Path: SC/Control
% Simulate a momentum bias spacecraft with a telescope on a roll pivot The momentum wheel is used to control spacecraft pitch orientation. The script includes an initial test of angular momentum conservation. It also computes the eigenvalues for the spacecraft when it is earth pointing. The pitch control loop is not included. In the simulation the telescope points at a ground target. -------------------------------------------------------------------------- See also LatLonAltToEF, OmegaLVLH, QLVLH, EarthRot, RHSThreeBody, FOrb, Jacobian, RK4, NewFig, Plot2D, TimeLabl, XLabelS, YLabelS, Date2JD, JD2T, Dot, Mag, Unit -------------------------------------------------------------------------
AerospaceUtils: Coord/LatLonAltToEF AerospaceUtils: Coord/OmegaLVLH AerospaceUtils: Coord/QLVLH Orbit: RHSOrbit/FOrb SC: Dynamics/RHSThreeBody SC: Ephem/EarthRot Common: GUIs/TimeDisplay Common: Graphics/NewFig Common: Graphics/TimeHistory Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Time/Date2JD Common: Time/JD2T Math: Analysis/Jacobian Math: Integration/RK4 Math: Linear/Dot Math: Linear/Mag Math: Linear/Unit
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