火力与指挥控制Issue(10)：142-145,4.
Halo轨道的航天器编队构型设计
Formation Configuration Design Based on Halo Orbit
摘要
Abstract
Formation configuration design method based on Halo orbit with different interferometric baseline constraints is studied. The relative motion model for two spacecraft flying on one Halo orbit is established,using the third order approximate analytical solution form of Halo orbit derived by Richardson. The rotation coordinate system related with chief and the observed target is constructed,and the calculation formulae of interferometric baseline are given. Then the optimal formation configuration is obtained,satisfying the baseline constraints and the longest observing time. Finally,the simulation for formation flying on Halo orbit around the sun-earth L2 libration point shows the validity of the design.关键词
Halo轨道/编队飞行/构型设计/干涉基线Key words
Halo orbit/formation flight/configuration design/interferometric baseline分类
航空航天引用本文复制引用
张云燕,李楠,李言俊..Halo轨道的航天器编队构型设计[J].火力与指挥控制,2014,(10):142-145,4.基金项目
国家自然科学基金（61174204）；航天支撑基金资助项目 （）
