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Featured researches published by Zhang Jiyang.


chinese control and decision conference | 2017

A novel suspended method based on flux density feedback for AMB system without position sensors

Wang Yingguang; Fan Yahong; Lu Ming; Xu Xiangbo; Liu Hu; Wu Dengyun; Zhang Jiyang

A novel suspended method based on flux density feedback for AMB system without position sensors is presented in this paper. Ultra-thin Hall sensor is a part of the flux density feedback control with the function of detecting the flux density. According to the model of AMB rotor, position control-loop is realized with rotor position resolved from magnetic flux density and winding current. Flux density feedback control eliminates the model error caused by the inconsistencies between sensor target and AMB. With the novel approach, position sensors and detection target are not required; besides, size and weight of AMB system are reduced. It is of great benefit to miniaturization and integration for the space AMB system.


international conference on mechatronics and automation | 2016

Research on high accuracy, long life, and high reliability technique of control moment gyroscope

Li Gang; Wu Dengyun; Lu Ming; Lai Lin; Tian Xing; Zhang Jiyang

The control moment gyroscope (CMG), which has the capability to produce large, continuously adjustable torques, is a key attitude control actuator for a spacecraft. The rotor spins at a constant rate about the rotor axis. Any rotation of the gimbal causes a change in the angular momentum of the spacecraft, which produces the gyroscopic moment for attitude control. On September, 2011, 200Nms CMGs were carried in orbit onboard Tiangong target spacecraft of China, which was the first inorbit application of independently developed CMG of China. 200Nms CMGs are designed for the attitude control of middle size spacecraft. Since then, even larger CMGs were under development to meet the demand of the attitude control for even larger spacecraft, such as the space station of China. In this research, three techniques are developed: System redundancy technique, for all electrical components and control electronics; Long life flywheel shafting lubrication technique, with screw cap shaped oil reservoir for 15 years long life lubrication; High stiffness gimbal drive and high accurate control technology, with harmonic reducer, and disturbance observer based terminal sliding mode control. The prototype of 1000Nms CMG was developed, and has successfully passed the qualification level environmental test.


Archive | 2013

Moment control gyro frame disturbance moment restraining method

Lu Ming; Li Gang; Zhang Jiyang; Wu Dengyun; Li Lianxiang; Zhai Baichen; Tian Limei; Hu Yuewei; Ma Wendong


Archive | 2014

Flywheel body with shock absorber

Wu Jintao; Qing Tao; Wang Yanrong; Liu Bin; Zhang Jiyang; Wu Dengyun; Wang Quanwu; Wang Hong; Luo Ruizhi; Zhou Ningning


Archive | 2016

Control system and control method for CMG framework permanent magnet synchronous motor

Lu Ming; Hu Yuewei; Wang Yingguang; Tian Limei; Li Gang; Tian Xing; Ma Wendong; Wu Dengyun; Zhang Jiyang


Archive | 2015

Ultralow rotation speed control method of ultrasonic motor

Zhao Lei; Wu Jintao; Zhai Baichen; Zhang Jiyang; Qing Tao; Wu Dengyun


Archive | 2015

High-reliability high-stability-degree hollow rotating traveling wave ultrasonic motor

Wu Jintao; Zhu Hua; Niu Zijie; Zhao Lei; Zhang Jiyang; Wu Dengyun; Qing Tao; Zhao Chunsheng; Ding Qingjun


Archive | 2014

Small-size speed change control moment gyroscope

Wu Jintao; Zhao Lei; Fu Rong; Zhang Jiyang; Wu Dengyun; Qing Tao; Wei Dazhong; Wang Quanwu; Zhou Gang; Luo Ruizhi


Archive | 2017

Three-freedom magnetic levitation station for full-physical simulation of gesture control system

Wang Yingguang; Fan Yahong; Chen Chen; Wu Dengyun; Zhang Jiyang; Tian Xing; Shi Meihua


Archive | 2016

Flux-density-feedback-based magnetic-levitation micro vibration control system

Wang Yingguang; Fan Yahong; Lu Ming; Wu Dengyun; Zhang Jiyang; Tian Limei; Hu Yuewei; Shi Meihua

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Wu Dengyun

China Aerospace Science and Technology Corporation

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Lu Ming

China Aerospace Science and Technology Corporation

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Li Gang

China Aerospace Science and Technology Corporation

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Tian Xing

China Aerospace Science and Technology Corporation

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Lai Lin

China Aerospace Science and Technology Corporation

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Niu Zijie

Nanjing University of Aeronautics and Astronautics

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