See: Description
| Interface | Description |
|---|---|
| CentralBodyInertialAxes.ComputeOrientationParameters.Function |
A functional interface for the containing delegate type.
|
| ComputeIauOrientationParameters.Function |
A functional interface for the containing delegate type.
|
| IJplDEWithMoonLibrationModel |
A
JplDE which can return a libration model for the Moon. |
| Class | Description |
|---|---|
| ArielCentralBody |
The Uranian moon Ariel.
|
| AtmosphericDragForce |
A simple model of atmospheric drag on a body according to its coefficient of drag and reference cross-sectional area.
|
| AtmosphericRefractionModel |
Defines a refraction model.
|
| CallistoCentralBody |
The Jovian moon Callisto.
|
| CentralBodiesFacet |
A
CalculationContextFacet that holds and provides information about
central bodies such as planets, moons, the sun, etc. |
| CentralBody |
A central body, such as a planet, star, asteroid, libration point, etc.
|
| CentralBodyInertialAxes |
This class provides the Axes based on the STK definition of a
CentralBody's Inertial Axes. |
| CentralBodyInertialAxes.ComputeOrientationParameters |
The definition of a function which computes a set of orientation parameters.
|
| CentralBodyIntersection |
A utility for checking for orbit intersection with a planet given two-body dynamics.
|
| CeresCentralBody |
The dwarf planet Ceres.
|
| CharonCentralBody |
The Plutonian moon Charon.
|
| ClassicalEquationOfEquinoxes |
Represents the classical equation of the equinox as defined in the Explanatory Supplement
to the Astronomical Almanac.
|
| ComputeIauOrientationParameters |
The definition of a function which computes a set of orientation parameters.
|
| ConstantForce |
Represents a constant force.
|
| ConstantSolarGeophysicalData |
Represents the solar radiation and geomagnetic flux indices as constant values.
|
| ConstantTorque |
Represents a constant torque.
|
| ConstantWindModel |
Represents a constant wind speed and direction.
|
| ContinuousThrustForceModel |
Represents a force generated by continuous thrust.
|
| CssiSolarGeophysicalData |
Represents the solar radiation and geomagnetic flux indices as they vary over time.
|
| DawnCeresVestaOrientation |
This is a collection of the orientation information available for Ceres and Vesta.
|
| DeimosCentralBody |
The Martian moon Deimos.
|
| DioneCentralBody |
The Saturnian moon Dione.
|
| DragBodyPlate |
A model of a discrete surface element of a spacecraft's body that has a surface area, unit normal direction,
and a drag coefficient.
|
| DragOneDofSolarPanelPlate |
A model of a discrete surface element of a spacecraft's solar panels that points
toward the Sun as much as it can while being constrained by a single rotational
degree of freedom about a specified rotation axis.
|
| DragPlate |
A model of a discrete surface element of a spacecraft that has a surface area, unit normal direction,
and a drag coefficient.
|
| DragTwoDofSolarPanelPlate |
A model of a discrete surface element of a spacecraft's solar panels that always points toward the Sun.
|
| EarthCentralBody |
The planet Earth.
|
| EarthGravitationalModel1996 |
Provides the semimajor axis, gravitational parameter, and 2nd, 3rd, 4th, and 5th zonal harmonic coefficients
for the Earth Gravitational Model of 1996 (EGM96) according to NASA Technical Publication 1998-206861.
|
| EarthGravitationalModel2008 |
Provides the semimajor axis, gravitational parameter, and 2nd, 3rd, 4th, and 5th zonal harmonic coefficients
for the Earth Gravitational Model of 2008 (EGM2008) according to the Journal of Geophysical Research, Vol 117, Issue B4, April 2012.
|
| EarthMoonBarycenter |
The barycenter of the Earth-Moon system.
|
| EarthOrientationParameters |
Specifies Earth polar motion coordinates and the difference between UT1 and UTC.
