论文信息 - AEROSPACE GAIN SCHEDULING DESIGN USING GENETIC OPTIMISATION

AEROSPACE GAIN SCHEDULING DESIGN USING GENETIC OPTIMISATION

Abstract In this work, some evolutionary-based approaches are presented for the gain-scheduling controller design. The cost-function is composed by restrictions on the dynamical behaviour like percent overshoot, rise time, settling time, etc. The attitude control of a launcher is used to present the results. Extensions of the procedures are discussed for other systems.

Waldemar de Castro Leite Filho | Alexandro Garro Britto

[1] Min-Yen Wu,et al. A note on stability of linear time-varying systems , 1974 .

[2] Gilles Duc,et al. An interpolation method for gain-scheduling , 2001, Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228).

[3] R. T. Reichert. Dynamic scheduling of modern-robust-control autopilot designs for missiles , 1992 .

[4] Fabio Ramos,et al. Approach Comparison for Controller Design of a Launcher , 2006 .

[5] Charles A. Desoer,et al. Slowly varying system ẋ = A(t)x , 1969 .

[6] W. Land,et al. Application of evolutionary computation to aircraft control law design , 2001, Proceedings of the 2001 Congress on Evolutionary Computation (IEEE Cat. No.01TH8546).

[7] Wilson J. Rugh,et al. Research on gain scheduling , 2000, Autom..

[8] Wilson J. Rugh,et al. A stability result for linear parameter-varying systems , 1995 .

[9] Peng-Yung Woo,et al. Gain Scheduled Output Feedback Control Based on LTI Controller Interpolation that Preserves LPV H∞ Performance , 2004, J. Intell. Robotic Syst..

[10] Pierre Apkarian,et al. Advanced gain-scheduling techniques for uncertain systems , 1998, IEEE Trans. Control. Syst. Technol..