TY - GEN
T1 - Dynamic obstacle avoidance of autonomous rendezvous and docking using potential function guidance based-fuzzy logic system
AU - Zhang, Dawei
AU - Song, Shenmin
AU - Pei, Run
PY - 2010
Y1 - 2010
N2 - A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance based-fuzzy logic system, which adapts the parameters of the potential function, is used for chaser to approach non-cooperative target and avoid dynamic obstacles. Stability of the proposed method is analyzed by Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.
AB - A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance based-fuzzy logic system, which adapts the parameters of the potential function, is used for chaser to approach non-cooperative target and avoid dynamic obstacles. Stability of the proposed method is analyzed by Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.
KW - Artificial potential function guidance
KW - Autonomous rendezvous and docking
KW - Dynamic obstacle avoidance
KW - Fuzzy logic system
KW - Non-cooperative target
UR - https://www.scopus.com/pages/publications/79952147730
U2 - 10.1109/ISSCAA.2010.5633236
DO - 10.1109/ISSCAA.2010.5633236
M3 - 会议稿件
AN - SCOPUS:79952147730
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 34
EP - 39
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -