describing the motion of Vesta. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
TimeVaryingSolidTideModel.addThirdBody(String name,
            Point point,
            double gravitationalParameter)
Adds a  
Point representing the position of the tide-inducing gravitational body
    and a double representing its gravitational parameter, in meters cubed per second squared. | 
void | 
ThirdBodyGravity.addThirdBody(String name,
            Point point,
            double gravitationalParameter)
Adds a  
Point representing the position of the perturbing gravitational body
    and a double representing its gravitational parameter, in meters cubed per second squared. | 
static Point | 
EarthMoonBarycenter.computeEarthMoonBarycenterPoint(Point earthCenterOfMassPoint,
                               Point moonCenterOfMassPoint,
                               double earthMoonMassRatio)
Computes the position of the Earth-Moon barycenter using the
    Earth-Moon mass ratio and the positions of the
    Earth and Moon. 
 | 
static MagneticCoilTorque | 
MagneticCoilTorque.createMagneticCoilTorqueUsingIgrfCofModel(String filename,
                                         Point bodyCenterOfMass,
                                         double numberOfLoops,
                                         Scalar current,
                                         Vector directedArea,
                                         Axes bodyAxes)
Creates a new magnetic coil torque that uses an  
InternationalGeomagneticReferenceFieldVector
    to describe the magnetic field and a Point to describe
    the position of the spacecraft. | 
static MagneticCoilTorque | 
MagneticCoilTorque.createMagneticCoilTorqueUsingIgrfTxtModel(String filename,
                                         Point bodyCenterOfMass,
                                         double numberOfLoops,
                                         Scalar current,
                                         Vector directedArea,
                                         Axes bodyAxes)
Creates a new magnetic coil torque that uses an  
InternationalGeomagneticReferenceFieldVector
    to describe the magnetic field and a Point to describe
    the position of the spacecraft. | 
static MagneticCoilTorque | 
MagneticCoilTorque.createMagneticCoilTorqueUsingWmmModel(String filename,
                                     Point bodyCenterOfMass,
                                     double numberOfLoops,
                                     Scalar current,
                                     Vector directedArea,
                                     Axes bodyAxes)
Creates a new magnetic coil torque that uses a  
WorldMagneticModelVector
    to describe the magnetic field and a Point to describe
    the position of the spacecraft. | 
MotionEvaluator1<AzimuthElevationRange> | 
CentralBody.getAzimuthElevationRangeEvaluator(Vector vector,
                                 Point observingPoint)
Gets an evaluator to find the azimuth, elevation, and range of a vector as observed
    from a given point. 
 | 
MotionEvaluator1<AzimuthElevationRange> | 
CentralBody.getAzimuthElevationRangeEvaluator(Vector vector,
                                 Point observingPoint,
                                 EvaluatorGroup group)
Gets an evaluator to find the azimuth, elevation, and range of a vector as observed
    from a given point, and associates the evaluator with the specified evaluator group. 
 | 
CentralBody | 
CentralBodiesFacet.getCentralBodyOfPoint(JulianDate date,
                     Point point)
Gets the central body most closely associated with a given point. 
 | 
int | 
ThirdBodyGravity.indexOf(Point point)
Searches  
ThirdBodies (get) and returns the index of the body with the given body position. | 
MotionEvaluator1<Cartographic> | 
CentralBody.observeCartographicPoint(Point point)
Gets an evaluator that can be used to find the  
Cartographic motion of a
    point relative to this central body. | 
MotionEvaluator1<Cartographic> | 
CentralBody.observeCartographicPoint(Point point,
                        EvaluatorGroup group)
Gets an evaluator that can be used to find the  
Cartographic motion of a
    point relative to this central body. | 
boolean | 
TimeVaryingSolidTideModel.removeThirdBody(Point point)
Removes a tidal perturbations due to the body represented by the  
Point. | 
boolean | 
ThirdBodyGravity.removeThirdBody(Point point)
Removes a third body gravitational force represented by the  
Point. | 
void | 
GravityGradientTorque.setBodyCenterOfMass(Point value)
Sets the center of mass point of the gravity-gradient satellite. 
 | 
void | 
VestaCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
VenusCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
UranusCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
TritonCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
TitaniaCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
TitanCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
TethysCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
SunCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
SolarSystemBarycenter.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this solar system. 
 | 
void | 
SaturnCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
RheaCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
PlutoCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
PlanetarySystemBarycenter.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this planetary system. 
 | 
void | 
PhoebeCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
PhobosCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
NeptuneCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
MoonCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
MimasCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
MercuryCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
MarsCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
JupiterCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
IoCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
IapetusCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
HyperionCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
GanymedeCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
EuropaCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
EnceladusCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
EarthCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
DioneCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
DeimosCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
CharonCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
CeresCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
abstract void | 
CentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
CallistoCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
ArielCentralBody.setCenterOfMassPoint(Point value)
Sets a point describing the center of mass of this central body. 
 | 
void | 
ScalarVariableAreaArgumentLatitude.setIntegrationPoint(Point value)
Sets the  
Point used to determine the argument of latitude
    at a particular time. | 
void | 
TwoBodyGravity.setTargetPoint(Point value)
Sets the target point at which to measure the gravitational acceleration. 
 | 
void | 
ThirdBodyGravity.setTargetPoint(Point value)
Sets the target point at which the gravity is measured. 
 | 
void | 
SphericalHarmonicGravity.setTargetPoint(Point value)
Sets the target point at which to measure the gravitational acceleration. 
 | 
void | 
ScalarAtmosphericDensity.setTargetPoint(Point value)
Sets the target point describing the time-varying position at which density is
    to be calculated. 
 | 
void | 
IersTechnicalNote36RelativisticCorrectionForce.setTargetPoint(Point value)
Sets the point at which the  
IersTechnicalNote36RelativisticCorrectionForce is applied. | 
void | 
ScalarOccultation.setTargetPoint(Point value)
Sets the  
Point representing the location at which
    the occultation factor is being calculated. | 
void | 
MagneticFieldVector.setTargetPoint(Point value)
Sets the point where the magnetic field vector is calculated. 
 | 
void | 
EarthMoonBarycenter.updateEarthMoonBarycenterPoint(Point earthCenterOfMassPoint,
                              Point moonCenterOfMassPoint,
                              double earthMoonMassRatio)
Updates the  
CenterOfMassPoint (get / set) of this EarthMoonBarycenter
    instance using the Earth-Moon mass ratio and the positions of the Earth and Moon. | 
| Constructor and Description | 
|---|
GravityGradientTorque(Point bodyCenterOfMass,
                     CentralBody centralBody,
                     double gravitationalParameter,
                     Matrix3By3Symmetric inertiaMatrix,
                     Axes bodyAxes)
Initializes the gravity-gradient torque model. 
 | 
GravityGradientTorque(Point bodyCenterOfMass,
                     Matrix3By3Symmetric inertiaMatrix,
                     Axes bodyAxes)
Initializes the gravity-gradient torque model. 
 | 
IersTechnicalNote36RelativisticCorrectionForce(Point targetPoint)
Initializes the correction force with the specified  
Point. | 
IersTechnicalNote36RelativisticCorrectionForce(Point targetPoint,
                                              CentralBody centralBody,
                                              CentralBody solarCentralBody,
                                              Vector centralBodyAngularMomentumPerUnitMass,
                                              double centralBodyGravitationalParameter,
                                              double solarGravitationalParameter,
                                              boolean useLenseThirringCorrection,
                                              boolean useDeSitterCorrection)
Initializes the correction force with the specified parameters. 
 | 
InternationalGeomagneticReferenceFieldVector(TimeIntervalCollection1<SphericalHarmonicCoefficients> initialMagneticFieldCoefficients,
                                            TimeIntervalCollection1<SphericalHarmonicCoefficients> magneticFieldCoefficientRates,
                                            Point targetPoint)
Initializes a new instance. 
 | 
MagneticFieldVector(TimeIntervalCollection1<SphericalHarmonicCoefficients> initialMagneticFieldCoefficients,
                   TimeIntervalCollection1<SphericalHarmonicCoefficients> magneticFieldCoefficientRates,
                   Point targetPoint,
                   double referenceDistance)
Initializes a new instance. 
