@inproceedings{02c8f98a2da44b158493b09f59b5310f,
title = "Adaptive backstepping control of spacecraft attitude with Variable Speed Control Moment Gyroscopes",
abstract = "To implement the rapid maneuvering and high stability control of spacecraft attitude, Variable Speed Control Moment Gyroscopes(VSCMGs) is used to produce the attitude control moments. However, the dynamic characteristic of VSCMGs, external environment disturbances and consumption of fuels have significant influence to spacecraft attitude control system. Taking into account the uncertainty of inertia parameters and external environment disturbances, adaptive control system is devised on account of backstepping method, which can estimate the uncertain parameters and inhibit the effects to attitude control system effectively. The attitude angles and attitude angle speeds both have good tracking performance. Simulation results demonstrate the designed control strategy is available and feasible.",
keywords = "Attitude Control, Backstepping Control, Control Momentum Gyroscopes, Spacecraft",
author = "Zhong Wu and Zhen Wang and Yaping Yang and Lei Guo",
year = "2013",
month = oct,
day = "18",
language = "英语",
isbn = "9789881563835",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "1002--1006",
booktitle = "Proceedings of the 32nd Chinese Control Conference, CCC 2013",
address = "美国",
note = "32nd Chinese Control Conference, CCC 2013 ; Conference date: 26-07-2013 Through 28-07-2013",
}