摘要
在详细分析平行接近法(理想约束方程ε=q=0)的基础上推导出一种新颖的平行接近法理想约束方程;该方法避开了在应用平行接近法时需要精确量测目标速度V_m和目标运动方位角η_(?)的难题,使得平行接近法的应用成为可能.以某型号导弹为例,利用这种新颖的平行接近法理想约束方程,进行了航向自导回路的数字仿真,得到令人满意的结果。
Based cm analysing the constant-bearing course guidance method(the ideal constraint equation is ε=q=0), a new ideal constraint equation of the method has been deduced. It is possible to use the method by avoiding the difficulties of accurately measuring the target velocity V_m and its azimuth η_m. The simulations of lateral guidance loop applying the new equation to some missile have been carried out to verify the new ideal constraint equation, and the results are fairly satisfactory.
出处
《战术导弹技术》
1992年第3期25-29,46,共6页
Tactical Missile Technology
关键词
平行接近法
导引
导弹
Constant-bearing course
Self- guidance loop
Proportional guidance
