Minimum-Time Trajectory Planning for Aeroassisted Maneuver Under Path Constraints

Xiangdong Feng, Hongwei Han*, Ruifeng Lv

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Aeroassist maneuvers offer significant fuel-saving advantages in planetary exploration orbital transfers. Multi-pass aeroassist can enhance maneuverability while reducing thermal protection costs. This paper addresses the minimum-time transfer for multi-pass aeroassisted maneuvers by formulating an optimal control problem with path constraints. Analyzing the characteristics of the minimum-time transfer trajectory yields the conditions necessary for the spacecraft's minimum transfer time. Then, a bisection-based rapid trajectory generation strategy is introduced, iteratively shooting the peak heating rate each pass to precisely activate path constraints, achieving the minimum time of entire maneuver. Simulations quantify the relationship between peak heating rate and atmospheric entry orbit size. Minimum transfer times and passes for varied path constraints were determined via simulation.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 11
编辑Liang Yan, Haibin Duan, Yimin Deng
出版商Springer Science and Business Media Deutschland GmbH
258-268
页数11
ISBN(印刷版)9789819622399
DOI
出版状态已出版 - 2025
活动International Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, 中国
期限: 9 8月 202411 8月 2024

出版系列

姓名Lecture Notes in Electrical Engineering
1347 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2024
国家/地区中国
Changsha
时期9/08/2411/08/24

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