Practical time-to-go estimation methods for optimal guidance
暂无分享,去创建一个
[1] Chi-Ching Yang,et al. Optimal pure proportional navigation for maneuvering targets , 1997 .
[2] Valery Y. Glizer,et al. Optimal planar interception with fixed end conditions: Closed-form solution , 1996 .
[3] Paul Zarchan,et al. A combined optimal/classical approach to robust missile autopilot design , 1979 .
[4] G. K. F. Lee. Estimation of the time-to-go parameter for air-to-air missiles , 1985 .
[5] Joseph Z. Ben-Asher,et al. Optimal Guidance with Reduced Sensitivity to Time-to-Go Estimation Errors , 1997 .
[6] D. Hull,et al. Time-to-go prediction for homing missiles based on minimum-time intercepts , 1991 .
[7] Min-Jea Tahk,et al. Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity , 1996 .
[8] Jang Gyu Lee,et al. Biased PNG law for impact with angular constraint , 1998 .