 | 
NPlateSolarRadiationForce(NPlateModel nPlateModel,
                         Axes bodyAxes,
                         Point targetPoint)
Initializes a  
ForceModel describing the solar radiation pressure force on an object. | 
ScalarAtmosphericDensity(Point targetPoint,
                        SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing atmospheric density using the target point
    and solar-geophysical data. | 
ScalarAtmosphericDensity(Point targetPoint,
                        SolarGeophysicalData solarGeophysicalData,
                        CentralBody centralBody,
                        Vector sunVector)
Initializes a  
Scalar representing atmospheric density using the target point
    and solar-geophysical data. | 
ScalarDensityJacchia1970(Point targetPoint,
                        SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing the Jacchia 1970 model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityJacchia1970(Point targetPoint,
                        SolarGeophysicalData solarGeophysicalData,
                        CentralBody earth,
                        Vector sunVector,
                        boolean useApproximateAltitude)
Initializes a  
Scalar representing the Jacchia 1970 model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityJacchiaRoberts(Point targetPoint,
                           SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing the Jacchia-Roberts model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityJacchiaRoberts(Point targetPoint,
                           SolarGeophysicalData solarGeophysicalData,
                           CentralBody earth,
                           Vector sunVector,
                           boolean useApproximateAltitude)
Initializes a  
Scalar representing the Jacchia-Roberts model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityMsis2000(Point targetPoint,
                     SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing the MSIS 2000 model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityMsis86(Point targetPoint,
                   SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing the MSIS 1986 model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarDensityMsis90(Point targetPoint,
                   SolarGeophysicalData solarGeophysicalData)
Initializes a  
Scalar representing the MSIS 1990 model
    of atmospheric density using the target point and solar-geophysical data. | 
ScalarOccultation(CentralBody illuminatingBody,
                 Point targetPoint,
                 CentralBody... occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultation(CentralBody illuminatingBody,
                 Point targetPoint,
                 Iterable<CentralBody> occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationCylindrical(CentralBody illuminatingBody,
                            Point targetPoint,
                            CentralBody... occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationCylindrical(CentralBody illuminatingBody,
                            Point targetPoint,
                            Iterable<CentralBody> occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationDualCone(CentralBody illuminatingBody,
                         Point targetPoint,
                         CentralBody... occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationDualCone(CentralBody illuminatingBody,
                         Point targetPoint,
                         Iterable<CentralBody> occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationNoShadow(CentralBody illuminatingBody,
                         Point targetPoint)
Initializes a new instance using the provided  
TargetPoint (get / set) and
    IlluminatingBody (get / set), which a SimpleSolarRadiationForce
    type will need to calculate the direction and magnitude of the un-occulted
    solar radiation. | 
ScalarOccultationRegulatedDualCone(CentralBody illuminatingBody,
                                  Point targetPoint,
                                  CentralBody... occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarOccultationRegulatedDualCone(CentralBody illuminatingBody,
                                  Point targetPoint,
                                  Iterable<CentralBody> occludingBodies)
Creates a new Scalar from the given illuminating body, target point, and occluding bodies. 
 | 
ScalarVariableAreaArgumentLatitude(int interpolationOrder,
                                  Map<Double,Double> areaData,
                                  Point integrationPoint,
                                  ReferenceFrame integrationFrame)
Initializes a new instance. 
 | 
SimpleSolarRadiationForce(Point targetPoint,
                         Scalar reflectivityCoefficient,
                         Scalar referenceArea)
Creates a instance based on the given target point and its coefficients. 
 | 
SphericalHarmonicGravity(Point targetPoint,
                        SphericalHarmonicGravityField field)
Initializes a new instance based on the given target point and gravity field data. 
 | 
ThirdBodyGravity(Point targetPoint)
Initializes a new instance based on the given target point. 
 | 
ThirdBodyInfo(String name,
             Point position,
             double gravitationalParameter)
Initializes a new instance. 
 | 
TwoBodyGravity(Point targetPoint)
Initializes a new instance based on the given target point. 
 | 
TwoBodyGravity(Point targetPoint,
              CentralBody centralBody,
              double gravitationalParameter)
Initializes a new instance based on the given target point and central body. 
 | 
WorldMagneticModelVector(TimeIntervalCollection1<SphericalHarmonicCoefficients> initialMagneticFieldCoefficients,
                        TimeIntervalCollection1<SphericalHarmonicCoefficients> magneticFieldCoefficientRates,
                        Point targetPoint)
Initializes a new instance. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
GraphicalVector.getLocationPoint()
Gets the point defining the tail end of the vector. 
 | 
Point | 
PointCesiumProperty.getPoint()
Gets the Point. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
GraphicalVector.setLocationPoint(Point value)
Sets the point defining the tail end of the vector. 
 | 
void | 
PointCesiumProperty.setPoint(Point value)
Sets the Point. 
 | 
static PointCesiumProperty | 
PointCesiumProperty.toPointCesiumProperty(Point value)
Converts a  
Point to a PointCesiumProperty. | 
| Constructor and Description | 
|---|
GraphicalVector(Vector vector,
               VectorGraphics vectorGraphics,
               Point locationPoint)
Initializes a new instance specifying all parameters. 
 | 
PointCesiumProperty(Point point)
Initializes a new instance with the provided  
Point. | 
| Constructor and Description | 
|---|
ComplexAnalogTransmitter(String name,
                        Point locationPoint,
                        Axes orientationAxes,
                        RadioFrequencyGainPattern antennaGainPattern,
                        Signal signalToTransmit)
Creates a new instance, specifying all parameters. 
 | 
ComplexAnalogTransmitter(String name,
                        Point locationPoint,
                        Axes orientationAxes,
                        RadioFrequencyGainPattern antennaGainPattern,
                        Signal signalToTransmit,
                        PolarizationSource polarizationSource)
Creates a new instance, specifying all parameters. 
 | 
ComplexAnalogTransmitter(String name,
                        Point locationPoint,
                        RadioFrequencyGainPattern antennaGainPattern,
                        Signal signalToTransmit)
 | 
ComplexDigitalTransmitter(String name,
                         Point locationPoint,
                         Axes orientationAxes,
                         DigitalModulation modulation,
                         RadioFrequencyGainPattern antennaGainPattern,
                         double carrierFrequency,
                         double power,
                         double dataRate,
                         SignalDataCollection signalData)
Creates a new instance from the specified parameters. 
 | 
ComplexDigitalTransmitter(String name,
                         Point locationPoint,
                         Axes orientationAxes,
                         DigitalModulation modulation,
                         RadioFrequencyGainPattern antennaGainPattern,
                         double carrierFrequency,
                         double power,
                         double dataRate,
                         SignalDataCollection signalData,
                         PolarizationSource polarizationSource)
Creates a new instance from the specified parameters. 
 | 
ComplexDigitalTransmitter(String name,
                         Point locationPoint,
                         DigitalModulation modulation,
                         RadioFrequencyGainPattern antennaGainPattern,
                         double carrierFrequency,
                         double power,
                         double dataRate,
                         SignalDataCollection signalData)
Creates a new instance from the specified parameters. 
 | 
ComplexReceiver(String name,
               Point location,
               Amplifier amplifier,
               RadioFrequencyGainPattern gainPattern)
Creates a new instance using the specified name, location, amplifier and gain pattern. 
 | 
ComplexReceiver(String name,
               Point location,
               Axes orientation,
               Amplifier amplifier,
               RadioFrequencyGainPattern gainPattern)
Creates a new instance specifying all parameters. 
 | 
ComplexReceiver(String name,
               Point location,
               Axes orientation,
               Amplifier amplifier,
               RadioFrequencyGainPattern gainPattern,
               PolarizationSource polarizationSource)
Creates a new instance specifying all parameters. 
 | 
OpticalReceiver(String name,
               Point location,
               Axes orientation,
               Photodetector photodetector,
               OpticalGainPattern gainPattern)
Creates a new instance specifying all parameters. 
 | 
OpticalReceiver(String name,
               Point location,
               Axes orientation,
               Photodetector photodetector,
               OpticalGainPattern gainPattern,
               PolarizationSource polarizationSource)
Creates a new instance specifying all parameters. 
 | 
OpticalReceiver(String name,
               Point location,
               Photodetector photodetector,
               OpticalGainPattern gainPattern)
Creates a new instance using the specified name, location, photodetector, and optical gain pattern. 
 | 
OpticalTransmitter(String name,
                  Point locationPoint,
                  Axes orientation,
                  DigitalModulation modulation,
                  OpticalGainPattern antennaGainPattern,
                  double wavelength,
                  double power,
                  double dataRate,
                  SignalDataCollection signalData)
Creates a new instance specifying all parameters. 
 | 
OpticalTransmitter(String name,
                  Point locationPoint,
                  Axes orientation,
                  DigitalModulation modulation,
                  OpticalGainPattern antennaGainPattern,
                  double wavelength,
                  double power,
                  double dataRate,
                  SignalDataCollection signalData,
                  PolarizationSource polarizationSource)
Creates a new instance specifying all parameters. 
 | 
OpticalTransmitter(String name,
                  Point locationPoint,
                  DigitalModulation modulation,
                  OpticalGainPattern antennaGainPattern,
                  double wavelength,
                  double power,
                  double dataRate,
                  SignalDataCollection signalData)
Creates a new instance specifying all parameters except the Axes. 
 | 
SimpleAnalogTransmitter(String name,
                       Point location,
                       Axes orientationAxes,
                       double carrierFrequency,
                       double effectiveIsotropicRadiatedPower,
                       double bandwidth)
Creates a new instance, specifying all parameters. 
