摘要
根据空空导弹末端控制(ENDGAME)制导系统的特点,引用基于零化视线角速度的滑模制导律,理论上分析了当制导系统存在视线角速度和相对速度的测量噪声及目标机动时,此制导律的鲁棒性。仿真验证了此制导律在对克服测量噪声和目标机动时比比例导引律有一定的优势。
In this paper,a sliding-mode guidance law based on making LOS rate zero is quoted during the ENDGAME.The robustness of the guidance law is analyzed in the circumstances of aiming at the noise of LOS rate, relative rate and highly maneuverable targets.The simulation results show that sliding-mode guidance law is of an advantage over the proportional navigation guidance law in robustness against noise and highly maneuverable targets during the ENDGAME.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第S6期132-134,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
