TY - JOUR
T1 - 扁平体空间非合作目标多指外包络抓捕构型设计
AU - Sun, Chong
AU - Wan, Wenya
AU - Cui, Yao
AU - Yuan, Jianping
N1 - Publisher Copyright:
© 2019, Editorial Office of Journal of Chinese Space Science and Technology. All right reserved.
PY - 2019/12/25
Y1 - 2019/12/25
N2 - Aiming at the problem of space non-cooperative target capture, a method was proposed for the optimal caging-based capture configuration design of multi-finger for flat non-cooperative objects. The core of the method is: selecting the lead finger of the capture mechanism and controlling it to track the caging point; calculating the feasible configuration of the follow fingers according to the geometric relationship of the capture mechanism; utilizing the caging-based capture constraints, as well as collision detection constraints, and selecting the effective caging-based capture configuration. Compared with the existing methods, the method adopts the simple mode of leader-followers, which can greatly reduce the calculation of the capture configuration optimization, and is suitable for real-time on-orbit capture of space non-cooperative targets. Further, the concept of safe capture margin is introduced to quantify the margin between the capture mechanism and the space non-cooperative target. Considering the collision avoidance between the non-cooperative target and the capture mechanism before the formation of the capture configuration, the configuration with maximum safe capture margin is chosen as the optimal. In order to verify the effectiveness of the proposed method, it is applied to the quadrilateral and regular pentagon moving target capture problems respectively. The simulation results show the effectiveness of the proposed algorithm.
AB - Aiming at the problem of space non-cooperative target capture, a method was proposed for the optimal caging-based capture configuration design of multi-finger for flat non-cooperative objects. The core of the method is: selecting the lead finger of the capture mechanism and controlling it to track the caging point; calculating the feasible configuration of the follow fingers according to the geometric relationship of the capture mechanism; utilizing the caging-based capture constraints, as well as collision detection constraints, and selecting the effective caging-based capture configuration. Compared with the existing methods, the method adopts the simple mode of leader-followers, which can greatly reduce the calculation of the capture configuration optimization, and is suitable for real-time on-orbit capture of space non-cooperative targets. Further, the concept of safe capture margin is introduced to quantify the margin between the capture mechanism and the space non-cooperative target. Considering the collision avoidance between the non-cooperative target and the capture mechanism before the formation of the capture configuration, the configuration with maximum safe capture margin is chosen as the optimal. In order to verify the effectiveness of the proposed method, it is applied to the quadrilateral and regular pentagon moving target capture problems respectively. The simulation results show the effectiveness of the proposed algorithm.
KW - Caging-based capture
KW - Leader-follower grasping mode
KW - Optimal capture configuration
KW - Safe capture margin
KW - Space non-cooperative target
UR - http://www.scopus.com/inward/record.url?scp=85076423140&partnerID=8YFLogxK
U2 - 10.16708/j.cnki.1000-758X.2019.0045
DO - 10.16708/j.cnki.1000-758X.2019.0045
M3 - 文章
AN - SCOPUS:85076423140
SN - 1000-758X
VL - 39
SP - 8
EP - 20
JO - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
JF - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
IS - 6
ER -