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
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;
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
Print_ISBN :
978-1-4673-2581-3