|
| EarthOrientationParametersData |
Specifies Earth Orientation Parameters at a specific instant.
|
| EarthOrientationParametersFile |
Contains static methods to read EOP data in the Celestrak EOP data file format which is documented at
https://celestrak.com/SpaceData/EOP-format.asp.
|
| EarthOrientationParametersReadOptions |
Specifies options for reading an
EarthOrientationParametersFile. |
| EffectiveRadiusAtmosphericRefractionModel |
The effective radius model approximates the effects of refraction by assuming that the refractive index decreases linearly with altitude.
|
| EnceladusCentralBody |
The Saturnian moon Enceladus.
|
| EquationOfEquinoxes |
Represents the equation of the equinox (also called the "nutation in right ascension" according
to the Explanatory Supplement to the Astronomical Almanac) which defines the right ascension of
the mean equinox with respect to the true equator and equinox.
|
| EuropaCentralBody |
The Jovian moon Europa.
|
| ForceEvaluator |
Base class for evaluators created by a
ForceModel to compute the force. |
| ForceModel |
Represents a Newtonian force which can be used to specify the equations
of motion for a mass body located by a
PropagationNewtonianPoint. |
| GanymedeCentralBody |
The Jovian moon Ganymede.
|
| GravityGradientTorque |
Represents the gravity-gradient torque effects on a satellite parameterized by
a
PropagationNewtonianPoint and a PropagationEulerianAxes. |
| HyperionCentralBody |
The Saturnian moon Hyperion.
|
| IapetusCentralBody |
The Saturnian moon Iapetus.
|
| Iau1976Precession |
Provides Earth precession information according to the IAU 1976 model
|
| Iau1980Nutation |
Provides Earth Nutation information according to the IAU 1980 model
|
| Iau2000Orientation |
This is a collection of the orientation information available for central bodies.
|
| Iau2006Orientation |
This is a collection of the orientation information available for central bodies.
|
| Iau2006XysData |
A table of IAU2006 XYS data that is used to evaluate the transformation between the International Celestial
Reference Frame (ICRF) and the International Terrestrial Reference Frame (ITRF).
|
| Iau2009Orientation |
This is a collection of the orientation information available for central bodies.
|
| Iau2015Orientation |
This is a collection of the orientation information available for central bodies.
|
| IauOrientationAxes |
The Axes representing the orientation of a
CentralBody as represented by the data
from the IAU/IAG Working Group reports on rotational elements expressed in the
InertialFrame (get / set)Axes (get / set) of the SolarSystemBarycenter. |
| IauOrientationParameters |
A structure containing the orientation data computed at a particular time.
|
| Iers2003SolidTideModel |
A high-fidelity, time-varying Earth solid tide model that is based on the IERS Conventions (2003) technical report 32.
|
| IersTechnicalNote21 |
Provides Earth orientation parameters according to the IERS Technical Note 21.
|
| IersTechnicalNote36RelativisticCorrectionForce |
A
KindOfForce.NEWTONIAN_SPECIFIC_FORCE that models the first order correction to the acceleration of a space object about a CentralBody (get / set). |
| IndividualPlateModel |
A model of a discrete surface element of a spacecraft that has a surface area, unit normal direction,
and drag or reflectivity coefficients.
|
| InternationalGeomagneticReferenceFieldVector | |
| IoCentralBody |
The Jovian moon Io.
|
| ItuRP834Version4AtmosphericRefractionModel |
ITU-R P.834-4 is the ITU recommendation concerning "Effects of tropospheric refraction on radio wave propagation."
