RandomOrbit:

Path: Orbit/OrbitMechanics

% Monte-Carlo orbit simulation.

   Type RandomOrbit for a demo with 2008 AE9

   Since version 11.
--------------------------------------------------------------------------
   Form:
   [r1S, v1S, rN, vN] = RandomOrbit( el, el1S, t, mu, n )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   elI     (1,6) Elements vector [a,i,W,w,e,M]
   el1S    (1,6) Gaussian noise vector [a,i,W,w,e,M]
   t       (1,1) Times from 0 to ƒ (sec)
   mu      (1,1) Gravitational parameter
   

   -------
   Outputs
   -------
   r1S     (3,1)  Mean position 1 sigma (km)
   v1S     (3,1)  Mean velocity 1 sigma (km)
   rN      (3,1)  Nominal position (km)
   vN      (3,1)  Nominal velocity (km)

--------------------------------------------------------------------------

Children:

AC: ACData/ACTConstants
Orbit: OrbitCoord/SLR
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/CP2I
SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Linear/DupVect
Math: Linear/Mag

Back to the Orbit Module page