标题: 中华卫星二号姿态控制系统控制器设计分析
Design and Analysis for the Controller of Rocsat-2 Attitude Control System
作者: 邱俊诚 
国立交通大学电机与控制工程学系 
关键字: 姿态控制;稳定性;卫星 ;Satellite;Attitude control;Bang-bang 
公开日期: 2000
摘要: 中华二号卫星之主要任务为高精密的解析度遥测作业,其操作性能与卫星本身之指向追踪能力息息相关,指向的稳定性经常是遥测照相成败的重要因素。在姿控模式的操控能力上,姿控系统控制扮演着非常重要的角色,因此,在卫星的研发过程中,姿控系统控制的分析设计应是不可或缺的关键技术之一。 本报告叙述卫星动力方程式的推导,及控制法则的建立,按卫星指向角度大小不同的情况来分别探讨系统之稳定性,配合bang-bang控制法则,发展增进控制性能及强韧性之控制器,以得到最佳时间需求下之姿控稳定控制。 
The major mission of Rocsat-2 is to fulfill the remote sensing operation with the high precise resolution. The sensing function is highly related to the directional tracking efficiency of the satellite. The stability of the directional track usually is the important factor that effects the results of remote sensing operation. In the operation of the satellite attitude control modes, the controller of the attitude control system plays a very important role. Thus, the analysis and design of the controller is a key technology in the research of the satellite. We will derive the dynamic governing equation of the satellite and build its control law in this project. Then we will discuss the stability of the system according to the different direction angles and the bang-bang type control method, we can build up the attitude control system with better controlling function and robustness at the optimal time. 
官方说明文件#: NSC89-NSPO(A)-PC-FA06-01 
URI: https://www.grb.gov.tw/search/planDetail?id=563364&docId=104661
http://hdl.handle.net/11536/132133
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