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📄 obmat.m

📁 剑桥大学用于线性和双线性动力学系统辨识的工具箱
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function y = obmat(A,C,i)%OBMAT   Constructs the observability matrix with a given index.%%   OBMAT(A,C,k) constructs the truncated (k < n), standard (k = n) or%      extended (k > n) observability matrix of the state-space system%      (A,B,C,D) with n states and p outputs.%%   Usage:%      Y = obmat(A,C,k)%%   Inputs: %      A := Square matrix with n rows and n columns.%      C := Matrix with p rows and n columns.%      k := Positive integer.%   %   Outputs:  %      Y := Observability matrix with k*p rows and n columns, defined as%%                           [     C     ]%                           [    C*A    ]%              Y := O_k :=  [   C*A^2   ]%                           [     :     ]%                           [ C*A^(k-1) ]%%   See also OBSV.%% CUED System Identification Toolbox.% Cambridge University Engineering Department.% Copyright (C) 1998-2002. All Rights Reserved.% Version 1.00, Date: 01/06/2002% Created by H. Chen and E.C. Kerrigan.   [rowA,colA] = size(A);[rowC,colC] = size(C);if rowA ~= colA,  error('A is not a square matrix.')endif colC ~= colA,  error('The column numbers of two input matrices are not equal.')endif (i < 1) | (i ~= fix(i)),   error('k is not a positive integer.')endp = rowC;n = rowA;if i == 1,   y = C;else  y = zeros(i*p,n);  d = C;  for j = 1:i,	y((j-1)*p+1:j*p,:) = d;	d = d*A;	  endend   % *** last line of obmat.m ***

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