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CubeSatSimulation:

Path: CubeSat/Demos/Simulation

% Demonstrate a CubeSat attitude and power system dynamics.
 This simulation includes drag and radiation pressure. The only actuator 
 available for attitude is magnetic torquers, which is modeled as a 
 dipole. Performs an animation at the end which may take a few minutes.
 The satellite is initialized pointing to the Earth with a rotation equal
 to orbit rate, to nominally maintain that pointing. The z body axis is
 pointed towards the Earth (nadir).

 Things to try:
   1. Turn surface disturbances off by uncommenting the line setting
      d.surfData to empty; notice that the altitude no longer drops.
   2. Initialize the battery charge b0 to zero
   3. Comment out or change the fixed dipole in the for loop
   4. Try a 1U instead of a 3U

 Since version 8.

  ----------------------------------------------------------------------
  See also AnimQ, QForm, Plot2D, TimeLabl, RK4, Skew, Date2JD, 
  InertiaCubeSat, CubeSatAero, RHSCubeSat, CubeSatFaces, BDipole, 
  SolarFluxPrediction
  ----------------------------------------------------------------------
%
------------------------------------------------------------------------
   Copyright (c) 2009 Princeton Satellite Systems, Inc.
   All rights reserved.
------------------------------------------------------------------------

Children:

AeroUtils: Coord/QLVLH
Common: Graphics/Figui
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Common: Quaternion/AnimQ
Common: Quaternion/QForm
Common: Quaternion/QMult
Common: Quaternion/QPose
Common: Time/Date2JD
CubeSat: AttitudeControl/InertiaCubeSat
CubeSat: Simulation/CubeSatAero
CubeSat: Simulation/CubeSatRadiationPressure
CubeSat: Simulation/RHSCubeSat
CubeSat: Utilities/CubeSatFaces
CubeSat: Visualization/GroundTrack
Math: Integration/RK4
Math: Linear/Mag
Math: Linear/Skew
SC: BasicOrbit/El2RV
SC: BasicOrbit/OrbRate
SC: BasicOrbit/Period
SC: BasicOrbit/PltOrbit
SC: Environs/BDipole
SC: Environs/SolarFluxPrediction

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