 | 
SimpleAnalogTransmitter(String name,
                       Point location,
                       Axes orientationAxes,
                       double carrierFrequency,
                       double effectiveIsotropicRadiatedPower,
                       double bandwidth,
                       PolarizationSource polarizationSource)
Creates a new instance, specifying all parameters. 
 | 
SimpleAnalogTransmitter(String name,
                       Point locationPoint,
                       double carrierFrequency,
                       double effectiveIsotropicRadiatedPower,
                       double bandwidth)
Creates a new instance with the specified parameters. 
 | 
SimpleDigitalTransmitter(String name,
                        Point locationPoint,
                        Axes orientationAxes,
                        double carrierFrequency,
                        double effectiveIsotropicRadiatedPower,
                        double dataRate)
Creates a new instance from the specified parameters. 
 | 
SimpleDigitalTransmitter(String name,
                        Point locationPoint,
                        Axes orientationAxes,
                        double carrierFrequency,
                        double effectiveIsotropicRadiatedPower,
                        double dataRate,
                        PolarizationSource polarizationSource)
Creates a new instance from the specified parameters. 
 | 
SimpleDigitalTransmitter(String name,
                        Point locationPoint,
                        double carrierFrequency,
                        double effectiveIsotropicRadiatedPower,
                        double dataRate)
Creates a new instance from the specified parameters. 
 | 
SimpleReceiver(String name,
              Point locationPoint,
              Axes orientationAxes,
              double gain,
              double noiseFactor,
              double targetFrequency,
              double filterBandwidth)
Creates a new instance specifying all parameters. 
 | 
SimpleReceiver(String name,
              Point locationPoint,
              Axes orientationAxes,
              double gain,
              double noiseFactor,
              double targetFrequency,
              double filterBandwidth,
              PolarizationSource polarizationSource)
Creates a new instance specifying all parameters. 
 | 
SimpleReceiver(String name,
              Point locationPoint,
              double gain,
              double noiseFactor,
              double targetFrequency,
              double filterBandwidth)
Creates a new instance with the specified parameters. 
 | 
Transceiver(String name,
           Point inputAntennaLocationPoint,
           Axes inputAntennaOrientationAxes,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           Point outputAntennaLocationPoint,
           Axes outputAntennaOrientationAxes,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           DigitalModulation modulation,
           double gain,
           double noiseFactor,
           double carrierFrequency,
           SignalFilter filter)
Creates a new instance specifying all properties. 
 | 
Transceiver(String name,
           Point inputAntennaLocationPoint,
           Axes inputAntennaOrientationAxes,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           PolarizationSource inputPolarizationSource,
           Point outputAntennaLocationPoint,
           Axes outputAntennaOrientationAxes,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           PolarizationSource outputPolarizationSource,
           DigitalModulation modulation,
           double gain,
           double noiseFactor,
           double carrierFrequency,
           SignalFilter filter)
Creates a new instance specifying all properties. 
 | 
Transceiver(String name,
           Point inputAntennaLocationPoint,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           Point outputAntennaLocationPoint,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           DigitalModulation modulation,
           double gain,
           double noiseFactor,
           double carrierFrequency)
Creates a new instance using the specified properties. 
 | 
Transponder(String name,
           Point inputAntennaLocationPoint,
           Axes inputAntennaOrientationAxes,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           Point outputAntennaLocationPoint,
           Axes outputAntennaOrientationAxes,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           double gain,
           double noiseFactor,
           SignalFilter filter)
Creates a new instance specifying all properties. 
 | 
Transponder(String name,
           Point inputAntennaLocationPoint,
           Axes inputAntennaOrientationAxes,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           PolarizationSource inputPolarizationSource,
           Point outputAntennaLocationPoint,
           Axes outputAntennaOrientationAxes,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           PolarizationSource outputPolarizationSource,
           double gain,
           double noiseFactor,
           SignalFilter filter)
Creates a new instance specifying all properties. 
 | 
Transponder(String name,
           Point inputAntennaLocationPoint,
           RadioFrequencyGainPattern inputAntennaGainPattern,
           Point outputAntennaLocationPoint,
           RadioFrequencyGainPattern outputAntennaGainPattern,
           double gain,
           double noiseFactor)
Creates a new instance with the specified properties. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
ParameterizedTemporallyPartitionedCoverageDefinition.getGridPoint()
Gets a  
Point object that defines the location of any given grid point during the 
    coverage computation. | 
Point | 
ParameterizedSpatiallyPartitionedCoverageDefinition.getGridPoint()
Gets a  
Point object that defines the location of any given grid point during the 
    coverage computation. | 
| Modifier and Type | Method and Description | 
|---|---|
CoverageGridPointWithResults | 
CoverageResults.findNearestGridPoint(Point location,
                    JulianDate date)
Given a  
Point and a date, find the nearest grid point according to physical distance. | 
| Modifier and Type | Class and Description | 
|---|---|
class  | 
CompositePoint
A Point that is defined by a collection of intervals, where the data
 associated with each interval is a another Point representing the
 location for that interval. 
 | 
class  | 
EntityPoint<TEntity extends IEntityPosition>
A  
Point that obtains its value from a tracking entity implementing
 IEntityPosition. | 
class  | 
JplDECenterOfMassPoint
 | 
class  | 
ParameterizedOnEvaluatorPoint
A point that is defined by a  
PointEvaluatorParameter at the time of evaluation. | 
class  | 
ParameterizedOnStatePoint
A point that is defined by a  
TimeBasedStateParameter at the time of evaluation. | 
class  | 
ParameterizedPoint
A point that is defined by a  
CartesianParameter at the time of evaluation. | 
class  | 
PointAtAltitude
 | 
class  | 
PointCartographic
A point representing a fixed planetodetic location on a central body specified
 using  
Cartographic coordinates. | 
class  | 
PointCentralBodyProjection
 | 
class  | 
PointDifferentiator
A Point that can provide higher-order derivatives by finite-differencing another point. 
 | 
class  | 
PointFixedAtJulianDate
A  
Point which is defined by the instantaneous location of another point at a specified 
 JulianDate. | 
class  | 
PointFixedOffset
A Point whose position does not change with respect to the reference frame in which it is defined. 
 | 
class  | 
PointFromArchive<TEntity extends IEntityIdentifier & IEntityLastUpdate>
A  
Point whose position is defined by archived tracking data. | 
class  | 
PointInPointsFrame
A point observed in another point's reference frame. 
 | 
class  | 
PointInReferenceFrame
A time varying point observed in a particular reference frame. 
 | 
class  | 
PointInRegionNearestToReferencePoint
A  
Point that is within an EllipsoidSurfaceRegion that is closest to a reference point which may be found in, on,
 or outside of the region. | 
class  | 
PointInterpolator
A point with its position, velocity, etc. 
 | 
class  | 
PointPropagationParameter
 | 
class  | 
PointVectorToPoint
 | 
class  | 
ServiceProviderPoint
A Point that can be used to refer to the current  
LocationPoint (get) of an IServiceProvider,
 whatever it is at the time that this point is evaluated. | 
| Modifier and Type | Method and Description | 
|---|---|
static Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(EarthCentralBody earth,
            Point point,
            String toFrame)
Converts a  
Point such that an ITRF transformation is applied when it is evaluated. | 
static Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(EarthCentralBody earth,
            Point point,
            String toFrame,
            ArrayList<InternationalTerrestrialReferenceFrameTransformer> itrfList)
Converts a  
Point such that an ITRF transformation is applied when it is evaluated. | 
Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(ReferenceFrame fromFrame,
            Point point)
Converts a  
Point such that the ITRF transformation is applied when it is evaluated. | 
Point | 
PointVectorToPoint.getBasePoint()
 | 
Point | 
PointDifferentiator.getDifferentiatedPoint()
Gets the point whose highest order derivative is being differentiated 
 | 
Point | 
VectorDisplacement.getFinalPoint()
Gets the point which defines the ending of the displacement vector. 
 | 
Point | 
PointFixedAtJulianDate.getFixedPoint()
 | 
Point | 
PointInPointsFrame.getFrameOwner()
 | 
Point | 
ScalarDeltaSphericalElement.getFromPoint()
Gets the  
initial point to measure the angle from. | 
Point | 
VectorDisplacement.getInitialPoint()
Gets the point which defines the beginning of the displacement vector. 
 | 
Point | 
ILocationPointService.getLocationPoint()
Gets the point that describes the position of the object. 
