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.orbits |
This package provides classes to represent orbits.
|
org.orekit.propagation.numerical.cr3bp |
Top level package for CR3BP Models used with a numerical propagator.
|
Modifier and Type | Method and Description |
---|---|
static CR3BPSystem |
CR3BPFactory.getEarthMoonCR3BP()
Get the Earth-Moon CR3BP singleton bodies pair.
|
static CR3BPSystem |
CR3BPFactory.getSunEarthCR3BP()
Get the Sun-Earth CR3BP singleton bodies pair.
|
static CR3BPSystem |
CR3BPFactory.getSunJupiterCR3BP()
Get the Sun-Jupiter CR3BP singleton bodies pair.
|
static CR3BPSystem |
CR3BPFactory.getSystem(CelestialBody primaryBody,
CelestialBody secondaryBody,
double a)
Get the corresponding CR3BP System.
|
Modifier and Type | Method and Description |
---|---|
CR3BPSystem |
RichardsonExpansion.getCr3bpSystem()
Get the considered CR3BP system.
|
Constructor and Description |
---|
CR3BPDifferentialCorrection(PVCoordinates firstguess,
CR3BPSystem syst,
double orbitalPeriod)
Simple Constructor.
|
CR3BPDifferentialCorrection(PVCoordinates firstguess,
CR3BPSystem syst,
double orbitalPeriod,
AttitudeProvider attitudeProvider,
TimeScale utc)
Simple Constructor.
|
HaloOrbit(CR3BPSystem syst,
PVCoordinates pv,
double orbitalPeriod)
Simple Constructor.
|
LibrationOrbit(CR3BPSystem system,
PVCoordinates initialPV,
double orbitalPeriod)
Constructor.
|
LyapunovOrbit(CR3BPSystem syst,
PVCoordinates pv,
double orbitalPeriod)
Simple Constructor.
|
RichardsonExpansion(CR3BPSystem cr3bpSystem,
LagrangianPoints point)
Simple Constructor.
|
Constructor and Description |
---|
CR3BPForceModel(CR3BPSystem cr3bp)
Simple constructor.
|
STMEquations(CR3BPSystem syst)
Simple constructor.
|
Copyright © 2002-2020 CS GROUP. All rights reserved.