Minimum-fuel two-impulse transfer between coplanar noncoaxial elliptical orbits

被引：0
|
作者：
Li, Jing [1 ]
机构：
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China
来源：
ADVANCES IN SPACE RESEARCH | 2024年 / 73卷 / 01期
关键词：
Minimum-fuel solutions; Two-impulse transfer; Primer vector; Homotopic approach; RELATIVE-MOTION; HOMOTOPY METHOD; LOW-THRUST; PRIMER VECTOR; TIME;
D O I：
10.1016/j.asr.2023.10.008
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper investigates minimum-fuel two-impulse transfer between general coplanar noncoaxial elliptical orbits in a Newtonian gravitational field. First, without any restriction on the transfer time and boundary conditions, a necessary condition of optimality for the minimum-fuel solutions is derived via the primer vector analysis and thus, a simplified optimization model is presented. Then, a homotopic approach based algorithm is proposed to obtain the minimum-fuel solutions, which can start automatically from the analytical generalized Hohmann transfers. Finally, accuracy and efficiency of the algorithm are illustrated via different examples. Symmetric property of the minimum-fuel solutions is drawn. Special cases where the two-impulse solutions degenerate to one-impulse solutions are analyzed. Further discussions are given to explore the global optimality of the obtained minimum-fuel solutions. (c) 2023 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码：143 / 159
页数：17
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