Robust switching missile autopilot

作者: P.B. Brugarolas , V. Fromion , M.G. Safonov

DOI: 10.1109/ACC.1998.703297

关键词:

摘要: A robust switching controller is developed by application of the unfalsified control concept. Key ideas and implementation issues are discussed. In particular, a new performance specification falsification algorithm developed. Simulation results provided using nonlinear model for missile.

参考文章(10)
G.J. Balas, A.K. Packard, Design of robust, time-varying controllers for missile autopilots international conference on control applications. pp. 104- 110 ,(1992) , 10.1109/CCA.1992.269891
Kevin A. Wise, Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics Journal of Guidance Control and Dynamics. ,vol. 15, pp. 861- 870 ,(1992) , 10.2514/3.20918
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
Dynamic scheduling of modern-robust-control autopilot designs for missiles IEEE Control Systems Magazine. ,vol. 12, pp. 35- 42 ,(1992) , 10.1109/37.158896
M.G. Safonov, Tung-Ching Tsao, The unfalsified control concept and learning IEEE Transactions on Automatic Control. ,vol. 42, pp. 843- 847 ,(1997) , 10.1109/9.587340
V. Fromion, G. Scorletti, G. Ferreres, Nonlinear performance of a PI controlled missile: an explanation conference on decision and control. ,vol. 5, pp. 4198- 4203 ,(1997) , 10.1109/CDC.1997.649492
R.A. Nichols, R.T. Reichert, W.J. Rugh, Gain scheduling for H-infinity controllers: a flight control example IEEE Transactions on Control Systems and Technology. ,vol. 1, pp. 69- 79 ,(1993) , 10.1109/87.238400
Michael G. Safonov, Tung-Ching Tsao, The unfalsified control concept: A direct path from experiment to controller Springer, Berlin, Heidelberg. pp. 196- 214 ,(1995) , 10.1007/BFB0027678
G. Ferreres, V. Fromion, G. Duc, M. M'Saad, Application of real/mixed μ computational techniques to an H∞ missile autopilot International Journal of Robust and Nonlinear Control. ,vol. 6, pp. 743- 769 ,(1996) , 10.1002/(SICI)1099-1239(199610)6:8<743::AID-RNC187>3.0.CO;2-O