Research of the Orbit Programming for On-orbit Emergency Service with Multi-constraint
The orbit programming for on-orbit emergency service is studied in this paper. The problem is considered under multi-constraint such as finite thrust and limited service time. The optimal object is to minimize the cost of orbit transfer. It is a nonlinear optimization problem with multi-constraint. A general optimization model is set up for multi-impulse, multi-revolution rendezvous which the impulse applied at apogee or perigee of the transfer orbit. A numerical example is given. The solutions show that this kind of problem can be solved by the strategy prospered in this paper.
Qi Ouyang Weiwei Yang Yong Zhao Xiaoqian Chen
College of Aerospace and Material Engineering National University of Defense Technology,Changsha,China
国际会议
哈尔滨
英文
1080-1084
2010-01-08(万方平台首次上网日期,不代表论文的发表时间)