Autopilot Design for Bank-to-Turn Missiles Using Receding Horizon Predictive Control Scheme
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Wook Hyun Kwon | Yong Ho Kim | Myungjoon Kim | Chanho Song | W. Kwon | Y. Kim | Myung-Joon Kim | Chanho Song
[1] Ronald A. Hess,et al. Precise flight-path control using a predictive algorithm , 1991 .
[2] A. Arrow,et al. Comparison of classical and modern missile autopilot design and analysis techniques , 1989 .
[3] Lena Valavani,et al. Autopilot Design for Bank-to-Turn Missiles using LQG/LTR Methodology , 1988, 1988 American Control Conference.
[4] J.R. Cloutier,et al. Assessment of air-to-air missile guidance and control technology , 1988, IEEE Control Systems Magazine.
[5] Wook Hyun Kwon,et al. Receding Horizon Tracking Control as a Predictive Control and its Stability Properties , 1988, 1988 American Control Conference.
[6] David W. Clarke,et al. Generalized predictive control - Part I. The basic algorithm , 1987, Autom..
[7] Bernard Friedland,et al. Modern Control Theory for Design of Autopilots for Bank-to-Turn Missiles , 1986, 1986 American Control Conference.
[8] R. G. Cottrell. Optimal intercept guidance for short-range tactical missiles , 1971 .
[9] P. Bendotti,et al. A skid‐to‐turn missile autopilot design: The generalized predictive adaptive control approach , 1993 .
[10] Kevin A. Wise,et al. Bank-to-turn missile autopilot design using loop transfer recovery , 1990 .
[11] K. Sobel,et al. Application of Eigenstructure Assignment to Flight Control Design: Some Extensions , 1987 .