Path: SpacecraftEstimation/SensorMeas
% Outputs the set of acceptable attitude measurements from vectors. Computes measurements given a pixel map from the unit vector measurements. This function is for use with the UKF as it does not return a linearized measurement matrix. -------------------------------------------------------------------------- Form: y = MeasurementsSunMagUKF( x, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) [dQ;b] d (.) Data structure ------- Outputs ------- y (:,1) Measurements --------------------------------------------------------------------------
AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/U2AzEl SC: BasicOrbit/Period SC: BasicOrbit/RVFromKepler SC: Environs/BDipole SC: Ephem/EarthRte SC: Ephem/MSidDay SC: Sensor/U2Pix Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Quaternion/QForm Common: Quaternion/QFromDQ Common: Quaternion/QMult Common: Quaternion/QUnit Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/T2JD Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Skew Math: Linear/Unit Math: MathUtils/R2P5
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