Entry vehicle control system design for the Tianwen-1 mission

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Astrodynamics Pub Date : 2022-01-04 DOI:10.1007/s42064-021-0124-y
Jinchang Hu, Xiangyu Huang, Maodeng Li, Minwen Guo, Chao Xu, Yu Zhao, Wangwang Liu, Xiaolei Wang
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引用次数: 2

Abstract

The entry vehicle for the Tianwen-1 mission successfully landed on the surface of Mars at 7:18 AM BJT on May 15, 2021. This successful landing made China the first country to orbit, land, and release a rover in their first attempt at the Mars exploration. The guidance, navigation, and control (GNC) system plays a crucial role in the entry, descent, and landing (EDL) phases. This study focused on the attitude control component of the GNC system design. The EDL phase can be divided into several sub-phases, namely the angle of attack control phase, lift control phase, parachute descent phase, and powered descent phase. Each sub-phase has unique attitude control requirements and challenges. This paper introduces the key aspects of designing attitude controllers for each phase. Furthermore, flight results are presented and analyzed.

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天文一号任务的进入飞行器控制系统设计
北京时间2021年5月15日上午7点18分,“天文一号”任务的进入飞行器成功降落在火星表面。这次成功着陆使中国成为第一个绕轨道运行、着陆并释放火星探测器的国家,这是中国首次尝试火星探测。制导、导航和控制(GNC)系统在进入、下降和着陆(EDL)阶段起着至关重要的作用。本文主要研究GNC系统中姿态控制部分的设计。EDL阶段可分为攻角控制阶段、升力控制阶段、降落伞下降阶段和动力下降阶段。每个子阶段都有独特的姿态控制要求和挑战。本文介绍了各阶段姿态控制器设计的关键问题。最后给出了飞行结果并进行了分析。
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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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