The parameters optimisation design for variable speed control momentum gyroscopes

Control momentum gyroscopes (CMGs) have many advantages over other actuators for the attitude control of a spacecraft. Compared with the single-gimbal control moment gyroscopes (SGCMGs), the mass and power of the flywheel of variable-speed control moment gyroscopes (VSCMGs) are greatly increased. In...

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Bibliographic Details

Published in:	International journal of control Vol. 90; no. 12; p. 2618
Main Authors:	Liu, Feng, Zhao, Hui, Yao, Yu, Guo, Yang, Wang, Long
Format:	Journal Article
Language:	English
Published:	Abingdon Taylor & Francis Ltd 01.12.2017
Subjects:	Control moment gyroscopes Design optimization Design parameters Flywheels Gyroscopes Laws Lower bounds Multiple objective analysis Product design Programming Spacecraft attitude control Speed control Steering
ISSN:	0020-7179, 1366-5820
Online Access:	Get full text
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