|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Orbit/Demos/ThreeBody
% Simulates a spiral out from LEO. The trajectory as plotted as well as the orbital elements in the heliocentric frame. The final orbital elements at the end of the spiral out are printed to the command window. This demo demonstrates several coordinate transformation Since version 10. ------------------------------------------------------------------------ See also Constant, CRTBPRHS, El2RV, RV2El, TransformECIToSEMR, SEMRToSEMI, FCRTBPRHS, LowThrustCRTBP_StopFcn, Plot2D, PlotSEMTraj ------------------------------------------------------------------------ % ------------------------------------------------------------------------------- Copyright (c) 2012 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/NewFig Common: Graphics/Plot2D Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit Orbit: OrbitCoord/SEMRToSEMI Orbit: OrbitCoord/TransformECIToSEMR Orbit: ThreeBody/CRTBPRHS Orbit: ThreeBody/FCRTBPRHS Orbit: ThreeBody/LowThrustCRTBP_StopFcn Orbit: Visualization/PlotSEMTraj OrbitMiniToolbox: Support/El2RV SC: BasicOrbit/RV2El
Back to the Orbit Module page