Integrated guidance/autopilot scheme for anti-vessel missiles based on three channels independence design idea
暂无分享,去创建一个
[1] I. G. Sarma,et al. Switched bias proportional navigation for homing guidance against highly maneuvering targets , 1994 .
[2] Ciann-Dong Yang,et al. Nonlinear H∞ Robust Guidance Law for Homing Missiles , 1998 .
[3] E. J. Ohlmeyer,et al. Integrated Design of Agile Missile Guidance and Autopilot Systems , 2001 .
[4] I. Yaesh,et al. Optimum guidance with a single uncertain time lag , 1995 .
[5] Houria Siguerdidjane,et al. Various strategies to design a three-axes missile autopilot , 1999 .
[6] Neil F. Palumbo,et al. Integrated missile guidance and control: a state dependent Riccati differential equation approach , 1999, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328).
[7] Ilan Rusnak,et al. Guidance of a homing missile via nonlinear geometric control methods , 1995 .
[8] Ernest J. Ohlmeyer,et al. Optimal Design of Integrated Missile Guidance and Control , 1998 .
[9] Paul Zarchan,et al. Tactical and strategic missile guidance , 1990 .
[10] Di Zhou,et al. Adaptive Sliding-Mode Guidance of a Homing Missile , 1999 .
[11] In-Joong Ha,et al. A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws , 1994 .
[12] Min-Jea Tahk,et al. Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity , 1996 .