Package | Description |
---|---|
org.orekit.bodies |
This package provides interface to represent the position and geometry of
space objects such as stars, planets or asteroids.
|
org.orekit.files.ccsds |
This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
|
org.orekit.files.general |
This package provides interfaces for orbit file representations and corresponding
parsers.
|
org.orekit.forces.gravity |
This package provides all gravity-related forces.
|
org.orekit.propagation.semianalytical.dsst.forces |
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
|
Modifier and Type | Method and Description |
---|---|
static CelestialBody |
CelestialBodyFactory.getBody(String name)
Get a celestial body.
|
static CelestialBody |
CelestialBodyFactory.getEarth()
Get the Earth singleton body.
|
static CelestialBody |
CelestialBodyFactory.getEarthMoonBarycenter()
Get the Earth-Moon barycenter singleton bodies pair.
|
static CelestialBody |
CelestialBodyFactory.getJupiter()
Get the Jupiter singleton body.
|
static CelestialBody |
CelestialBodyFactory.getMars()
Get the Mars singleton body.
|
static CelestialBody |
CelestialBodyFactory.getMercury()
Get the Mercury singleton body.
|
static CelestialBody |
CelestialBodyFactory.getMoon()
Get the Moon singleton body.
|
static CelestialBody |
CelestialBodyFactory.getNeptune()
Get the Neptune singleton body.
|
static CelestialBody |
CelestialBodyFactory.getPluto()
Get the Pluto singleton body.
|
static CelestialBody |
CelestialBodyFactory.getSaturn()
Get the Saturn singleton body.
|
static CelestialBody |
CelestialBodyFactory.getSolarSystemBarycenter()
Get the solar system barycenter aggregated body.
|
static CelestialBody |
CelestialBodyFactory.getSun()
Get the Sun singleton body.
|
static CelestialBody |
CelestialBodyFactory.getUranus()
Get the Uranus singleton body.
|
static CelestialBody |
CelestialBodyFactory.getVenus()
Get the Venus singleton body.
|
CelestialBody |
CelestialBodyLoader.loadCelestialBody(String name)
Load celestial body.
|
CelestialBody |
JPLEphemeridesLoader.loadCelestialBody(String name)
Load celestial body.
|
Modifier and Type | Method and Description |
---|---|
abstract CelestialBody |
CenterName.getCelestialBody()
Get the celestial body corresponding to the CCSDS constant.
|
CelestialBody |
ODMMetaData.getCenterBody()
Get the
CelestialBody corresponding to the center name. |
Modifier and Type | Method and Description |
---|---|
OrekitEphemerisFile.OrekitEphemerisSegment |
OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states,
CelestialBody body,
int interpolationSampleSize)
Injects pre-computed satellite states into this ephemeris file
object, returning the generated
OrekitEphemerisFile.OrekitEphemerisSegment that
has been stored internally. |
Constructor and Description |
---|
SolidTides(Frame centralBodyFrame,
double ae,
double mu,
TideSystem centralTideSystem,
boolean poleTide,
double step,
int nbPoints,
IERSConventions conventions,
UT1Scale ut1,
CelestialBody... bodies)
Simple constructor.
|
SolidTides(Frame centralBodyFrame,
double ae,
double mu,
TideSystem centralTideSystem,
IERSConventions conventions,
UT1Scale ut1,
CelestialBody... bodies)
Simple constructor.
|
ThirdBodyAttraction(CelestialBody body)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
CelestialBody |
DSSTThirdBody.getBody()
Get third body.
|
Constructor and Description |
---|
DSSTThirdBody(CelestialBody body)
Complete constructor.
|
Copyright © 2002-2017 CS Systèmes d'information. All rights reserved.