Measurement and control integrated method for spacecraft attitude based on MSCMGs with pyramid configuration

被引：3
|
作者：
Wang, Ping [1 ]
Wang, Hua [2 ]
Ren, Yuan [2 ]
机构：
[1] College of Postgraduate, Academy of Equipment, Beijing,101416, China
[2] Department of Space Equipment, Academy of Equipment, Beijing,101416, China
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2016年 / 38卷 / 01期
关键词：
Magnetism - Angular velocity - Magnetic actuators - Spacecraft - Suspensions (components) - Magnetic bearings - Gyroscopes - Integrated control;
D O I：
10.3969/j.issn.1001-506X.2016.01.20
中图分类号：
学科分类号：
摘要：
A measurement and control integrated method of spacecraft attitude based on magnetically suspended control moment gyroscope (MSCMG) of pyramid configuration is proposed. The actuator in attitude control loop is used to measure and control spacecraft attitude, thus breaking the traditional attitude control loop which is composed by attitude sensor, controller, actuator. The radial torque model of the magnetic suspension rotor is established firstly, real-time detect magnetic bearing current, magnetic suspension rotor displacement and the frame angular velocity in MSCMG, get spacecraft attitude angular velocity through simultaneous three radial torque model in pyramid configuration. Then the control law of attitude and steering law of framework is designed to realize spacecraft attitude regulation. The simulation results show the effectiveness and superiority of this method. © 2016, Chinese Institute of Electronics. All right reserved.
引用
收藏
页码：123 / 129
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