论文信息 - Design of Autopilots for High Performance Missiles

Design of Autopilots for High Performance Missiles

A novel control algorithm involving a robust inverse dynamics estimation (RIDE) is presented. It is shown how the control algorithm can be used in conjunction with a new safe criterion to result in the optimal and safe control algorithm (OSCA). The OSCA control algorithm is applied to the control of a high performance missile, where it is shown to provide excellent performance in terms of tight non-interacting and safe control in the presence of actuator saturation.

A Bradshaw | J M Counsell | A. Bradshaw | J. Counsell

[1] Yik-Chung Wu,et al. Integral variable structure control approach for robot manipulators , 1992 .

[2] Kevin A. Wise,et al. Optimizing singular value robustness measures in a conventional bank-to-turn missile autopilot design , 1988 .

[3] R. Reichert. Application of H(infinity) control to missile autopilot design , 1989 .

[4] Michel Kinnaert,et al. Conditioning technique, a general anti-windup and bumpless transfer method , 1987, Autom..

[5] R. Kálmán. On the general theory of control systems , 1959 .

[6] B. Porter,et al. Singular perturbation methods in the design of tracking systems incorporating high-gain error-actuated controllers , 1981 .

[7] D. J. East,et al. Guided Weapon Control Systems , 1979, IEEE Transactions on Systems, Man, and Cybernetics.

[8] Douglas Williams,et al. A computer-aided autopilot design procedure for a high performance bank-to-turn controlled tactical missile , 1987 .

[9] A. Arrow,et al. A bank-to-turn autopilot design for an advanced air-to-air interceptor , 1987 .

[10] Vadim I. Utkin,et al. A singular perturbation analysis of high-gain feedback systems , 1977 .

[11] J. M. Counsell. Design of autopilots for wingless missiles , 1991 .

[12] E. Davison,et al. Robust control of a general servomechanism problem: The servo compensator , 1975, Autom..

[13] A. Arrow. Status and concerns for bank-to-turn control of tactical missiles , 1985 .