@inproceedings{e62026e1d14146d6b9567440b84edd29,
title = "The design, test and on-orbit application of a gimbal control system for mini-variable speed control moment gyroscope",
abstract = "The China's first mini-Variable Speed Control Moment Gyroscope (VSCMG) had been launched with Super View-1 in December 28, 2016, which signals successfully application of on-orbit. Here the paper focuses on design, test and on-orbit application of gimbal control system for mini-VSCMG. A Permanent Magnet Synchronous Motor(PMSM) and an absolute-inductosyn is employed to constitute a gimbal angular rate closed-loop control system, with which, high performance is obtained within the angular-rate ranged from 0.01-60 deg./s and the high speed stability is validated to be better than 0.005 deg./s. Besides, a high dynamic response of gimbal performance that above 50Hz is realized by a composite controller. Furthermore, a dual range current detection circuit has been used to improve the control stability of gimbal angular rate over 10%. Moreover, with this gimbal control system, a 20 degrees of attitude maneuvering is able to completed within 17 seconds while the stabilization of satellites is superior to 0.0001deg./s.",
author = "Zhao Lei and Wei Wenshan and Dai Yaping and Zhai Baichen and Wu Jintao and Zhang Jiyang and Guan Xin",
note = "Publisher Copyright: {\textcopyright} 2018 KASHYAP.; 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 ; Conference date: 21-05-2018 Through 23-05-2018",
year = "2018",
language = "English",
isbn = "9780877036531",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "1019--1027",
editor = "Jeng-Shing Chern and Ya-Zhong Luo and Xiao-Qian Chen and Lei Chen",
booktitle = "Dynamics and Control of Space Systems",
address = "United States",
}