Reconfiguration Allocation of Satellite Attitude Control Systems

被引：0

作者：

Xiang Changyi ^{[1
]}

Yang Hao ^{[1
]}

Cheng Yuehua ^{[2
]}

Jiang Bin ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China

[2] Nanjing Univ Aeronaut & Astronaut, Acad Frontier Sci, Nanjing 210016, Peoples R China

来源：

2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2013年

关键词：

Reconfigurability; Reconfigurability degree; Reconfigurability allocation; Fuzzy comprehensive evaluation; Satellite attitude control system;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

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.

引用

页码：4101 / 4105

页数：5