A Trade Study On Missile Autopilot Design Using Optimal Control Theory
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[1] K. A. Wise,et al. High gain H/sub /spl infin// feedback control for an anti-air missile , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[2] J. Doyle. Synthesis of robust controllers and filters , 1983, The 22nd IEEE Conference on Decision and Control.
[3] K. A. Wise,et al. H/sub /spl infin// missile autopilot design with and without imaginary axis zeros , 1994, Proceedings of 1994 American Control Conference - ACC '94.
[4] Kevin A. Wise,et al. Approximating a linear quadratic missile autopilot design using an output feedback projective control , 1991 .
[5] Kevin A. Wise,et al. Nonlinear H^ Optimal Control for Agile Missiles , 1995 .
[6] F. Nesline,et al. Why Modern Controllers Can Go Unstable in Practice , 1984 .
[7] W. Perkins,et al. Output feedback pole placement in the design of suboptimal linear quadratic regulators , 1981 .
[8] Zdravko Uskokovic,et al. The design of optimal output regulators for linear multivariable systems with constant disturbances , 1983 .
[9] Kevin A. Wise,et al. Optimal disturbance rejection in missile autopilot design using projective controls , 1992 .
[10] Kevin A. Wise,et al. Bank-to-turn missile autopilot design using loop transfer recovery , 1990 .
[11] W. R. Perkins,et al. Robust Projective Controls for Structured Perturbations , 1986, 1986 American Control Conference.
[12] Kevin A. Wise,et al. Agile missile dynamics and control , 1996 .
[13] Kevin A. Wise,et al. Automated gain schedules for missile autopilots using robustness theory , 1992, [Proceedings 1992] The First IEEE Conference on Control Applications.
[14] William L. Brogan,et al. Modern control theory (3rd ed.) , 1991 .
[15] Kevin A. Wise,et al. Missile autopilot design using H∞ optimal control with μ-synthesis , 1990, 1990 American Control Conference.
[16] G. Stein,et al. Robustness with observers , 1978, 1978 IEEE Conference on Decision and Control including the 17th Symposium on Adaptive Processes.