天文一号火星进入、下降和着陆的制导、导航和控制

IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Xiangyu Huang, Maodeng Li, Xiaolei Wang, Jinchang Hu, Yu Zhao, Minwen Guo, Chao Xu, Wangwang Liu, Yunpeng Wang, Ce Hao, Lijia Xu
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引用次数: 17

摘要

“天文一号”是中国行星探测计划的第一个任务,完成了绕火星轨道运行、着陆和漫游火星的目标。进入、下降和着陆(EDL)阶段直接决定了整个任务的成功,其中制导、导航和控制(GNC)系统是至关重要的。本文概述了天文一号EDL GNC系统设计,介绍了GNC需求,给出了满足GNC需求的GNC系统架构和算法。文中还给出了整个EDL阶段的实际飞行结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Tianwen-1 Guidance, Navigation, and Control for Mars Entry, Descent, and Landing
Tianwen-1, the first mission of China’s planetary exploration program, accomplished its goals of orbiting, landing, and roving on the Mars. The entry, descent, and landing (EDL) phase directly determines the success of the entire mission, of which the guidance, navigation, and control (GNC) system is crucial. This paper outlines the Tianwen-1 EDL GNC system design by introducing the GNC requirements followed by presenting the GNC system architecture and algorithms to meet such requirements. The actual flight results for the whole EDL phase are also provided in this paper.
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来源期刊
中国空间科学技术
中国空间科学技术 ENGINEERING, AEROSPACE-
CiteScore
1.80
自引率
66.70%
发文量
3141
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