 | 
Point | 
PointInReferenceFrame.getObservedPoint()
 | 
Point | 
PointInPointsFrame.getObservedPoint()
 | 
Point | 
VectorBPlane.getOrbitalPoint()
Gets the  
Point to use when computing this VectorBPlane. | 
Point | 
AxesBPlane.getOrbitalPoint()
Gets the  
Point to use when computing this VectorBPlane. | 
Point | 
ScalarModifiedKeplerianElement.getOrbitalPoint()
Gets the  
Point to compute. | 
Point | 
ScalarKozaiIzsakMeanElement.getOrbitalPoint()
Gets the  
Point to compute. | 
Point | 
ScalarEquinoctialElement.getOrbitalPoint()
Gets the  
Point to compute. | 
Point | 
ScalarDelaunayElement.getOrbitalPoint()
Gets the  
Point to compute. | 
Point | 
DynamicModifiedKeplerianElements.getOrbitalPoint()
Gets the  
Point to use to compute the elements. | 
Point | 
DynamicKozaiIzsakMeanElements.getOrbitalPoint()
Gets the  
Point to use to compute the elements. | 
Point | 
DynamicEquinoctialElements.getOrbitalPoint()
Gets the  
Point to use to compute the elements. | 
Point | 
DynamicDelaunayElements.getOrbitalPoint()
Gets the  
Point to use to compute the elements. | 
Point | 
PointCentralBodyProjection.getOrigin()
Gets the origin of the ray to project onto the central body. 
 | 
Point | 
ReferenceFrame.getOrigin()
Gets the origin of the reference frame. 
 | 
Point | 
AxesVehicleVelocityLocalHorizontal.getPoint()
Gets the point that defines this axes with its motion. 
 | 
Point | 
AxesLocalVerticalLocalHorizontal.getPoint()
Gets the point that defines this axes. 
 | 
Point | 
VectorVelocity.getPoint()
Gets the point. 
 | 
Point | 
VectorInPointsAxes.getPoint()
Gets the point. 
 | 
Point | 
VectorEllipsoidSurfaceNormal.getPoint()
Gets the point to be projected onto the ellipsoid surface. 
 | 
Point | 
VectorAcceleration.getPoint()
Gets the point. 
 | 
Point | 
AxesInPointsAxes.getPoint()
Gets the point. 
 | 
static Point | 
PointHelper.getPoint(IServiceProvider provider)
Gets the  
Point from the ILocationPointService provided by an object. | 
static Point | 
PointHelper.getPoint(IServiceProvider provider,
        String exceptionMessage)
Gets the  
Point from the ILocationPointService provided by an object. | 
Point | 
AxesFromBankAngle.getPosition()
Gets the  
Point representing the position of the platform and its derivatives. | 
Point | 
AxesAlongTerrain.getPosition()
 | 
Point | 
ScalarCartographicElement.getReferencePoint()
Gets the  
Point to use. | 
Point | 
PointInRegionNearestToReferencePoint.getReferencePoint()
Gets the point which is on, or will be projected on, the surface of the ellipsoid in which the region is defined. 
 | 
Point | 
PointAtAltitude.getReferencePoint()
Gets the  
Point to use. | 
Point | 
AxesVelocityOrbitNormal.getReferencePoint()
Gets the  
Point used to construct these axes. | 
Point | 
AxesNorthEastDown.getReferencePoint()
Gets the reference point that defines the axes. 
 | 
Point | 
AxesEastNorthUp.getReferencePoint()
Gets the reference point that defines the axes. 
 | 
Point | 
ScalarSphericalElement.getReferencePoint()
 | 
Point | 
ScalarPointElement.getReferencePoint()
Gets the  
Point to use. | 
static Point | 
Point.getRoot()
Gets the root point, which is not defined in terms of any reference frame. 
 | 
Point | 
ScalarDeltaSphericalElement.getToPoint()
Gets the other  
Point to compute the multi-body value with. | 
Point | 
ScalarDeltaSphericalElement.getVertex()
 | 
static Point | 
GeometryTransformer.Advanced.unwrap(Point point)
 | 
| Modifier and Type | Method and Description | 
|---|---|
TimeIntervalCollection1<Point> | 
CompositePoint.getIntervals()
Gets the collection of intervals where the data for a given interval represents the Point for that time. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
protected boolean | 
PointFromArchive.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
EntityPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointPropagationParameter.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointInRegionNearestToReferencePoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointCentralBodyProjection.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointCartographic.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointAtAltitude.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
JplDECenterOfMassPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
ServiceProviderPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointVectorToPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointInterpolator.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointInReferenceFrame.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointInPointsFrame.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointFixedOffset.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointFixedAtJulianDate.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
PointDifferentiator.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected abstract boolean | 
Point.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
ParameterizedPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
ParameterizedOnStatePoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
ParameterizedOnEvaluatorPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
protected boolean | 
CompositePoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
static Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(EarthCentralBody earth,
            Point point,
            String toFrame)
Converts a  
Point such that an ITRF transformation is applied when it is evaluated. | 
static Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(EarthCentralBody earth,
            Point point,
            String toFrame,
            ArrayList<InternationalTerrestrialReferenceFrameTransformer> itrfList)
Converts a  
Point such that an ITRF transformation is applied when it is evaluated. | 
Point | 
InternationalTerrestrialReferenceFrameTransformer.convertPoint(ReferenceFrame fromFrame,
            Point point)
Converts a  
Point such that the ITRF transformation is applied when it is evaluated. | 
static AxesEvaluator | 
GeometryTransformer.Advanced.getTransformationFromPointsAxes(Point fromPoint,
                               Axes to)
Gets an evaluator that can be used to find the transformation from the axes in which a point is defined to a given axes. 
 | 
static AxesEvaluator | 
GeometryTransformer.Advanced.getTransformationFromPointsAxes(Point fromPoint,
                               Axes to,
                               EvaluatorGroup group)
Gets an evaluator that can be used to find the transformation from the axes in which a point is defined to a given axes. 
 | 
static PointEvaluator | 
GeometryTransformer.observePoint(Point point,
            ReferenceFrame inFrame)
Gets an evaluator that can be used to find the  
Motion<Cartesian>
    of this point in the new Frame (get / set) at a given JulianDate. | 
static PointEvaluator | 
GeometryTransformer.observePoint(Point point,
            ReferenceFrame inFrame,
            EvaluatorGroup group)
Gets an evaluator that can be used to find the  
Motion<Cartesian>
    of this point in the new Frame (get / set) at a given JulianDate. | 
static PointEvaluator | 
GeometryTransformer.Advanced.observePointInOtherPointsFrame(Point pointToObserve,
                              Point frameOwner)
Gets an evaluator that can be used to observe the  
Motion<Cartesian>
        of a point at a given JulianDate in the reference frame in which another point is defined. | 
static PointEvaluator | 
GeometryTransformer.Advanced.observePointInOtherPointsFrame(Point pointToObserve,
                              Point frameOwner,
                              EvaluatorGroup group)
Gets an evaluator that can be used to observe the  
Motion<Cartesian>
        of a point at a given JulianDate in the reference frame in which another point is defined. | 
static VectorEvaluator | 
GeometryTransformer.Advanced.observeVectorInPointsAxes(Vector vector,
                         Point point)
 | 
static VectorEvaluator | 
GeometryTransformer.Advanced.observeVectorInPointsAxes(Vector vector,
                         Point point,
                         EvaluatorGroup group)
 | 
void | 
PointVectorToPoint.setBasePoint(Point value)
 | 
void | 
PointDifferentiator.setDifferentiatedPoint(Point value)
Sets the point whose highest order derivative is being differentiated 
 | 
void | 
VectorDisplacement.setFinalPoint(Point value)
Sets the point which defines the ending of the displacement vector. 
 | 
void | 
PointFixedAtJulianDate.setFixedPoint(Point value)
 | 
void | 
PointInPointsFrame.setFrameOwner(Point value)
 | 
void | 
ScalarDeltaSphericalElement.setFromPoint(Point value)
Sets the  
initial point to measure the angle from. | 
void | 
VectorDisplacement.setInitialPoint(Point value)
Sets the point which defines the beginning of the displacement vector. 
 | 
void | 
PointInReferenceFrame.setObservedPoint(Point value)
 | 
void | 
PointInPointsFrame.setObservedPoint(Point value)
 | 
void | 
VectorBPlane.setOrbitalPoint(Point value)
Sets the  
Point to use when computing this VectorBPlane. | 
void | 
AxesBPlane.setOrbitalPoint(Point value)
Sets the  
Point to use when computing this VectorBPlane. | 
void | 
ScalarModifiedKeplerianElement.setOrbitalPoint(Point value)
Sets the  
Point to compute. | 
void | 
ScalarKozaiIzsakMeanElement.setOrbitalPoint(Point value)
Sets the  
Point to compute. | 
void | 
ScalarEquinoctialElement.setOrbitalPoint(Point value)
Sets the  
Point to compute. | 
void | 
ScalarDelaunayElement.setOrbitalPoint(Point value)
Sets the  
Point to compute. | 
void | 
DynamicModifiedKeplerianElements.setOrbitalPoint(Point value)
Sets the  
Point to use to compute the elements. | 
void | 
DynamicKozaiIzsakMeanElements.setOrbitalPoint(Point value)
Sets the  
Point to use to compute the elements. | 
void | 
DynamicEquinoctialElements.setOrbitalPoint(Point value)
Sets the  
Point to use to compute the elements. | 
void | 
DynamicDelaunayElements.setOrbitalPoint(Point value)
Sets the  
Point to use to compute the elements. | 
void | 
PointCentralBodyProjection.setOrigin(Point value)
Sets the origin of the ray to project onto the central body. 
