DocumentCode
724322
Title
The research on flywheel acceleration assessment with null motion escaping singularity for variable speed control moment gyros
Author
Liu Feng ; Yao Yu ; Zhao Hui
Author_Institution
Control Simulation Center, Harbin Inst. of Technol., Harbin, China
fYear
2015
fDate
23-25 May 2015
Firstpage
3527
Lastpage
3532
Abstract
Compare with single gimbal control moment gyroscope, the variable flywheel speed of variable speed control moment gyroscope can be changed and easily realized, which have the ability of singular escaping. The flywheel acceleration and singularity problem are close connect with each other. In this paper, the flywheel acceleration index evaluation problem is solved with null motion to escaping the singular point. The mechanism of singular escaping is analyzed, and the process of singular escaping is revealed. The new null motion steering method is proposed, which is perpendicular to the gradient direction of null motion. The reasonable trajectory of gimbal position is planned. The optimal method is given to distribute the flywheel acceleration index with maximum escaping ability. The flywheel acceleration index assessment method is solved. The theory analysis result is foundation for the VSCMGs system optimization design.
Keywords
control system synthesis; flywheels; gradient methods; gyroscopes; machine control; optimisation; velocity control; VSCMG system optimization design; flywheel acceleration assessment; gradient direction; null motion escaping singularity; single gimbal control moment gyroscope; variable speed control moment gyros; Acceleration; Bandwidth; Flywheels; Planning; Servomotors; Torque; Trajectory; VSCMG cluster; flywheel acceleration assessment; pyramid configuration; singular escaping;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162534
Filename
7162534
Link To Document