An intelligent missile autopilot using genetic algorithm

This paper presents an intelligent autopilot for STT missiles with multiple controllers. The mixed H/sub 2//H/sub /spl infin// control technique is applied for each controller and implemented by using the genetic searching algorithm. To facilitate automatic switching of multiple controllers under different operating conditions, an error based switching scheme is also combined with the intelligent control system. It is shown via computer simulation that the proposed autopilot outperforms the conventional one.

[1]  B. Francis,et al.  A Course in H Control Theory , 1987 .

[2]  Bor-Sen Chen,et al.  A genetic approach to mixed H/sub 2//H/sub /spl infin// optimal PID control , 1995 .

[3]  양해원,et al.  시변 시스템의 적응제어에 관한 연구 ( Adaptive Control of Time Varying System ) , 1988 .

[4]  E. Jury,et al.  A general formulation of the total square integrals for continuous systems , 1965 .

[5]  Kumpati S. Narendra,et al.  Improving transient response of adaptive control systems using multiple models and switching , 1994 .

[6]  A. J. Calise Neural networks in nonlinear aircraft flight control , 1995 .

[7]  David E. Goldberg,et al.  Genetic Algorithms in Search Optimization and Machine Learning , 1988 .

[8]  James E. Steck,et al.  Linear and neural network feedback for flight control decoupling , 1996 .

[9]  Walter Baker,et al.  Learning augmented flight control for high performance aircraft , 1991 .

[10]  A. Arrow,et al.  Large Angle-of-Attack Missile Control Concepts for Aerodynamically Controlled Missiles , 1977 .

[11]  Kumpati S. Narendra,et al.  Identification and control of dynamical systems using neural networks , 1990, IEEE Trans. Neural Networks.

[12]  A. J. Calise,et al.  Neural networks in nonlinear aircraft flight control , 1995, Proceedings of WESCON'95.

[13]  Kevin A. Wise,et al.  Bank-to-turn missile autopilot design using loop transfer recovery , 1990 .

[14]  F. William Nesline,et al.  How Autopilot Requirements Constrain the Aerodynamic Design of Homing Missiles , 1984, 1984 American Control Conference.

[15]  Walter C. Merrill,et al.  Neural network application to aircraft control system design , 1991 .