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