Robustness Optimization Approach for Control Parameter of Small UAVs

XU Guo-dong; DIAO Zhao-shi; LI Zhi-tao

doi:10.3969/j.issn.1671-637x.2016.08.010

[1] MCLEAN D. Automatic flight control systems［M］. Englewood Cliffs: Prentice Hall Inc. , 1990.

[2] SCHOEMIG E, SZNAIER M. Mixed H2/H∞control of multi-model plants［J］. Journal of Guidance Control and Dynamics, 1995, 18(3): 525-531.

[3] JEROMEL J C, PERES P L, SOUZA S R. Convex analysis of output feedback control problems: robust stability and performance［J］. IEEE Transactions on Automatic Control, 1996, 41(7): 997-1003.

[4] TUNIK A A, AHN I K. Platform airship's robust stabiliza-tion in stochastic atmosphere［C］//Proceedings of the KSAS Fall Annual Meeting, Sejong Univ. , 2001: 293-299.

[7] ACKERMANN J. Parameter space design of robust control systems［J］. IEEE Transactions on Automatic Control, 1980, 25(6): 1058-1072.

[8] DE P E, CARVALHO J R, FERREIRA P A. An H2/H∞ pid heading controller for aurora-1 semi-autonomous robotic airship［C］//Proceedings of AIAA 14th Lighter-Than-Air Technical Committee Convention and Exhibi-tion, Akron, USA, Session 2, 2001: 21-27.

[12] SOYLEMEZ M T, MUMRO N. A parametric solution to the pole assignment problem using dynamic output feedback［J］. IEEE Transactions on Automatic Control, 2001, 46(5): 711-723.