TY - JOUR
T1 - 小天体柔性附着技术
AU - Cui, Pingyuan
AU - Zhang, Chengyu
AU - Zhu, Shengying
AU - Ge, Dantong
AU - Long, Jiateng
AU - Shao, Wei
AU - Liang, Zixuan
N1 - Publisher Copyright:
© 2023 China Spaceflight Society. All rights reserved.
PY - 2023/6
Y1 - 2023/6
N2 - Aiming at the problem that the probe is easy to bounce and tumble in the low-gravity environment on small celestial bodies, the flexible landing mode and the related technologies are discussed. Firstly, the characteristics and the challenges of asteroid landing missions are analyzed. Then, combined with the previous missions, shortcomings of the rigid landing mode and the touch-and-go mode are discussed, and the novel mode called flexible landing is introduced. On this basis, focusing on the flexible landing mode, the progress and difficulties of key technologies are summarized from the aspects of autonomous guidance control and navigation, and the future research directions are forecasted.
AB - Aiming at the problem that the probe is easy to bounce and tumble in the low-gravity environment on small celestial bodies, the flexible landing mode and the related technologies are discussed. Firstly, the characteristics and the challenges of asteroid landing missions are analyzed. Then, combined with the previous missions, shortcomings of the rigid landing mode and the touch-and-go mode are discussed, and the novel mode called flexible landing is introduced. On this basis, focusing on the flexible landing mode, the progress and difficulties of key technologies are summarized from the aspects of autonomous guidance control and navigation, and the future research directions are forecasted.
KW - Cooperative control
KW - Cooperative estimation
KW - Flexible landing
KW - Intelligent sensing
KW - Small celestial body
KW - Strongly constrained guidance
UR - http://www.scopus.com/inward/record.url?scp=85169662844&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2023.06.001
DO - 10.3873/j.issn.1000-1328.2023.06.001
M3 - 文章
AN - SCOPUS:85169662844
SN - 1000-1328
VL - 44
SP - 805
EP - 816
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 6
ER -