Integrated Design of Agile Missile Guidance and Autopilot Systems
暂无分享,去创建一个
[1] A. TUSTIN,et al. Automatic Control Systems , 1950, Nature.
[2] Benjamin C. Kuo,et al. AUTOMATIC CONTROL SYSTEMS , 1962, Universum:Technical sciences.
[3] J. Meditch,et al. Applied optimal control , 1972, IEEE Transactions on Automatic Control.
[4] R. Brockett. Nonlinear systems and differential geometry , 1976, Proceedings of the IEEE.
[5] Thomas Kailath,et al. Linear Systems , 1980 .
[6] A. Isidori. Nonlinear Control Systems , 1985 .
[7] R. Walker,et al. Nonlinear flight test trajectory controllers for aircraft , 1987 .
[8] Sanjay Garg. Integrated Flight/Propulsion Control Design for a STOVL Aircraft using H-Infinity Control Design Techniques , 1991, 1991 American Control Conference.
[9] J. R. Cloutier,et al. Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method , 1994 .
[10] Paul Zarchan,et al. Proportional navigation and weaving targets , 1995 .
[11] Ernest J. Ohlmeyer. Root-mean-square miss distance of proportional navigation missile against sinusoidal target , 1996 .
[12] J. Cloutier. State-dependent Riccati equation techniques: an overview , 1997, Proceedings of the 1997 American Control Conference (Cat. No.97CH36041).
[13] Padmanabhan Menon,et al. Adaptive Techniques for Multiple Actuator Blending , 1998 .
[14] Ernest J. Ohlmeyer,et al. Software Tools for Nonlinear Missile Autopilot Design , 1999 .