低推力转移交会任务的轨道与时间联合规划策略

IF 6.5 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Jia Guo, Zhaojun Pang, Zhonghua Du
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引用次数: 0

摘要

为了降低低推力交会任务的燃料消耗,提出了一种轨道规划与时间规划相结合的策略。首先,提出了一种调整自变量的变换方法,使采用逆多项式的基于形状的算法得到的结果可以作为伪谱方法的初始猜测。其次,设计了低推力转移轨迹优化与边界条件优化相结合的规划策略;该规划策略分为外层和内层。外部规划优化了等待和转移时间,从而确定了边界条件。内平面采用伪谱法对低推力转移轨迹进行了优化。内部平面嵌在外部平面中。数值仿真结果表明,自变量变换方法是可行的,并且将基于形状的算法与逆多项式和伪谱方法相结合,保证了较好的收敛性。采用轨迹优化和时间优化相结合的方法,大大降低了交会任务的成本。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Combined trajectory and time-planning strategy for rendezvous missions using low-thrust transfer

In this study, a combined trajectory and time-planning strategy is proposed to reduce the fuel consumption of low-thrust rendezvous missions. First, a transformation method was developed to adjust the independent variable such that results obtained using the shape-based algorithm that employs an inverse polynomial can be used as an initial guess for a pseudospectral method. Second, a planning strategy that combined low-thrust transfer trajectory optimization and boundary condition optimization was designed. This planning strategy was divided into outer and inner layers. The outer plan optimized waiting and transfer times and thus determined boundary conditions. The inner plan optimized the low-thrust transfer trajectory using the pseudospectral method. The inner plan was embedded in the outer plan. Numerical simulations show that the independent variable transformation method is feasible, and the combined use of the shape-based algorithm with the inverse polynomial and pseudospectral method ensures good convergence. The cost of rendezvous missions is significantly decreased using combined trajectory and time optimization.

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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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