Necessary and sufficient conditions of the rendezvous between a single spacecraft and three non-coplanar Walker constellation satellites

作     者：ZHANG Jing WU MeiPing 

作者机构：College of Mechatronics Engineering and Automation National University of Defense Technology Changsha 410073 China 

基　　金：supported by the Pre-Research Foundation of General Armament Department of China (Grant No. 6140551) 

出 版 物：《Science China(Technological Sciences)》 (中国科学（技术科学英文版）)

年 卷 期：2011年第54卷第9期

页      码：2254-2262页

摘      要：The probability of the rendezvous between a single spacecraft and three non-coplanar constellation satellites is studied,and the necessary and sufficient conditions of the rendezvous without orbital maneuver are *** rendezvous orbit design can be transformed into the patching of two spacecraft orbits,either of which can achieve the rendezvous with two ***,due to the precious quality of spherical geometry,the unique existence of the rendezvous orbit for two constellation satellites is ***,according to the difference between equispaced and non-equispaced orbital planes of three satellites,the necessary and sufficient conditions are given respectively,and the calculating method of the spacecraft orbit is *** last,the constraint conditions between two different rendezvous orbits is derived,while the relative position of two groups of objects are under specific *** results can be applied to the rendezvous between a single spacecraft and multiple constellation satellites without orbital maneuver.

主 题 词：Walker constellation necessary and sufficient conditions orbital design rendezvous with multiple satellites, patchedorbit, constraint conditions 

学科分类：08[工学] 081105[081105] 0825[工学-环境科学与工程类] 0811[工学-水利类] 

核心收录：

D　O　I：10.1007/s11431-011-4523-9

馆 藏 号：203541027...