机载布撒器方案飞行的弹道设计

BALLISTIC DESIGN OF AIRBORNE DISPENSER DURING PROGRAMMED FLIGHT

利用在可操纵质点模型中加入约束，选取目标函数，求最优解的方法，对机载布撒器方案飞行的弹道进行了设计．给出了五条最优方案飞行弹道的飞行方案和基本运动参数，并分析评估了它们各自的优缺点．对一类无动力和有动力弹道的运动参数进行了对比．

In this paper the ballistics of airborne dispenser during programmed flight are designed by use of controllable mass point model to which constraints are added. The optimum ballistic is obtained by selecting objective function. The five optimun flight programs and basic motion parameters of programmed fight are presented. The advantage and disadvantages of them are analyzed. The comparison of motion parameters of a kind of ballistic without power and with power is given.