Path: SCPro/ProControl
% 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. In the simulation the telescope points at a ground target. -------------------------------------------------------------------------- See also LatLonAltToEF, OmegaLVLH, QLVLH, EarthRot, RHSThreeBody, NewFig, Plot2D, TimeLabl, XLabelS, YLabelS, Date2JD, JD2T, Jacobian, RK4, Dot, Mag, Unit -------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: Coord/LatLonAltToEF AerospaceUtils: Coord/OmegaLVLH AerospaceUtils: Coord/QIToBDot AerospaceUtils: Coord/QLVLH SC: Ephem/EOfE SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: SCData/sCTConstants SCPro: DynamicalModels/RHSThreeBody Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Control/C2DZOH Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/IsVersionAfter Common: General/MatToCell Common: General/StringToTokens Common: General/Watermark Common: Graphics/AddAxes Common: Graphics/Coordinates Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Quaternion/AU2Q Common: Quaternion/Mat2Q Common: Quaternion/Q2Mat Common: Quaternion/QTForm Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Transform/AU2M Math: Analysis/Jacobian Math: Integration/RK4 Math: Linear/Cross Math: Linear/Dot Math: Linear/Mag Math: Linear/Skew Math: Linear/SkewSq Math: Linear/SkewSymm Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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