The recommendation provides an analytical formula for the refracted elevation at the ground.
|
| JovianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of some of the Jovian moons computed using a
J4Propagator with gravitational terms provided by the
comments file
for the jup365 ephemeris file. |
| JplDE |
The common base for classes for loading and accessing JPL DE files.
|
| JplDE200 |
Represents JPL DE200 ephemeris data.
|
| JplDE403 |
Represents JPL DE403 ephemeris data.
|
| JplDE405 |
Represents JPL DE405 ephemeris data.
|
| JplDE421 |
Represents JPL DE421 ephemeris data.
|
| JplDE430 |
Represents JPL DE430 ephemeris data.
|
| JplDE440 |
Represents JPL DE440 ephemeris data.
|
| JplDEFile |
Provides raw access to a JPL DE file.
|
| JplDEFileEvaluator |
The class returned by
JplDEFile.getEvaluator(JplDEDataIndex,EvaluatorGroup) to allow calculation of
time-varying information in the JPL DE file. |
| JupiterCentralBody |
The planet Jupiter.
|
| JupiterSystemBarycenter |
The barycenter of the Jupiter system.
|
| LibrationModel |
A model of the libration of a central body.
|
| LinkRefracted | |
| MagneticCoilTorque |
Represents the torque effects of a magnetic field vector on a magnetic torquer coil
implemented on a spacecraft parameterized by a
PropagationEulerianAxes. |
| MagneticFieldVector | |
| MarsCentralBody |
The planet Mars.
|
| MarsSystemBarycenter |
The barycenter of the Mars system.
|
| MartianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of the Martian moons computed using a
J4Propagator with gravitational terms provided by the
comments file
for the mar097 ephemeris file. |
| MercuryCentralBody |
The planet Mercury.
|
| MimasCentralBody |
The Saturnian moon Mimas.
|
| MoonCentralBody |
The moon of the Earth.
|
| NeptuneCentralBody |
The planet Neptune.
|
| NeptuneSystemBarycenter |
The barycenter of the Neptune system.
|
| NeptunianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of one of the Neptunian moons computed using a
J4Propagator with gravitational terms provided by the
comments file
for the nep097 ephemeris file. |
| NPlateAtmosphericDragForce |
A medium-fidelity force model for atmospheric drag on a spacecraft.
|
| NPlateModel |
A collection that models the spacecraft's body as a collection of individual plates
with surface areas, body-fixed directions, and drag or reflectivity coefficients.
|
| NPlateSolarRadiationForce |
A medium-fidelity force model for solar radiation pressure on a spacecraft.
|
| Nutation |
Holds nutation angles in longitude and in obliquity.
|
| NutationModel |
A model of the nutation of a central body.
|
| OffAxisTorque |
Represents the torque effects of a thruster that is not aligned with the center of mass of a
a vehicle parameterized by a
PropagationEulerianAxes. |
| PermanentSolidTideModel |
A constant solid tide model that can add permanent tides to a tide-free model to form a zero-tide model.
|
| PhobosCentralBody |
The Martian moon Phobos.
|
| PhoebeCentralBody |
The Saturnian moon Phoebe.
|
| PlanetarySystemBarycenter |
The barycenter of a planetary system.
|
| PlutoCentralBody |
The dwarf planet Pluto.
|
| PlutonianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of one of the Plutonian moons computed using a
TwoBodyPropagator with gravitational parameter provided by the
comments file
of the plu043 ephemeris file. |
| PlutoSystemBarycenter |
The barycenter of the Pluto system.
|
| Precession |
Holds precession angles.
|
| PrecessionModel |
A model of the precession of a central body.
|
| ReactionWheelTorque |
Represents the torque effects of a reaction wheel implemented on
a spacecraft parameterized by a
PropagationEulerianAxes. |
| ResultantForceBuilder |
A tool used by
ForceModel objects to add their RoleOfForce.PRINCIPAL and
RoleOfForce.PERTURBATION forces to a list of forces in a resultant force. |
| ResultantTorqueBuilder |
A tool used by
TorqueModel objects to add to a list of torques in a resultant torque. |
| RheaCentralBody |
The Saturnian moon Rhea.
|
| SaturnCentralBody |
The planet Saturn.
