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Path: SpacecraftEstimation/Demos/StellarAttDet
% Demonstrate a Kalman Filter for a gyro based attitude determination system. There are two angle measurements from sensors separated by an initially unknown bias. ------------------------------------------------------------------------- See also C2DZOH, KFilter, Plot2D ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright (c) 2001 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
Common: Control/C2DZOH Common: Estimation/KFilter Common: Graphics/Plot2D
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