DocumentCode :
3217491
Title :
Collision-avoiding research based on barrier theory for satellites formation flying
Author :
Liu Jianfeng ; Cui Naigang
Author_Institution :
Dept. of Space Eng., Harbin Inst. of Technol., China
fYear :
2006
fDate :
7-11 Aug. 2006
Firstpage :
663
Lastpage :
667
Abstract :
It is mission critical to avoid collisions between satellites as they moving in space. We present a method based on the barrier theory of differential game that may consider one satellite as a pursuer, the other as evader. According to optimal control theory, Hamiltonian function with the state inequality constraints of the min distance between adjacent satellites is investigated, and then obtaining optimal control. Finally the barrier trace is achieved according to barrier theory.
Keywords :
aerospace control; artificial satellites; collision avoidance; game theory; mobile robots; optimal control; Hamiltonian function; barrier theory; differential game; optimal control; satellites collision avoidance; satellites formation flying; state inequality constraints; Game theory; Helium; Mission critical systems; Optimal control; Planets; RNA; Satellites; Space technology; X-ray lasers; Zinc; barrier theory; collision-avoiding; differential game; formation flying;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2006. CCC 2006. Chinese
Conference_Location :
Harbin
Print_ISBN :
7-81077-802-1
Type :
conf
DOI :
10.1109/CHICC.2006.280695
Filename :
4060604
Link To Document :
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