scholarly journals Gain-Scheduled Control/Steering Design for a Spacecraft with Variable-Speed Control Moment Gyros

2017 ◽  
Vol 10 (3) ◽  
pp. 237-242 ◽  
Author(s):  
Takahiro SASAKI ◽  
Takashi SHIMOMURA
Keyword(s):  
Speed Control ◽  
Variable Speed ◽  
Control Moment ◽  
Gain Scheduled ◽  
Variable Speed Control

Robust Attitude Control Using a Double-Gimbal Variable-Speed Control Moment Gyroscope

2018 ◽  
Vol 55 (5) ◽  
pp. 1235-1247 ◽  
Author(s):  
Takahiro Sasaki ◽  
Takashi Shimomura ◽  
Hanspeter Schaub
Keyword(s):  
Attitude Control ◽  
Speed Control ◽  
Variable Speed ◽  
Control Moment Gyroscope ◽  
Control Moment ◽  
Variable Speed Control

Convex Optimization for Power Tracking of Double-Gimbal Variable-Speed Control Moment Gyroscopes

2018 ◽  
Vol 55 (3) ◽  
pp. 541-551 ◽  
Author(s):  
Takahiro Sasaki ◽  
John Alcorn ◽  
Hanspeter Schaub ◽  
Takashi Shimomura
Keyword(s):  
Convex Optimization ◽  
Speed Control ◽  
Variable Speed ◽  
Control Moment ◽  
Control Moment Gyroscopes ◽  
Variable Speed Control

scholarly journals Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros

2016 ◽  
Vol 2016 ◽  
pp. 1-13 ◽  
Author(s):  
Zhongyi Chu ◽  
Jing Cui
Keyword(s):  
Attitude Control ◽  
Disturbance Observer ◽  
Peak Power ◽  
Speed Control ◽  
Variable Speed ◽  
Control Approach ◽  
Small Satellites ◽  
Control Moment ◽  
Fuzzy Adaptive ◽  
Variable Speed Control

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.

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