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.frames |
This package provides classes to handle frames and transforms between them.
|
org.orekit.propagation.semianalytical.dsst.forces |
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
|
Modifier and Type | Method | 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 | 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 | 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 | 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.
|
Constructor | Description |
---|---|
L1Frame(CelestialBody primaryBody,
CelestialBody secondaryBody) |
Simple constructor.
|
L1TransformProvider(CelestialBody primaryBody,
CelestialBody secondaryBody) |
Simple constructor.
|
L2Frame(CelestialBody primaryBody,
CelestialBody secondaryBody) |
Simple constructor.
|
Modifier and Type | Method | Description |
---|---|---|
CelestialBody |
DSSTThirdBody.getBody() |
Get third body.
|
Constructor | Description |
---|---|
DSSTThirdBody(CelestialBody body) |
Complete constructor.
|
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