|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Orbit/LowEnergyManeuver
% Plot the Low Energy Transfer
Plot the Low Energy Transfer for a 4 body problem in a Non-Rotating Frame as
well as in a Sun-Earth Rotating Frame
--------------------------------------------------------------------------
Form:
h = PlotLET(elements,dV1Eph,det,h)
--------------------------------------------------------------------------
------
Inputs
------
elements (1,6) Ecliptic orbital elements of the initial
state
dV1Eph (1) Magnitude of the intial burn
det (1) Transfer time
h (1,2) Optional. Figure handles to use for plots.
-------
Outputs
-------
h (1,2) Figure handles used for the plots.
--------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/NewFig Math: Linear/Unit Orbit: OrbitCoord/J20002RotPuls Orbit: OrbitSim/Propagate4BP SC: BasicOrbit/El2RV SC: Ephem/PlanetPositionEMBarycenter
Back to the Orbit Module page