Review of Guidance, Navigation, and Control Strategy for Aerobraking

被引：0
|
作者：
Liu X. [1 ,2 ]
Dong F. [2 ,3 ]
Xu C. [3 ,4 ]
Huang X. [3 ,4 ]
Li S. [2 ]
机构：
[1] School of Information Engineering, Nanchang University, Nanchang
[2] School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing
[3] Beijing Institute of Control Engineering, Beijing
[4] National Key Laboratory of Space Intelligent Control, Beijing
来源：
Yuhang Xuebao/Journal of Astronautics | 2024年 / 45卷 / 04期
关键词：
Aerobraking; Guidance; navigation; and control; Mars exploration; Venus exploration;
D O I：
10.3873/j.issn.1000-1328.2024.04.002
中图分类号：
学科分类号：
摘要：
Aerobraking effectively saves the fuel for orbital maneuvers through atmospheric drag deceleration,yet it also presents risks. To advance the aerobraking technology in Venus or Mars exploration,the fundamental profile and common characteristics of aerobraking missions are summarized. Simultaneously,the guidance,navigation,and control (GNC)scheme and its difficulties are outlined,along with the progress in autonomous aerobraking software. This study will provide a valuable reference for the mission profile design and GNC system development of future Venus and Mars exploration missions. © 2024 Chinese Society of Astronautics. All rights reserved.
引用
收藏
页码：499 / 512
页数：13
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