DocumentCode :
620440
Title :
Reconfiguration allocation of satellite attitude control systems
Author :
Xiang Changyi ; Yang Hao ; Cheng Yuehua ; Jiang Bin
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2013
fDate :
25-27 May 2013
Firstpage :
4101
Lastpage :
4105
Abstract :
The paper addresses the issue of reconfigurability allocation for satellite attitude control system with constraints and with considering the lack of reconfigurability statistics data and the requirement of resource optimization. The reconfigurability allocation is divided into primary and secondary allocations, two novel allocation methods are proposed that are based on the fuzzy comprehensive evaluation and NN heuristic algorithm respectively. Simulation results show the efficiency of the proposed methods.
Keywords :
artificial satellites; attitude control; data handling; fuzzy set theory; optimisation; statistical analysis; NN heuristic algorithm; fuzzy comprehensive evaluation; primary allocations; reconfigurability statistics data; reconfiguration allocation; resource optimization; satellite attitude control systems; secondary allocations; Abstracts; Attitude control; Automation; Educational institutions; Optimization; Resource management; Satellites; Fuzzy comprehensive evaluation; Reconfigurability; Reconfigurability allocation; Reconfigurability degree; Satellite attitude control system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location :
Guiyang
Print_ISBN :
978-1-4673-5533-9
Type :
conf
DOI :
10.1109/CCDC.2013.6561669
Filename :
6561669
Link To Document :
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