Purpose
To compute, for a given open-loop model (A,B,C,0), and for given state feedback gain F and full observer gain G, such that A+B*F and A+G*C are stable, the Cholesky factors Su and Ru of a controllability Grammian P = Su*Su' and of an observability Grammian Q = Ru'*Ru corresponding to a frequency-weighted model reduction of the left or right coprime factors of the state-feedback controller.Specification
SUBROUTINE SB16CY( DICO, JOBCF, N, M, P, A, LDA, B, LDB, C, LDC, $ F, LDF, G, LDG, SCALEC, SCALEO, S, LDS, R, LDR, $ DWORK, LDWORK, INFO ) C .. Scalar Arguments .. CHARACTER DICO, JOBCF INTEGER INFO, LDA, LDB, LDC, LDF, LDG, LDR, LDS, LDWORK, $ M, N, P DOUBLE PRECISION SCALEC, SCALEO C .. Array Arguments .. DOUBLE PRECISION A(LDA,*), B(LDB,*), C(LDC,*), DWORK(*), $ F(LDF,*), G(LDG,*), R(LDR,*), S(LDS,*)Arguments
Mode Parameters
DICO CHARACTER*1 Specifies the type of the open-loop system as follows: = 'C': continuous-time system; = 'D': discrete-time system. JOBCF CHARACTER*1 Specifies whether a left or right coprime factorization of the state-feedback controller is to be used as follows: = 'L': use a left coprime factorization; = 'R': use a right coprime factorization.Input/Output Parameters
N (input) INTEGER The order of the open-loop state-space representation, i.e., the order of the matrix A. N >= 0. M (input) INTEGER The number of system inputs. M >= 0. P (input) INTEGER The number of system outputs. P >= 0. A (input) DOUBLE PRECISION array, dimension (LDA,N) The leading N-by-N part of this array must contain the state matrix A of the open-loop system. LDA INTEGER The leading dimension of array A. LDA >= MAX(1,N). B (input) DOUBLE PRECISION array, dimension (LDB,M) The leading N-by-M part of this array must contain the input/state matrix B of the open-loop system. LDB INTEGER The leading dimension of array B. LDB >= MAX(1,N). C (input) DOUBLE PRECISION array, dimension (LDC,N) The leading P-by-N part of this array must contain the state/output matrix C of the open-loop system. LDC INTEGER The leading dimension of array C. LDC >= MAX(1,P). F (input) DOUBLE PRECISION array, dimension (LDF,N) The leading M-by-N part of this array must contain a stabilizing state feedback matrix. LDF INTEGER The leading dimension of array F. LDF >= MAX(1,M). G (input) DOUBLE PRECISION array, dimension (LDG,P) The leading N-by-P part of this array must contain a stabilizing observer gain matrix. LDG INTEGER The leading dimension of array G. LDG >= MAX(1,N). SCALEC (output) DOUBLE PRECISION Scaling factor for the controllability Grammian. See METHOD. SCALEO (output) DOUBLE PRECISION Scaling factor for the observability Grammian. See METHOD. S (output) DOUBLE PRECISION array, dimension (LDS,N) The leading N-by-N upper triangular part of this array contains the Cholesky factor Su of frequency-weighted cotrollability Grammian P = Su*Su'. See METHOD. LDS INTEGER The leading dimension of the array S. LDS >= MAX(1,N). R (output) DOUBLE PRECISION array, dimension (LDR,N) The leading N-by-N upper triangular part of this array contains the Cholesky factor Ru of the frequency-weighted observability Grammian Q = Ru'*Ru. See METHOD. LDR INTEGER The leading dimension of the array R. LDR >= MAX(1,N).Workspace
DWORK DOUBLE PRECISION array, dimension (LDWORK) On exit, if INFO = 0, DWORK(1) returns the optimal value of LDWORK. LDWORK INTEGER The length of the array DWORK. LDWORK >= MAX(1, N*(N + MAX(N,M) + MIN(N,M) + 6)), if JOBCF = 'L'; LDWORK >= MAX(1, N*(N + MAX(N,P) + MIN(N,P) + 6)), if JOBCF = 'R'. For optimum performance LDWORK should be larger. An upper bound for both cases is LDWORK >= MAX(1, N*(N + MAX(N,M,P) + 7)).Error Indicator
INFO INTEGER = 0: successful exit; < 0: if INFO = -i, the i-th argument had an illegal value; = 1: eigenvalue computation failure; = 2: the matrix A+G*C is not stable; = 3: the matrix A+B*F is not stable; = 4: the Lyapunov equation for computing the observability Grammian is (nearly) singular; = 5: the Lyapunov equation for computing the controllability Grammian is (nearly) singular.Method
In accordance with the type of the coprime factorization of the controller (left or right), the Cholesky factors Su and Ru of the frequency-weighted controllability Grammian P = Su*Su' and of the frequency-weighted observability Grammian Q = Ru'*Ru are computed by solving appropriate Lyapunov or Stein equations [1]. If JOBCF = 'L' and DICO = 'C', P and Q are computed as the solutions of the following Lyapunov equations: (A+B*F)*P + P*(A+B*F)' + scalec^2*B*B' = 0, (1) (A+G*C)'*Q + Q*(A+G*C) + scaleo^2*F'*F = 0. (2) If JOBCF = 'L' and DICO = 'D', P and Q are computed as the solutions of the following Stein equations: (A+B*F)*P*(A+B*F)' - P + scalec^2*B*B' = 0, (3) (A+G*C)'*Q*(A+G*C) - Q + scaleo^2*F'*F = 0. (4) If JOBCF = 'R' and DICO = 'C', P and Q are computed as the solutions of the following Lyapunov equations: (A+B*F)*P + P*(A+B*F)' + scalec^2*G*G' = 0, (5) (A+G*C)'*Q + Q*(A+G*C) + scaleo^2*C'*C = 0. (6) If JOBCF = 'R' and DICO = 'D', P and Q are computed as the solutions of the following Stein equations: (A+B*F)*P*(A+B*F)' - P + scalec^2*G*G' = 0, (7) (A+G*C)'*Q*(A+G*C) - Q + scaleo^2*C'*C = 0. (8)References
[1] Liu, Y., Anderson, B.D.O. and Ly, O.L. Coprime factorization controller reduction with Bezout identity induced frequency weighting. Automatica, vol. 26, pp. 233-249, 1990.Further Comments
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