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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Vydané v:	International journal of control Ročník 90; číslo 12; s. 2618
Hlavní autori:	Liu, Feng, Zhao, Hui, Yao, Yu, Guo, Yang, Wang, Long
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Abingdon Taylor & Francis Ltd 01.12.2017
Predmet:	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
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