摘要
本文运用微分对策理论研究了战术导弹与目标飞机之间的共面变速拦截问题,采用强迫奇异摄动方法求得了统一的近似反馈制导控制规律。选用实际空气动力数据的算例表明这个次最优制导控制规律是有效的。
In this paper, the problem of coplanar variable-:peed interception between a tactical missile and an aircraft is analysed by using the differential games theory. A unified approximate guidance law in feedback form is obtained by using the technique of forced singular perturbation(FSPT). The illustrative example with the realistic aerodynamic and propulsion data shows that this subopimal guidance control law is available for the practical applications.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1989年第9期A427-A433,共7页
Acta Aeronautica et Astronautica Sinica
关键词
共面拦截
微分对策
反馈解
two-player zero-sum games, nonlinear differential games, singular perturbation, feedback control strategies.