 | 
void | 
ReferenceFrame.setOrigin(Point value)
Sets the origin of the reference frame. 
 | 
void | 
AxesVehicleVelocityLocalHorizontal.setPoint(Point value)
Sets the point that defines this axes with its motion. 
 | 
void | 
AxesLocalVerticalLocalHorizontal.setPoint(Point value)
Sets the point that defines this axes. 
 | 
void | 
VectorVelocity.setPoint(Point value)
Sets the point. 
 | 
void | 
VectorInPointsAxes.setPoint(Point value)
Sets the point. 
 | 
void | 
VectorEllipsoidSurfaceNormal.setPoint(Point value)
Sets the point to be projected onto the ellipsoid surface. 
 | 
void | 
VectorAcceleration.setPoint(Point value)
Sets the point. 
 | 
void | 
AxesInPointsAxes.setPoint(Point value)
Sets the point. 
 | 
void | 
AxesFromBankAngle.setPosition(Point value)
Sets the  
Point representing the position of the platform and its derivatives. | 
void | 
AxesAlongTerrain.setPosition(Point value)
 | 
void | 
ScalarCartographicElement.setReferencePoint(Point value)
Sets the  
Point to use. | 
void | 
PointInRegionNearestToReferencePoint.setReferencePoint(Point value)
Sets the point which is on, or will be projected on, the surface of the ellipsoid in which the region is defined. 
 | 
void | 
PointAtAltitude.setReferencePoint(Point value)
Sets the  
Point to use. | 
void | 
AxesVelocityOrbitNormal.setReferencePoint(Point value)
Sets the  
Point used to construct these axes. | 
void | 
AxesNorthEastDown.setReferencePoint(Point value)
Sets the reference point that defines the axes. 
 | 
void | 
AxesEastNorthUp.setReferencePoint(Point value)
Sets the reference point that defines the axes. 
 | 
void | 
ScalarSphericalElement.setReferencePoint(Point value)
 | 
void | 
ScalarPointElement.setReferencePoint(Point value)
Sets the  
Point to use. | 
void | 
ScalarDeltaSphericalElement.setToPoint(Point value)
Sets the other  
Point to compute the multi-body value with. | 
void | 
ScalarDeltaSphericalElement.setVertex(Point value)
 | 
static Point | 
GeometryTransformer.Advanced.unwrap(Point point)
 | 
| Constructor and Description | 
|---|
AxesAlongTerrain(Point referencePoint,
                TerrainProvider terrain)
Create a new instance based on the given point and terrain provider. 
 | 
AxesBPlane(Point location,
          CentralBody centralBody,
          double gravitationalParameter)
Initializes a new instance. 
 | 
AxesBPlane(Point location,
          CentralBody centralBody,
          double gravitationalParameter,
          ReferenceFrame parentReferenceFrame)
Initializes a new instance. 
 | 
AxesEastNorthUp(CentralBody centralBody,
               Point referencePoint)
Initializes a new instance. 
 | 
AxesFromBankAngle(Point position,
                 CentralBody centralBody,
                 double surfaceGravity,
                 List<JulianDate> specialTimes,
                 double targetRollRate)
Create a new instance based on the given point and special times of interest. 
 | 
AxesInPointsAxes(Axes axesToObserve,
                Point point)
Initializes a new instance. 
 | 
AxesLocalVerticalLocalHorizontal(ReferenceFrame frame,
                                Point point)
Initializes a new instance with the specified parameters. 
 | 
AxesNorthEastDown(CentralBody centralBody,
                 Point referencePoint)
Initializes a new instance. 
 | 
AxesVehicleVelocityLocalHorizontal(ReferenceFrame referenceFrame,
                                  Point point)
Initializes a new instance with the specified parameters. 
 | 
AxesVelocityOrbitNormal(Point point)
Initializes a new instance. 
 | 
AxesVelocityOrbitNormal(Point point,
                       CentralBody centralBody)
Initializes a new instance. 
 | 
DynamicDelaunayElements(Point location,
                       double gravitationalParameter,
                       ReferenceFrame frame)
Initializes a new instance. 
 | 
DynamicEquinoctialElements(Point location,
                          double gravitationalParameter,
                          ReferenceFrame frame)
Initializes a new instance. 
 | 
DynamicKozaiIzsakMeanElements(Point location,
                             double gravitationalParameter,
                             ReferenceFrame frame,
                             double j2UnnormalizedValue,
                             double referenceDistance)
Initializes a new instance. 
 | 
DynamicModifiedKeplerianElements(Point location,
                                double gravitationalParameter,
                                ReferenceFrame frame)
Initializes a new instance. 
 | 
Point(Point existingInstance,
     CopyContext context)
Initializes a new instance as a copy of an existing instance. 
 | 
PointAtAltitude(Point referencePoint,
               CentralBody centralBody,
               Scalar altitude)
Initializes a new instance from a reference point, body, and altitude scalar. 
 | 
PointCentralBodyProjection(CentralBody centralBody,
                          Point origin,
                          Vector direction)
Initializes a new instance from a body, a ray origin, and a ray direction. 
 | 
PointDifferentiator(Point differentiatedPoint,
                   double increment)
Initializes a new instance. 
 | 
PointDifferentiator(Point differentiatedPoint,
                   double increment,
                   int derivativeToCompute)
Initializes a new instance. 
 | 
PointFixedAtJulianDate(Point fixedPoint,
                      ReferenceFrame fixedWithRespectTo,
                      ValueDefinition<JulianDate> fixedAt)
Initializes a new instance. 
 | 
PointFixedAtJulianDate(Point fixedPoint,
                      ValueDefinition<JulianDate> fixedAt)
Initializes a new instance. 
 | 
PointInPointsFrame(Point observedPoint,
                  Point frameOwner)
Initializes a new instance. 
 | 
PointInReferenceFrame(Point point,
                     ReferenceFrame frame)
Initializes a new instance. 
 | 
PointInRegionNearestToReferencePoint(CentralBody centralBody,
                                    Point referencePoint,
                                    EllipsoidSurfaceRegion surfaceRegion)
Initializes an instance with the specified parameters. 
 | 
PointInRegionNearestToReferencePoint(CentralBody centralBody,
                                    Point referencePoint,
                                    IGetEllipsoidSurfaceRegion surfaceRegionInterface)
Initializes an instance with the specified parameters. 
 | 
PointInRegionNearestToReferencePoint(Point referencePoint,
                                    EllipsoidSurfaceRegion surfaceRegion)
 | 
PointVectorToPoint(Vector displacementVector,
                  Point basePoint)
Initializes a new instance. 
 | 
ReferenceFrame(Point origin,
              Axes axes)
Initializes a new instance with the specified origin and axes. 
 | 
ScalarCartographicElement(CentralBody centralBody,
                         Point point,
                         CartographicElement element)
Initializes a new instance. 
 | 
ScalarDelaunayElement(double gravitationalParameter,
                     Point location,
                     DelaunayElement element,
                     ReferenceFrame frame)
Initializes a new instance. 
 | 
ScalarDeltaSphericalElement(Point satellitePoint,
                           CentralBody primaryCentralBody,
                           CentralBody otherCentralBody,
                           SphericalElement element)
Initializes a new instance. 
 | 
ScalarDeltaSphericalElement(Point fromPoint,
                           Point vertex,
                           Point toPoint,
                           ReferenceFrame frame,
                           SphericalElement element)
Initializes a new instance. 
 | 
ScalarEquinoctialElement(double gravitationalParameter,
                        Point location,
                        EquinoctialElement element,
                        ReferenceFrame frame)
Initializes a new instance. 
 | 
ScalarKozaiIzsakMeanElement(double gravitationalParameter,
                           Point location,
                           KozaiIzsakMeanElement element,
                           ReferenceFrame frame,
                           double j2UnnormalizedValue,
                           double referenceDistance)
Initializes a new instance. 
 | 
ScalarModifiedKeplerianElement(double gravitationalParameter,
                              Point location,
                              KeplerianElement element,
                              ReferenceFrame frame)
Initializes a new instance. 
 | 
ScalarPointElement(Point location,
                  CartesianElement element,
                  ReferenceFrame frameOfPoint)
Initializes a new instance. 
 | 
ScalarSphericalElement(Point location,
                      ReferenceFrame frame,
                      SphericalElement element)
Initializes a new instance. 
