Optimal Impulsive Rendezvous Under Target Flyby Constraint Based on Primer Vector Theory
Tian Liao, Gang Zhang, Shunli Li
Harbin Institute of Technology
阅读操作
确认中在文库中上传 PDF 后可生成中文音频讲解。
摘要与影响
This paper investigates the two-body fuel-optimal impulsive rendezvous problem with a target flyby constraint. Firstly, by defining the corresponding impulsive trajectory parameters, the constraint is implicitly incorporated into the problem formulation, and the feasibility of the constrained impulsive trajectory is ensured through solving the Lambert two-point boundary value problem. Secondly, to solve for the optimal impulsive trajectory, the constrained cost gradient and impulse addition criteria are derived based on the calculus of variations. In this derivation process, the constrained primer vector is defined, with the conventional primer vector proven to be a special form of the former in the unconstrained case. As a key conclusion of this paper, under the framework of the constrained primer vector, both the impulse addition method and the optimality necessary conditions can be formulated in forms analogous to those in the unconstrained case, thereby revealing the intrinsic connection between constrained and unconstrained problems. Finally, in the typical scenarios analyzed, the optimal flyby-rendezvous trajectory is successfully solved using the constrained cost gradient, and its optimality is verified via the necessary conditions. Meanwhile, a comparison with results obtained via the direct method demonstrates the advantage of the proposed method in terms of optimality and solution efficiency.
逐年被引趋势
暂无年度引用数据
关键指标
同类平均 = 1
同领域 · 同年份 · 同类型
Google Scholar 与 OpenAlex 的被引统计范围不同,数值存在差异属正常。
AI 辅助阅读
依据:摘要
可就本文提问;依据不足时会说明。
学术脉络
学科主题
工程Spacecraft Dynamics and Control
Space Satellite Systems and Control · Guidance and Control Systems
参考文献 38
此处列出前 3 条