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
相关论文
共 50 条
  • [31] A Attitude Control Method for Spacecraft Considering Actuator Constraint and Dynamics based Backstepping
    Huo, Xing
    Zhang, Aihua
    Zhang, Zhiqiang
    She, Zhiyong
    [J]. 2016 SEVENTH INTERNATIONAL CONFERENCE ON INTELLIGENT CONTROL AND INFORMATION PROCESSING (ICICIP), 2016, : 131 - 136
  • [32] Optimal Combined Attitude Control Method for Spacecraft Based on Minimum Energy Cost
    Ran Dechao
    Sheng Tao
    Chen Xiaoqian
    [J]. 2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 2356 - 2361
  • [33] An spacecraft attitude maneuver method based on ADRC
    Yao Yao
    Liu Lei
    Wang Yong-ji
    [J]. 2015 27TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2015, : 3032 - 3037
  • [34] Spacecraft control method for fast attitude maneuver and stabilization
    Lei, Yongjun
    Tan, Shuping
    Liu, Yiwu
    [J]. Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology, 2010, 30 (05): : 48 - 53
  • [35] Attitude control for spacecraft using pyramid-type variable-speed control moment gyros
    Higashiyama, Daiki
    Shoji, Yasuhiro
    Satoh, Satoshi
    Jikuya, Ichiro
    Yamada, Katsuhiko
    [J]. ACTA ASTRONAUTICA, 2020, 173 : 252 - 265
  • [36] Spacecraft Attitude Sliding Mode Control Method Design
    Zhang Luwen
    Bai Chengchao
    Guo Jifeng
    Zheng Han
    [J]. 2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 2355 - 2360
  • [37] Integrated control method for spacecraft considering the flexibility of the spacecraft bus
    Tang, Liang
    Guo, Zixi
    Guan, Xin
    Wang, Youyi
    Zhang, Kebei
    [J]. ACTA ASTRONAUTICA, 2020, 167 : 73 - 84
  • [38] On the magnetic attitude control for spacecraft via the ε-strategies method
    Smirnov, Georgi V.
    Ovchinnikov, Mikhail
    Miranda, Francisco
    [J]. ACTA ASTRONAUTICA, 2008, 63 (5-6) : 690 - 694
  • [39] MEASUREMENT OF THE PASSIVE ATTITUDE-CONTROL PERFORMANCE OF A RECOVERED SPACECRAFT
    GREGORY, JC
    PETERS, PN
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (01) : 282 - 284
  • [40] Attitude control of spacecraft simulator without angular velocity measurement
    Malekzadeh, Maryam
    Sadeghian, Hamid
    [J]. CONTROL ENGINEERING PRACTICE, 2019, 84 : 72 - 81
12345