 | 
VectorAcceleration(Point point,
                  ReferenceFrame referenceFrame)
Initializes a new instance of the  
VectorAcceleration class to represent the
    acceleration of a given point in a given reference frame. | 
VectorApparentDisplacement(Point initialPoint,
                          Point finalPoint,
                          ReferenceFrame inertialFrame)
Initializes a new instance of the  
VectorApparentDisplacement class which only accounts for light travel time. | 
VectorApparentDisplacement(Point initialPoint,
                          Point finalPoint,
                          ReferenceFrame inertialFrame,
                          SignalDirection direction,
                          double lightTravelTimeConvergenceTolerance)
Initializes a new instance of the  
VectorApparentDisplacement class which only accounts for light travel time. | 
VectorApparentDisplacement(Point initialPoint,
                          Point finalPoint,
                          ReferenceFrame inertialFrame,
                          SignalDirection direction,
                          double lightTravelTimeConvergenceTolerance,
                          VectorVelocity velocityOfMovingFrame)
Initializes a new instance of the  
VectorApparentDisplacement class which accounts for aberration in addition to light travel time. | 
VectorApparentDisplacement(Point initialPoint,
                          Point finalPoint,
                          ReferenceFrame inertialFrame,
                          VectorVelocity velocityOfMovingFrame)
Initializes a new instance of the  
VectorApparentDisplacement class which accounts for aberration in addition to light travel time. | 
VectorBPlane(Point location,
            CentralBody centralBody,
            double gravitationalParameter)
Initializes a new instance. 
 | 
VectorBPlane(Point location,
            CentralBody centralBody,
            double gravitationalParameter,
            ReferenceFrame parentReferenceFrame)
Initializes a new instance. 
 | 
VectorDisplacement(Point initialPoint,
                  Point finalPoint)
Initializes a new instance. 
 | 
VectorEllipsoidSurfaceNormal(Ellipsoid ellipsoid,
                            ReferenceFrame ellipsoidFixedFrame,
                            Point point)
Initializes a new instance. 
 | 
VectorInPointsAxes(Vector vectorToObserve,
                  Point point)
Initializes an instance. 
 | 
VectorTrueDisplacement(Point initialPoint,
                      Point finalPoint)
Initializes a new instance of the  
VectorTrueDisplacement class using the provided points. | 
VectorVelocity(Point point,
              ReferenceFrame frame)
Initializes a new instance of the  
VectorVelocity class to represent the
    velocity of a given point in a given reference frame. | 
| Constructor and Description | 
|---|
CompositePoint(TimeIntervalCollection1<Point> intervals)
Initializes a new instance with the provided intervals. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
CoverageGridPoint.getPosition()
Gets the point representing this grid point. 
 | 
| Constructor and Description | 
|---|
CoverageGridPoint(Point position,
                 Scalar weight,
                 ICoverageGridCell coverageGridCell,
                 ReferenceFrame referenceFrame)
Creates a new instance based on the given point, weight, grid cell, and reference frame. 
 | 
CoverageGridPoint(Point position,
                 Scalar weight,
                 ICoverageGridCell coverageGridCell,
                 ReferenceFrame referenceFrame,
                 CentralBody centralBody)
Creates a new instance based on the given point, weight, grid cell, central body, and reference frame. 
 | 
CoverageGridPoint(Point position,
                 Scalar weight,
                 ReferenceFrame referenceFrame)
Creates a new instance based on the given point, weight, and reference frame. 
 | 
CoverageGridPoint(Point position,
                 Scalar weight,
                 ReferenceFrame referenceFrame,
                 CentralBody centralBody)
Creates a new instance based on the given point, weight, central body, and reference frame. 
 | 
| Constructor and Description | 
|---|
SpecifiedCoverageGrid(ReferenceFrame referenceFrame,
                     List<Point> gridPoints,
                     List<Scalar> weights)
Initializes the grid with the specified parameters. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
Camera.view(Axes axes,
    Point cameraPosition,
    Point referencePoint)
Views from a point to a point. 
 | 
void | 
Camera.view(Axes axes,
    Point cameraPosition,
    Point referencePoint,
    UnitCartesian upAxis)
Views from a point to a point. 
 | 
void | 
Camera.viewCentralBody(CentralBody centralBody,
               Axes axes,
               Point cameraPosition)
Zoom to a central body and use the specified axes for rotation. 
 | 
void | 
Camera.viewDirection(Axes axes,
             Point cameraPosition,
             Vector direction)
Views from a point to a direction. 
 | 
void | 
Camera.viewDirection(Axes axes,
             Point cameraPosition,
             Vector direction,
             UnitCartesian upAxis)
Views from a point to a direction. 
 | 
void | 
Camera.viewOffset(Axes axes,
          Point referencePoint,
          Cartesian offset)
Sets the camera's reference point - the point the camera is looking at. 
 | 
void | 
Camera.viewOffset(Axes axes,
          Point referencePoint,
          Cartesian offset,
          UnitCartesian upAxis)
Sets the camera's reference point - the point the camera is looking at. 
 | 
void | 
Camera.viewOffsetDirection(Axes axes,
                   Point referencePoint,
                   Vector direction)
Sets the camera's reference point - the point the camera is looking at. 
 | 
void | 
Camera.viewOffsetDirection(Axes axes,
                   Point referencePoint,
                   Vector direction,
                   UnitCartesian upAxis)
Sets the camera's reference point - the point the camera is looking at. 
 | 
| Constructor and Description | 
|---|
GpsLineOfSightVector(Point initialPoint,
                    Point finalPoint)
Initializes a new instance. 
 | 
| Constructor and Description | 
|---|
GpsCommunicationsFrontEnd(PlatformCollection gpsConstellation,
                         GpsSignalConfiguration signalConfiguration,
                         Point location,
                         Axes orientation)
Creates a front end for a  
GpsReceiver that can be used to model communications between GPS satellites and 
    the GpsReceiver, using a predefined receiver signal configuration. | 
GpsCommunicationsFrontEnd(PlatformCollection gpsConstellation,
                         NavigationSignalCollection signalsToTrack,
                         List<SignalPropagationModel> signalPropagationModels,
                         Point location,
                         Axes orientation)
Creates a front end for a  
GpsReceiver that can be used to model communications between GPS satellites and 
    the GpsReceiver. | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
SP3aEphemeris.createPoint(int prn)
Creates a point based on the  
PointInterpolator using the ECEF coordinate frame and the default
    TranslationalMotionInterpolator. | 
| Modifier and Type | Class and Description | 
|---|---|
class  | 
PlatformLocationPoint
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
Platform.getLocationPoint()
Gets the time-varying location of this platform. 
 | 
Point | 
LocationPointExtension.getLocationPoint()
Gets the point that describes the position of the object. 
 | 
Point | 
GraphicalVector.getLocationPoint()
Gets the point defining the the tail end of the vector. 
 | 
Point | 
PointGraphicsParameter.getPoint()
 | 
| Modifier and Type | Method and Description | 
|---|---|
protected boolean | 
PlatformLocationPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
Evaluator<Boolean> | 
IFieldOfViewEnclosureService.getPointIsInFieldOfViewEvaluator(Point point)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
Evaluator<Boolean> | 
FieldOfViewExtension.getPointIsInFieldOfViewEvaluator(Point point)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
Evaluator<Boolean> | 
DynamicFieldOfViewExtension.getPointIsInFieldOfViewEvaluator(Point point)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
Evaluator<Boolean> | 
IFieldOfViewEnclosureService.getPointIsInFieldOfViewEvaluator(Point point,
                                EvaluatorGroup group)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
Evaluator<Boolean> | 
FieldOfViewExtension.getPointIsInFieldOfViewEvaluator(Point point,
                                EvaluatorGroup group)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
Evaluator<Boolean> | 
DynamicFieldOfViewExtension.getPointIsInFieldOfViewEvaluator(Point point,
                                EvaluatorGroup group)
Gets an evaluator to determine if a point is inside the field of view of the sensor at
    different dates. 
 | 
void | 
Platform.setLocationPoint(Point value)
Sets the time-varying location of this platform. 
 | 
void | 
LocationPointExtension.setLocationPoint(Point value)
Sets the point that describes the position of the object. 
 | 
void | 
GraphicalVector.setLocationPoint(Point value)
Sets the point defining the the tail end of the vector. 
 | 
void | 
PointGraphicsParameter.setPoint(Point value)
 | 
| Constructor and Description | 
|---|
GraphicalVector(Vector vector,
               Point locationPoint,
               VectorGraphics graphics)
Initializes a new instance specifying all parameters. 
 | 
LocationPointExtension(Point locationPoint)
Initialize the extension with the given point. 
 | 
Platform(String name,
        Point locationPoint,
        Axes orientationAxes)
Initializes a new instance with a specified name, time-varying position, and time-varying orientation. 
 | 
PointGraphicsParameter(Point point,
                      ReferenceFrame inFrame)
Initializes a new instance with the specified point and frame. 
