DocumentCode
582354
Title
Configuration optimization of four dissimilar redundant flywheels with application to IPACS
Author
Shengyong, Tang ; Xibin, Cao ; Yulin, Zhang
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China
fYear
2012
fDate
25-27 July 2012
Firstpage
4664
Lastpage
4669
Abstract
Configuration optimization is performed to maximize the performance of a control system with constrained number of redundant actuators. In this paper we focus on exploring the optimal configuration of spacecraft mechanized with four dissimilar flywheels which maximizes the ability of momentum envelope and torque envelope respectively. Power management of the integrated power and attitude control system is also discussed when mechanizing the optimal momentum envelope configuration.
Keywords
actuators; aircraft control; attitude control; flywheels; power control; IPACS; configuration optimization; dissimilar redundant flywheels; integrated power and attitude control system; optimal momentum envelope configuration; power management; redundant actuators; spacecraft optimal configuration; torque envelope; Attitude control; Flywheels; Optimization; Power demand; Resource management; Torque; Vectors; Flywheel; IPACS; configuration optimization; momentum envelope; power management;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390746
Link To Document