摘要
本文从再入大气层弹道导弹弹头运动的解析解着手，找出了在再入点参数一定的情况下，决定弹头运动状态的唯一因素是弹头的弹道系数。为此，本文提出了一种设计弹头伴随重诱饵的方法。按此方法设计诱饵，可使得在整个再入段，诱饵即使不带小型发动机调整姿态，也能保持与弹头相同的运动状态，以此达到掩护弹头突防的目的。
This paper is started with the closed form motion solution for ballistic missile to reenter the Earth's atomosphere. It is found when the parameters are unchanged at the point of reentry, the only cause to decide the motion of the missile is its trajectory coefficient, where a method is proposed to design heavy decoy flying together with a missile. The decoy designed by the method, even if there is not small engines with it to adjust its posture, will keep the same motion with the missile along the whole reentry trajectory so as to shield the missile to break through the defense.
出处
《系统工程与电子技术》
EI
CSCD
1998年第8期1-3,57,共4页
Systems Engineering and Electronics
基金
国家自然科学基金
国防预研基金
