Design and Development of Hardware-in-Loop Simulation of Spacecraft Attitude Control System Based on Wireless Ad Hoc Networking

摘要：

Spacecraft attitude control system simulator is a laboratory system designed for developing and testing attitude control algorithm in a low-risk,low-cost environment. In this paper,the design and development of the hardware-in-loop simulation of spacecraft attitude control system is described,including hardware and software. The distinguished feature of the simulation system different from other simulators is that on-board data handling is based on wireless ad hoc network,which breaks through the traditional conception. Based on the established simulator,the paper presents some experimental results of spacecraft attitude control. The test results show that reliability and validity of the simulator,which provides a new way and a good support environment for the ground test of spacecrafts attitude control approaches.

关键词： attitude control wireless ad hoc networking hardware-in-loop simulation air-bearing table

作者: Gao Yudong Wu Jinjie Hu Min Zheng Wei

作者单位: Institute of Aerospace and Material Engineering,National University of Defense Technology,Changsha,C Academy of Equipment,Beijing,China College of Computer Science and Technology,JiLin University,Changchun,China

会议类型: 国际会议

会议名称: 2011 International Conference on Opto-Electronics Engineering and Information Science(2011光电电子工程与信息科学国际会议 ICOEIS 2011)

会议地点: 西安

会议语种:英文

页码: 1699-1703

在线出版日期: 2011-12-23（万方平台首次上网日期，不代表论文的发表时间）