The Tianwen-1 Guidance, Navigation, and Control for Mars Entry, Descent, and Landing

Author:

Huang Xiangyu1,Li Maodeng1ORCID,Wang Xiaolei2,Hu Jinchang1,Zhao Yu2,Guo Minwen1,Xu Chao1,Liu Wangwang2,Wang Yunpeng2,Hao Ce2,Xu Lijia2

Affiliation:

1. Science and Technology on Space Intelligent Control Laboratory, Beijing Institute of Control Engineering, Beijing 100091, China

2. Beijing Institute of Control Engineering, Beijing 100091, China

Abstract

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.

Funder

National Natural Science Foundation of China

Publisher

American Association for the Advancement of Science (AAAS)

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