 | 
| Modifier and Type | Class and Description | 
|---|---|
class  | 
PropagatorPoint
A point with its location computed by a propagator. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
PropagationNewtonianPoint.getIntegrationPoint()
Gets a  
Point which is parameterized on the position and velocity in the state during integration. | 
Point | 
SinglePointStoppablePropagatorDefinition.getPropagationPoint()
Gets the  
Point to use in other geometry types that depend on the
    propagation of this propagator, such as in StoppingConditions
    that depend on geometry types. | 
| Modifier and Type | Method and Description | 
|---|---|
protected boolean | 
PropagatorPoint.checkForSameDefinition(Point other)
Checks to determine if another instance has the same definition as this instance and
    returns  
true if it does. | 
| Modifier and Type | Method and Description | 
|---|---|
abstract Point | 
PropagationPointElement.getIntegrationPoint()
Gets the  
Point of the integrated position. | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
PropagatedRoute.createPointFromRoute()
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
ImpulsiveManeuverInformation.getPropagationPoint()
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
Jup365BspEphemerisProvider.getAdrasteaPoint()
 | 
Point | 
Jup365BspEphemerisProvider.getAmaltheaPoint()
 | 
Point | 
UranusBspEphemerisProvider.getArielPoint()
 | 
Point | 
JupiterBspEphemerisProvider.getCallistoPoint()
 | 
Point | 
Sat441BspEphemerisProvider.getCalypsoPoint()
 | 
Point | 
CeresBspEphemerisProvider.getCeresPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getCeresPoint()
Gets a point representing the location of Ceres. 
 | 
Point | 
PlutoBspEphemerisProvider.getCharonPoint()
 | 
Point | 
MarsBspEphemerisProvider.getDeimosPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getDidymosPoint()
Gets a point representing the location of Didymos. 
 | 
Point | 
SaturnBspEphemerisProvider.getDionePoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getDonaldJohansonPoint()
Gets a point representing the location of DonaldJohanson. 
 | 
Point | 
PlanetsBspEphemerisProvider.getEarthMoonBarycenter()
Gets a point representing the location of the barycenter
    of the Earth-Moon system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getEarthPoint()
Gets a point representing the location of Earth. 
 | 
Point | 
SaturnBspEphemerisProvider.getEnceladusPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getErosPoint()
Gets a point representing the location of Eros. 
 | 
Point | 
JupiterBspEphemerisProvider.getEuropaPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getEurybatesPoint()
Gets a point representing the location of Eurybates. 
 | 
Point | 
JupiterBspEphemerisProvider.getGanymedePoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getGasparaPoint()
Gets a point representing the location of Gaspara. 
 | 
Point | 
Sat441BspEphemerisProvider.getHelenePoint()
 | 
Point | 
Plu058BspEphemerisProvider.getHydraPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getHyperionPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getIapetusPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getIdaPoint()
Gets a point representing the location of Ida. 
 | 
Point | 
JupiterBspEphemerisProvider.getIoPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getItokawaPoint()
Gets a point representing the location of Itokawa. 
 | 
Point | 
PlanetsBspEphemerisProvider.getJupiterPoint()
Gets a point representing the location of Jupiter. 
 | 
Point | 
Jup365BspEphemerisProvider.getJupiterPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getJupiterSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Jupiter system. 
 | 
Point | 
JupiterBspEphemerisProvider.getJupiterSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Jupiter planetary system. 
 | 
Point | 
Jup365BspEphemerisProvider.getJupiterSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Jupiter planetary system. 
 | 
Point | 
Plu058BspEphemerisProvider.getKerberosPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getLeucusPoint()
Gets a point representing the location of Leucus. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getLutetiaPoint()
Gets a point representing the location of Lutetia. 
 | 
Point | 
PlanetsBspEphemerisProvider.getMarsPoint()
Gets a point representing the location of Mars (which
    is identical to the position of the Mars system
    barycenter in this model). 
 | 
Point | 
MarsBspEphemerisProvider.getMarsPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getMarsSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Mars system. 
 | 
Point | 
MarsBspEphemerisProvider.getMarsSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Mars planetary system. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getMathildePoint()
Gets a point representing the location of Mathilde. 
 | 
Point | 
PlanetsBspEphemerisProvider.getMercuryPoint()
Gets a point representing the location of Mercury. 
 | 
Point | 
Sat441BspEphemerisProvider.getMethonePoint()
 | 
Point | 
Jup365BspEphemerisProvider.getMetisPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getMimasPoint()
 | 
Point | 
Ura111BspEphemerisProvider.getMirandaPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getMoonPoint()
Gets a point representing the location of the Moon. 
 | 
Point | 
PlanetsBspEphemerisProvider.getNeptunePoint()
Gets a point representing the location of Neptune. 
 | 
Point | 
Nep097BspEphemerisProvider.getNeptunePoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getNeptuneSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Neptune system. 
 | 
Point | 
NeptuneBspEphemerisProvider.getNeptuneSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Neptune planetary system. 
 | 
Point | 
Nep097BspEphemerisProvider.getNeptuneSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Neptune planetary system. 
 | 
Point | 
Plu058BspEphemerisProvider.getNixPoint()
 | 
Point | 
Ura111BspEphemerisProvider.getOberonPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getOrusPoint()
Gets a point representing the location of Orus. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getPatroclusPoint()
Gets a point representing the location of Patroclus. 
 | 
Point | 
MarsBspEphemerisProvider.getPhobosPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getPhoebePoint()
 | 
Point | 
Plu058BspEphemerisProvider.getPlutoPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getPlutoPoint()
Gets a point representing the location of Pluto. 
 | 
Point | 
PlutoBspEphemerisProvider.getPlutoSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Pluto planetary system. 
 | 
Point | 
Plu058BspEphemerisProvider.getPlutoSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Pluto planetary system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getPlutoSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Pluto system. 
 | 
Point | 
Sat441BspEphemerisProvider.getPolydeucesPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getPolymelePoint()
Gets a point representing the location of Polymele. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getPsychePoint()
Gets a point representing the location of Psyche. 
 | 
Point | 
SaturnBspEphemerisProvider.getRheaPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getRyuguPoint()
Gets a point representing the location of Ryugu. 
 | 
Point | 
Sat441BspEphemerisProvider.getSaturnPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getSaturnPoint()
Gets a point representing the location of Saturn. 
 | 
Point | 
SaturnBspEphemerisProvider.getSaturnSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Saturn planetary system. 
 | 
Point | 
Sat441BspEphemerisProvider.getSaturnSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Saturn planetary system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getSaturnSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Saturn system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getSolarSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Solar System. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getSolarSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Solar System. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getSteinsPoint()
Gets a point representing the location of Steins. 
 | 
Point | 
Plu058BspEphemerisProvider.getStyxPoint()
 | 
Point | 
VestaBspEphemerisProvider.getSunPoint()
Gets a point representing the location of the Sun. 
 | 
Point | 
PlanetsBspEphemerisProvider.getSunPoint()
Gets a point representing the location of the Sun. 
 | 
Point | 
CeresBspEphemerisProvider.getSunPoint()
Gets a point representing the location of the Sun. 
 | 
Point | 
JplSpkFile.getTargetPoint(int naifIdOfTargetPoint,
              int naifIdOfCenterPoint,
              Point centerPoint)
Gets a point describing the position of a target location with respect
    to a center location. 
 | 
Point | 
JplSpkFile.getTargetPoint(IProvideNaifIdCode targetPointProvider,
              IProvideNaifIdCode centerPointProvider)
    Gets a point describing the position of a target location with respect
    to a center location. 
 | 
Point | 
JplSpkFile.getTargetPoint(IProvideNaifIdCode targetPointProvider,
              IProvideNaifIdCode centerPointProvider,
              Point centerPoint)
Gets a point describing the position of a target location with respect
    to a center location. 
 | 
Point | 
Sat441BspEphemerisProvider.getTelestoPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getTethysPoint()
 | 
Point | 
Jup365BspEphemerisProvider.getThebePoint()
 | 
Point | 
UranusBspEphemerisProvider.getTitaniaPoint()
 | 
Point | 
SaturnBspEphemerisProvider.getTitanPoint()
 | 
Point | 
NeptuneBspEphemerisProvider.getTritonPoint()
 | 
Point | 
Ura111BspEphemerisProvider.getUmbrielPoint()
 | 
Point | 
Ura111BspEphemerisProvider.getUranusPoint()
 | 
Point | 
PlanetsBspEphemerisProvider.getUranusPoint()
Gets a point representing the location of Uranus. 
 | 
Point | 
UranusBspEphemerisProvider.getUranusSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Uranus planetary system. 
 | 
Point | 
Ura111BspEphemerisProvider.getUranusSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Uranus planetary system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getUranusSystemBarycenter()
Gets a point representing the location of the barycenter
    of the Uranus system. 
 | 
Point | 
PlanetsBspEphemerisProvider.getVenusPoint()
Gets a point representing the location of Venus. 
 | 
Point | 
VestaBspEphemerisProvider.getVestaPoint()
 | 
Point | 
AsteroidsBspEphemerisProvider.getVestaPoint()
Gets a point representing the location of Vesta. 
