NadirSunPointingDemo:

Path: SC/Control

% An attitude and orbit simulation with reaction wheels.
 This simulation includes reaction wheels with Coulomb friction and
 damping. It is easy to specify the damping terms for each wheel. The demo
 also includes the PID3Axis controller. The core dynamics is for a
 gyrostat orbiting around a point mass.

 The simulation uses the vector pointing mode of PID3Axis to point
 a vector in the spacecraft frame either at nadir or at the sun.

 Control logic is included to point at nadir when the spacecraft is 
 over the continental United States and at the sun otherwise.

  ------------------------------------------------------------------------
  See also RHSRWAOrbit, PID3Axis, Plot2D, RK4
  ------------------------------------------------------------------------
%

Children:

Orbit: OrbitCoord/OverArea
Orbit: OrbitCoord/RAzToLatLon
SC: Control/PID3Axis
SC: Dynamics/RHSRWAOrbit
SC: Ephem/EarthRot
SC: Ephem/SunV1
SC: Visualization/LoadEarthMap
Common: Control/PIDMIMO
Common: GUIs/Figui
Common: Graphics/AddFillToPlots
Common: Graphics/AnimateVectors
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Common: Quaternion/QTForm
Common: Time/Date2JD
Common: Time/JD2T
Math: Integration/RK4
Math: Linear/Unit

Back to the SC Module page