Bounds on maximal and minimal distances for coplanar satellite relative motion under given initial conditions

被引：10

作者：

Dang, Zhaohui ^{[1
,3
]}

Li, Taibo ^{[2
]}

Wang, Zhaokui ^{[4
]}

Zhang, Yulin ^{[4
]}

机构：

[1] Natl Univ Def Technol, Acad Equipment, Changsha 410073, Hunan, Peoples R China

[2] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China

[3] Acad Equipment, Beijing 101416, Peoples R China

[4] Tsinghua Univ, Sch Aerosp, Beijing 100084, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2015年 / 46卷

基金：

中国国家自然科学基金;

关键词：

Maximal distance; Minimal distance; Satellite relative motion; Bounds; Coplanar; METRICS;

D O I：

10.1016/j.ast.2015.07.012

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Maximal and minimal distances are the key parameters for a typical leader follower satellite formation. For the mission designers, the definition of the initial relative orbital elements that are constrained by extreme distances is a difficult but meaningful problem. In this paper, the analytic distance bounds for the coplanar relative motion are obtained. These solutions are accurate for those periodic close formations in which the follower and leader satellite have equal semi-major axis. Besides, the assumption that the leader satellite has a circular orbit is adopted. Five kinds of special positions that are located on a single axis and generated the given extremum distances are derived and discussed. The simulation results are also provided to corroborate the analytic developments. (C) 2015 Elsevier Masson SAS. All rights reserved.

引用

页码：204 / 209

页数：6

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