|
| SaturnianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of some of the Saturnian moons computed using a
J4Propagator with gravitational terms provided by the
comments file
of the sat441 ephemeris file. |
| SaturnSystemBarycenter |
The barycenter of the Saturn system.
|
| ScalarAtmosphericDensity |
Abstract base class for all atmospheric models used to calculate density.
|
| ScalarDensityJacchia1970 |
Calculates atmospheric density according to the Jacchia 1970 model.
|
| ScalarDensityJacchiaRoberts |
Calculates atmospheric density according to the Jacchia-Roberts model.
|
| ScalarDensityMsis2000 |
Calculates atmospheric density according to the NRLMSISE 2000 model.
|
| ScalarDensityMsis86 |
Calculates atmospheric density according to the MSIS 1986 model.
|
| ScalarDensityMsis90 |
Calculates atmospheric density according to the MSIS 1990 model.
|
| ScalarOccultation |
A class that provides evaluators for percentage of occultation/eclipse at a position, as well as
EclipseType. |
| ScalarOccultationCylindrical |
Provides evaluators for percentage of occultation/eclipse at a position,
as well as
EclipseType using the cylindrical shadow model. |
| ScalarOccultationDualCone |
Provides evaluators for percentage of occultation/eclipse at a position,
as well as
EclipseType using the dual cone shadow model. |
| ScalarOccultationNoShadow |
This is a
ScalarOccultation for use with SimpleSolarRadiationForce. |
| ScalarOccultationRegulatedDualCone |
Provides evaluators for percentage of occultation/eclipse at a position,
as well as
EclipseType using the dual cone shadow model. |
| ScalarVariableArea |
A
Scalar that enables interpolation of spacecraft area data from .dat files to use
as a reference area for AtmosphericDragForce and SimpleSolarRadiationForce. |
| ScalarVariableAreaArgumentLatitude |
A
Scalar that enables interpolation of spacecraft area data to use
as a reference area for AtmosphericDragForce and SimpleSolarRadiationForce. |
| ScalarVariableAreaJulianDate |
A
Scalar that enables interpolation of spacecraft area data to use
as a reference area for AtmosphericDragForce and SimpleSolarRadiationForce. |
| Simon1994PlanetaryPositions |
Provides
Point instances representing the positions of the planets computed using the
equations described in
Simon J.L., Bretagnon P., Chapront J., Chapront-Touze M., Francou G., Laskar J.,
1994, A&A 282, 663-683. |
| SimpleSolarRadiationForce |
Represents the acceleration from solar radiation pressure exerted on the given reflective area at the target position.
|
| SimpleSolidTideModel |
A simplified, time-varying solid tide model.
|
| SmallSolarSystemBodyAnalyticEphemeris |
Provides
Point instances representing the positions of a selection of dwarf planets and
other small solar system bodies based on the osculating orbital elements defined at reference epochs
by the Small-Body Database
maintained by the Solar System Dynamics group of JPL. |
| SolarGeophysicalData |
This class holds information on the F10.7 solar flux and the kp and ap geomagnetic flux.
|
| SolarRadiationBodyPlate |
A model of a discrete surface element of a spacecraft's body that has a surface area, unit normal direction,
a specular reflectivity coefficient, and a diffuse reflectivity coefficient.
|
| SolarRadiationBoundaryMitigation |
Corrects for eclipse crossings during satellite propagation.
|
| SolarRadiationOneDofSolarPanelPlate |
A model of a discrete surface element of a spacecraft's solar panels that points
toward the Sun as much as it can while being constrained by a single rotational
degree of freedom about a specified rotation axis.
|
| SolarRadiationPlate |
A model of a discrete surface element of a spacecraft that has a surface area, unit normal direction,
a specular reflectivity coefficient, and a diffuse reflectivity coefficient.
|
| SolarRadiationTwoDofSolarPanelPlate |
A model of a discrete surface element of a spacecraft's solar panels that always points toward the Sun.
