An optimal guidance and nonlinear filtering method for space interceptor is presented in this paper.
本文提出了一种空间拦截弹的最优制导和非线性滤波方法。
Consulting the structure of the some space intercepting device, the conceptual model of the space interceptor is provided.
参考某些空间拦截器的构造形式，给出了空间拦截器的概念模型。
The idea of control based decision tree was proposed for attitude control of the space interceptor with the on-off actuators.
拦截器的发动机为带脉冲型发动机，从而限定了作动器的输出集。对于该拦截器的姿态控制，提出了基于决策树的控制方法。
After flying into space, the interceptor released its exoatmospheric kill vehicle, which tracked, intercepted and destroyed the target warhead.
飞入太空后，拦截弹释放外大气层杀伤装置，该装置进一步跟踪、拦截并摧毁目标弹头。
Six-degree of freedom equations are described for high-speed interceptor flying in extra-atmospheric space.
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.
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。
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