固体火箭技术2012，Vol.35Issue(1)：11-16,6.
空间快速响应航天器轨道/弹道一体化规划
Orbit-trajectory integrated programming for operationally responsive space spacecraft
摘要
Abstract
Taking the operationally responsive space (ORS) task as the background,all-phase trace programming of the ORS spacecraft using orbit-trajectory integrated programming method was accomplished. Firstly, the influence of the designed trajectory features on the orbit elements was analyzed. Secondly,trajectory programming was divided into flight program design and firing data design,which were separately resolved by the improved particle swarm optimization and the Newton iterative method. The result shows that it is effective to program the flight trace by the algorithm proposed in the paper due to the fast convergence rate and the reduced iterative steps. The proposed algorithm can be easily implemented in engineering application. The obtained conclusions can provide theoretical guidance for ORS orbit-trajectory design.关键词
空间快速响应/轨道规划/弹道规划/混合优化/一体化Key words
operationally responsive space/orbit programming/trajectory programming/hybrid optimization/integrating分类
航空航天引用本文复制引用
黄文博,张强,肖飞,张为华..空间快速响应航天器轨道/弹道一体化规划[J].固体火箭技术,2012,35(1):11-16,6.基金项目
国家863计划资助项目(2007AAX02503). （2007AAX02503）
