TY - JOUR
T1 - Robust output tracking for nonlinear systems with weakly non-minimum phase
AU - Li-Chen, Kuang Yow
AU - Fu, Li Chen
AU - Liao, Teh Lu
N1 - Funding Information:
The authors would like to thank Professor Hauser for his fruitful comments that contributed to this work. This research was supported by National Science Council under the grant NSC-79-0404-E002-03.
PY - 1993/1/1
Y1 - 1993/1/1
N2 - This paper is concerned with the problem of designing a robust output tracking controller for MIMO nonlinear systems with weakly non-minimum phase. Based on our system formulation, control plants with uncertainties and/or with actuator dynamics fall into the class under consideration. The controller design here is divided into two phases: Fast feedback control and slow feedback control, so that a final composite control is obtained. The former is chosen to stabilize the boundary layer system, whereas the latter essentially handles the mismatched uncertainties after the system is reformulated. Under some mild assumptions, it is shown that the overall states are bounded and the tracking errors converge to a residual set whose size is a class k function of ϵ. As ϵ → 0, the residual set shrinks to the origin. An interesting application to a simplified aircraft model with fast actuator dynamics, which turns out to be weakly non-minimum phase, is given. The computer simulation has verified the expected satisfactory performance.
AB - This paper is concerned with the problem of designing a robust output tracking controller for MIMO nonlinear systems with weakly non-minimum phase. Based on our system formulation, control plants with uncertainties and/or with actuator dynamics fall into the class under consideration. The controller design here is divided into two phases: Fast feedback control and slow feedback control, so that a final composite control is obtained. The former is chosen to stabilize the boundary layer system, whereas the latter essentially handles the mismatched uncertainties after the system is reformulated. Under some mild assumptions, it is shown that the overall states are bounded and the tracking errors converge to a residual set whose size is a class k function of ϵ. As ϵ → 0, the residual set shrinks to the origin. An interesting application to a simplified aircraft model with fast actuator dynamics, which turns out to be weakly non-minimum phase, is given. The computer simulation has verified the expected satisfactory performance.
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U2 - 10.1080/00207179308923004
DO - 10.1080/00207179308923004
M3 - Article
AN - SCOPUS:0001465738
SN - 0020-7179
VL - 58
SP - 301
EP - 316
JO - International Journal of Control
JF - International Journal of Control
IS - 2
ER -