摘要
基于冲量变轨理论,针对追踪器通过一次变轨机动对目标的拦截,以普适变量法进行快速轨道规划,给出轨道规划算法及流程。仿真结果表明:该法可快速确定追踪区,并得到最小燃耗对应的变轨点,方法简单,易于实现。
Based on impulse orbit-transfer theory, the method of the quickly designing orbit was made by general variable law for the intercepting target through only one orbit maneuver in this paper. The algorithm of the designing orbit and its flowchart were given out. The simulation results showed that the tracking area was assumed by the method quickly and the maneuver point was gained according to the least fueL, which was easy and feasible.
出处
《上海航天》
2013年第1期44-47,共4页
Aerospace Shanghai
基金
国家863基金项目(2010AA8091404)
关键词
空间拦截
普适变量法
冲量变轨
轨道规划
Space interception
General variable law
Impulse orbit-transfer
Orbit design
作者简介
作者简介：魏鹏涛（1986-），男，硕士生，主要研究方向为飞行器设计。
