摘要
控制力矩陀螺是一种常用的航天器的执行机构,广泛应用于卫星、空间站中.为了掌握控制力矩陀螺的原理,针对控制力矩陀螺Model750装置组成进行了介绍,为该装置建立了近似的数学模型,基于RTWT实验系统平台及线性二次型调节器为其设计了最优控制器,并且设计了控制器参数,进行实物控制验证,得到的曲线说明了控制器的有效性.
Control moment gyroscopes（ CMG） are widely used in spacecrafts such as satellites and space stations as actuators of attitude control. In order to grasp the principle of control moment gyroscope,the constitution of Model750 was introducedand the mathematical model of the device has been constructed for Model750. The controller for Model750 using linear quadratic regulatormethod based on real time windows target platform and design parameters of controller were put forward in this paper. The efficiency of controller was proved by graphs.
出处
《哈尔滨商业大学学报（自然科学版）》
CAS
2017年第6期702-707,共6页
Journal of Harbin University of Commerce：Natural Sciences Edition
基金
黑龙江省教学研究项目(JG2013010268)
关键词
控制陀螺力矩
实验系统平台
线性二次型调节器
控制器设计
control moment gyroscope
real time windows target
linear quadratic regulator
controller design