|
| SolarSystemBarycenter |
The barycenter of a solar system.
|
| SolidTideModel |
A solid tide model that could be permanent or time-varying.
|
| SpaceControlFacilityAtmosphericRefractionModel |
The Satellite Control Facility (SCF) refraction model is based upon the paper "Refraction Correction, 'RC, Refraction Addition, 'RA, Milestone 4, Model 15.3A" by A.
|
| SphericalHarmonicCoefficients |
Contains the coefficient data for a spherical harmonic model.
|
| SphericalHarmonicGravity |
Represents the acceleration (force for a given unit mass) at a particular point
from the gravitational effects of the distribution of the Earth's mass.
|
| SphericalHarmonicGravityField |
The immutable class that describes the chosen subset and configuration
of spherical harmonic gravitational model.
|
| SphericalHarmonicGravityModel |
Contains the coefficient data for a gravity model, either specified upon construction or
read in from a file.
|
| SphericalHarmonicGravitySecularVariations |
A linear model for the secular variations of a gravity model.
|
| SunCentralBody |
The star at the center of our solar system.
|
| TethysCentralBody |
The Saturnian moon Tethys.
|
| ThirdBodyGravity |
Represents the gravitational acceleration created by bodies other than the central body around
which a target object is orbiting.
|
| ThirdBodyGravity.ThirdBodyInfo |
A combination of the position and gravitational parameter for a perturbing gravitational body.
|
| TimeVaryingSolidTideModel |
A solid tide model that must vary with time.
|
| TitanCentralBody |
The Saturnian moon Titan.
|
| TitaniaCentralBody |
The Uranian moon Titania.
|
| TorqueEvaluator |
Base class for evaluators created by a
TorqueModel to compute the torque. |
| TorqueModel |
Represents a torque which can be used to specify the equations
of rotational motion for a rigid-body parameterized by a
PropagationEulerianAxes. |
| TritonCentralBody |
The Neptunian moon Triton.
|
| TwoBodyGravity |
Represents the acceleration from a simple two body gravity model.
|
| UranianMoonsAnalyticEphemeris |
Provides
Point instances representing the positions of some of the Uranian moons computed using a
J4Propagator with gravitational terms provided by the
comments file
of the ura111 ephemeris file. |
| UranusCentralBody |
The planet Uranus.
|
| UranusSystemBarycenter |
The barycenter of the Uranus system.
|
| USStandardAtmosphere1976 |
Provides scalars that calculate values using the U.S.
|
| USStandardAtmosphere1976.Result |
The result of the calculation.
|
| VectorRefractedDisplacement |
A vector representing the refracted displacement from an initial point to a final point as
both points move over time.
|
| VenusCentralBody |
The planet Venus.
|
| VestaCentralBody |
The asteroid Vesta.
|
| WindModel |
Defines a wind model for an atmosphere.
|
| WorldGeodeticSystem1984 |
Provides the set of four World Geodetic System of 1984, WGS84 (G873), defining constants according
to Table 3.1 on page 3-5 of the National Imagery and Mapping Agency Technical Report TR8350.2,
Third Edition, Amendment 1, 3 January 2000.
|
| WorldMagneticModelVector |
| Enum | Description |
|---|---|
| CoefficientOfReflectivityType |
Defines the type of Reflectivity Coefficient used in initializing
SimpleSolarRadiationForce. |
| EclipseType |
Enumerates the different types of shadowing that can occur during an eclipse.
|
| JplDECentralBody |
The central bodies referenced in a JPL DE file.
|
| JplDEDataIndex |
Indices of the data available in a JPL DE file.
|
| KindOfForce |
Indicates the properties of a given force to be used when
distinguishing the behavior of forces when defining equations of motion.
|
| RadiationVectorType |
Defines the type of vector to use between the target and the illuminating body in context of scalar occultation.
|
| RoleOfForce |
An indication of how important a given force is in the overall composite force
acting on a given object.
|