Configuration Optimization of Four Dissimilar Redundant Flywheels with Application to IPACS

摘要：

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.

关键词： Flywheel configuration optimization momentum envelope IPACS power management

作者: TANG Shengyong CAO Xibin ZHANG Yulin

作者单位: Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 4

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 4664-4669

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）