Attitude control of a rigid spacecraft with one variable-speed control moment gyro

2013 ◽  
Vol 29 (5) ◽  
pp. 749-760 ◽  
Author(s):  
Hai-Chao Gui ◽  
Lei Jin ◽  
Shi-Jie Xu
2018 ◽  
Vol 55 (5) ◽  
pp. 1235-1247 ◽  
Author(s):  
Takahiro Sasaki ◽  
Takashi Shimomura ◽  
Hanspeter Schaub

2016 ◽  
Vol 2016 ◽  
pp. 1-13 ◽  
Author(s):  
Zhongyi Chu ◽  
Jing Cui

To satisfy the requirements for small satellites that seek agile slewing with peak power, this paper investigates integrated power and attitude control using variable-speed control moment gyros (VSCMGs) that consider the mass and inertia of gimbals and wheels. The paper also details the process for developing the controller by considering various environments in which the controller may be implemented. A fuzzy adaptive disturbance observer (FADO) is proposed to estimate and compensate for the effects of equivalent disturbances. The algorithms can simultaneously track attitude and power. The simulation results illustrate the effectiveness of the control approach, which exhibits an improvement of 80 percent compared with alternate approaches that do not employ a FADO.


2020 ◽  
Vol 173 ◽  
pp. 252-265 ◽  
Author(s):  
Daiki Higashiyama ◽  
Yasuhiro Shoji ◽  
Satoshi Satoh ◽  
Ichiro Jikuya ◽  
Katsuhiko Yamada

2021 ◽  
Author(s):  
HeokJune You ◽  
Geongsu Park ◽  
Kenwoo Kim ◽  
Dongwon Jung

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