Automatic tuning for model based predictive control during reconfiguration.
作者： M. Huzmezan , J.M. Maciejowski
DOI: 10.1016/S1474-6670(17)41083-4
关键词:
摘要: Abstract When major failures are encountered in a missile controlled by nominal Model Based Predictive Control (MBPC) these reflected the internal model via relatively sophisticated mechanism involving high fidelity models written quasi-LPV form. At this stage an optimisation will provide tuning parameters controller cost function weights- which enable to match, online, reference closed loop. The algorithm is applied MBPC while reconfiguring on-line for structural impairments.
harvard.edu
sci-hub.se 参考文章(4)
J.B. Rawlings, K.R. Muske, The stability of constrained receding horizon control IEEE Transactions on Automatic Control. ,vol. 38, pp. 1512- 1516 ,(1993) , 10.1109/9.241565
Jeff S. Shamma, James R. Cloutier, Gain-Scheduled Missile Autopilot Design Using Linear Parameter Varying Transformations Journal of Guidance Control and Dynamics. ,vol. 16, pp. 256- 263 ,(1993) , 10.2514/3.20997
M. Huzmezan, J. Maciejowski, Reconfiguration and scheduling in flight using quasi-LPV high-fidelity models and MBPC control american control conference. ,vol. 6, pp. 3649- 3653 ,(1998) , 10.1109/ACC.1998.703294
ZHIQIANG GAO, PANOS J. ANTSAKLIS, Stability of the pseudo-inverse method for reconfigurable control systems International Journal of Control. ,vol. 53, pp. 717- 729 ,(1991) , 10.1080/00207179108953643