Path: Math/Demos/FDIR
% Demonstrate a detection filter for a spinning spacecraft. This filter will detect measurement failures and actuator failures This function uses an analytical derivation of a detection filter which is feasible for this simple system. For linear time invariant systems the detection filter gain matrix is a constant. Since version 9. ------------------------------------------------------------------------- See also C2DZOH, Plot2D ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright (c) 2006-2008 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
Common: Control/C2DZOH Common: Graphics/Plot2D
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