针对大气层外高速飞行的动能拦截器，描述了末制导段拦截器的六自由度运动学方程。
Six-degree of freedom equations are described for high-speed interceptor flying in extra-atmospheric space.
大气层内的动能拦截器末制导段，为了提高对目标未知逃逸机动的鲁棒性，可采用变结构制导律。
During the terminal guidance phase of the kinetic kill vehicle in the atmosphere, the variable structure guidance law can be used to improve the robustness to unknown escaping maneuver of the target.
数学仿真表明，变结构自动驾驶仪具有很好的快速性和很高的姿态控制精度，可以满足动能拦截器对姿态控制的要求。
The simulation result shows that the variable structure automatic pilot for KKV is fast and has high attitude control accuracy, which satisfies the requirements.
拦截器在飞行过程中轨控推力以持续定常方式或小脉冲方式施加在垂直视线的方向，目标具有一定的机动能力。
The interceptor had sustain constant thrust or impulsive thrust perpendicular to the line-of-sight during the flight, and the target was maneuverable.
拦截器在飞行过程中轨控推力以持续定常方式或小脉冲方式施加在垂直视线的方向，目标具有一定的机动能力。
The interceptor had sustain constant thrust or impulsive thrust perpendicular to the line-of-sight during the flight, and the target was maneuverable.
应用推荐