 | 
Point | 
AsteroidsBspEphemerisProvider.getVirginiaPoint()
Gets a point representing the location of the asteroid Virginia. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
JplSpkFile.getTargetPoint(int naifIdOfTargetPoint,
              int naifIdOfCenterPoint,
              Point centerPoint)
Gets a point describing the position of a target location with respect
    to a center location. 
 | 
Point | 
JplSpkFile.getTargetPoint(IProvideNaifIdCode targetPointProvider,
              IProvideNaifIdCode centerPointProvider,
              Point centerPoint)
Gets a point describing the position of a target location with respect
    to a center location. 
 | 
void | 
JupiterBspEphemerisProvider.setJupiterSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Jupiter planetary system. 
 | 
void | 
Jup365BspEphemerisProvider.setJupiterSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Jupiter planetary system. 
 | 
void | 
MarsBspEphemerisProvider.setMarsSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Mars planetary system. 
 | 
void | 
NeptuneBspEphemerisProvider.setNeptuneSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Neptune planetary system. 
 | 
void | 
Nep097BspEphemerisProvider.setNeptuneSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Neptune planetary system. 
 | 
void | 
PlutoBspEphemerisProvider.setPlutoSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Pluto planetary system. 
 | 
void | 
Plu058BspEphemerisProvider.setPlutoSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Pluto planetary system. 
 | 
void | 
SaturnBspEphemerisProvider.setSaturnSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Saturn planetary system. 
 | 
void | 
Sat441BspEphemerisProvider.setSaturnSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Saturn planetary system. 
 | 
void | 
VestaBspEphemerisProvider.setSunPoint(Point value)
Sets a point representing the location of the Sun. 
 | 
void | 
CeresBspEphemerisProvider.setSunPoint(Point value)
Sets a point representing the location of the Sun. 
 | 
void | 
UranusBspEphemerisProvider.setUranusSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Uranus planetary system. 
 | 
void | 
Ura111BspEphemerisProvider.setUranusSystemBarycenter(Point value)
Sets a point representing the location of the barycenter
    of the Uranus planetary system. 
 | 
| Constructor and Description | 
|---|
CeresBspEphemerisProvider(JplSpkFile file,
                         Point sunPoint)
Initializes an instance using the specified  
JplSpkFile instance. | 
CeresBspEphemerisProvider(StreamFactory streamFactory,
                         Point sunPoint)
Initializes a new instance with the specified stream factory. 
 | 
CeresBspEphemerisProvider(String filename,
                         Point sunPoint)
Initializes an instance using the specified ceres.bsp filename. 
 | 
Jup365BspEphemerisProvider(JplSpkFile file,
                          Point jupiterSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
Jup365BspEphemerisProvider(StreamFactory streamFactory,
                          Point jupiterSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
Jup365BspEphemerisProvider(String filename,
                          Point jupiterSystemBarycenter)
Initializes an instance using the specified jup365.bsp filename. 
 | 
JupiterBspEphemerisProvider(JplSpkFile file,
                           Point jupiterSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
JupiterBspEphemerisProvider(StreamFactory streamFactory,
                           Point jupiterSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
JupiterBspEphemerisProvider(String filename,
                           Point jupiterSystemBarycenter)
Initializes an instance using the specified jupiter.bsp filename. 
 | 
MarsBspEphemerisProvider(JplSpkFile file,
                        Point marsSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
MarsBspEphemerisProvider(StreamFactory streamFactory,
                        Point marsSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
MarsBspEphemerisProvider(String filename,
                        Point marsSystemBarycenter)
Initializes an instance using the specified mars.bsp filename. 
 | 
Nep097BspEphemerisProvider(JplSpkFile file,
                          Point neptuneSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
Nep097BspEphemerisProvider(StreamFactory streamFactory,
                          Point neptuneSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
Nep097BspEphemerisProvider(String filename,
                          Point neptuneSystemBarycenter)
Initializes an instance using the specified nep097.bsp filename. 
 | 
NeptuneBspEphemerisProvider(JplSpkFile file,
                           Point neptuneSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
NeptuneBspEphemerisProvider(StreamFactory streamFactory,
                           Point neptuneSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
NeptuneBspEphemerisProvider(String filename,
                           Point neptuneSystemBarycenter)
Initializes an instance using the specified neptune.bsp filename. 
 | 
Plu058BspEphemerisProvider(JplSpkFile file,
                          Point plutoSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
Plu058BspEphemerisProvider(StreamFactory streamFactory,
                          Point plutoSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
Plu058BspEphemerisProvider(String filename,
                          Point plutoSystemBarycenter)
Initializes an instance using the specified plu058.bsp filename. 
 | 
PlutoBspEphemerisProvider(JplSpkFile file,
                         Point plutoSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
PlutoBspEphemerisProvider(StreamFactory streamFactory,
                         Point plutoSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
PlutoBspEphemerisProvider(String filename,
                         Point plutoSystemBarycenter)
Initializes an instance using the specified pluto.bsp filename. 
 | 
Sat441BspEphemerisProvider(JplSpkFile file,
                          Point saturnSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
Sat441BspEphemerisProvider(StreamFactory streamFactory,
                          Point saturnSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
Sat441BspEphemerisProvider(String filename,
                          Point saturnSystemBarycenter)
Initializes an instance using the specified sat441.bsp filename. 
 | 
SaturnBspEphemerisProvider(JplSpkFile file,
                          Point saturnSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
SaturnBspEphemerisProvider(StreamFactory streamFactory,
                          Point saturnSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
SaturnBspEphemerisProvider(String filename,
                          Point saturnSystemBarycenter)
Initializes an instance using the specified saturn.bsp filename. 
 | 
Ura111BspEphemerisProvider(JplSpkFile file,
                          Point uranusSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
Ura111BspEphemerisProvider(StreamFactory streamFactory,
                          Point uranusSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
Ura111BspEphemerisProvider(String filename,
                          Point uranusSystemBarycenter)
Initializes an instance using the specified ura111.bsp filename. 
 | 
UranusBspEphemerisProvider(JplSpkFile file,
                          Point uranusSystemBarycenter)
Initializes an instance using the specified  
JplSpkFile instance. | 
UranusBspEphemerisProvider(StreamFactory streamFactory,
                          Point uranusSystemBarycenter)
Initializes a new instance with the specified stream factory. 
 | 
UranusBspEphemerisProvider(String filename,
                          Point uranusSystemBarycenter)
Initializes an instance using the specified uranus.bsp filename. 
 | 
VestaBspEphemerisProvider(JplSpkFile file,
                         Point sunPoint)
Initializes an instance using the specified  
JplSpkFile instance. | 
VestaBspEphemerisProvider(StreamFactory streamFactory,
                         Point sunPoint)
Initializes a new instance with the specified stream factory. 
 | 
VestaBspEphemerisProvider(String filename,
                         Point sunPoint)
Initializes an instance using the specified vesta.bsp filename. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
StkEphemerisFile.createPoint()
Creates a  
Point whose time-varying position is computed by interpolating
    over the ephemeris data held by this instance. | 
abstract Point | 
StkEphemerisFile.Ephemeris.createPoint()
Creates a  
Point whose time-varying position is computed by interpolating
        over the ephemeris data held by this instance. | 
Point | 
StkEphemerisFile.EphemerisTimePos.createPoint()
Creates a  
Point whose time-varying position is computed by interpolating
        over the ephemeris data held by this instance. | 
Point | 
StkEphemerisFile.EphemerisLLATimePos.createPoint()
Creates a  
Point whose time-varying position is computed by interpolating
        over the ephemeris data held by this instance. | 
Point | 
StkEphemerisFile.EphemerisLLRTimePos.createPoint()
Creates a  
Point whose time-varying position is computed by interpolating
        over the ephemeris data held by this instance. | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
StkEphemerisFile.configureFromPoint(Point point,
                  JulianDate start,
                  JulianDate stop,
                  Duration step,
                  int order)
Configures this instance with values computed by sampling a  
Point over an interval with
    a fixed step. | 
| Modifier and Type | Method and Description | 
|---|---|
Point | 
ViewFromTo.getFromPoint()
Gets the Point whose position will be used to place the camera or null if an entity is being used. 
 | 
Point | 
ViewFromTo.getToPoint()
Gets the Point whose position will be used to aim the camera or null if an entity is being used. 
 | 
| Modifier and Type | Method and Description | 
|---|---|
void | 
ViewFromTo.setFrom(Point point)
Specifies a  
Point which will be used to place the camera. | 
void | 
ViewFromTo.setTo(Point point)
Specifies the  
Point at which the camera will be aimed. | 
| Constructor and Description | 
|---|
ViewFromTo(TypeLiteral<TEntity> typeLiteralTEntity,
          Camera camera,
          Point fromPoint,
          Point toPoint)
 | 
ViewFromTo(TypeLiteral<TEntity> typeLiteralTEntity,
          Camera camera,
          Point fromPoint,
          TEntity toEntity)
 | 
ViewFromTo(TypeLiteral<TEntity> typeLiteralTEntity,
          Camera camera,
          TEntity fromEntity,
          Point toPoint)
 |