大气制动的制导、导航与控制方案综述  

Review of Guidance,Navigation,and Control Strategy for Aerobraking

作　　者：刘旭 董峰[2,3] 徐超 黄翔宇[3,4] 李爽 LIU Xu;DONG Feng;XU Chao;HUANG Xiangyu;LI Shuang(School of Information Engineering,Nanchang University,Nanchang 330031,China;School of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Beijing Institute of Control Engineering,Beijing 100094,China;National Key Laboratory of Space Intelligent Control,Beijing 100094,China)

机构地区：[1]南昌大学信息工程学院,南昌330031 [2]南京航空航天大学航天学院,南京210016 [3]北京控制工程研究所,北京100094 [4]空间智能控制技术全国重点实验室,北京100094

出　　处：《宇航学报》2024年第4期499-512,共14页Journal of Astronautics

基　　金：国家自然科学基金(U20B2001,11672126)。

摘　　要：大气制动借助行星大气阻力实现减速变轨,节约燃料的同时也存在诸多风险。面向金星和火星探测对大气制动技术的需求,综述了大气制动任务的基本流程和共性特征。同时,总结了相关的制导、导航与控制(GNC)方案和技术要点,并介绍了自主大气制动软件的研制情况。调研和分析内容将为金星和火星探测的总体方案设计以及GNC系统研制提供参考。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.

关 键 词：大气制动 制导、导航与控制 金星探测 火星探测 

分 类 号：V448[航空宇航科学与技术—飞行器设计]