Manifold path selection steering law for pyramid-type single-gimbal control moment gyros

2020 ◽  
Vol 106 ◽  
pp. 106207
Author(s):  
Jitang Guo ◽  
Yunhai Geng ◽  
Baolin Wu ◽  
Xianren Kong
2016 ◽  
Vol 39 (4) ◽  
pp. 952-962 ◽  
Author(s):  
Takuya Kanzawa ◽  
Misuzu Haruki ◽  
Koji Yamanaka

Author(s):  
He ZHU ◽  
Weikui LIANG ◽  
Guangfu MA ◽  
Yanning GUO ◽  
Peng HAN
Keyword(s):  

Author(s):  
Jixiang Fan ◽  
Di Zhou

Dynamic equations describing the attitude motion of flexible spacecraft with scissored pairs of control moment gyroscopes are established. A nonlinear controller is designed to drive the flexible spacecraft to implement three-axis large-angle attitude maneuvers with the vibration suppression. Singularity analysis for three orthogonally mounted scissored pairs of control moment gyros shows that there exists no internal singularity in this configuration. A new pseudo-inverse steering law is designed based on the synchronization of gimbal angles of the twin gyros in each pair. To improve the synchronization performance, an adaptive nonlinear feedback controller is designed for each pairs of control moment gyros by using the stability theory of Lyapunov. Simulation results are provided to show the validity of the controllers and the steering law.


2017 ◽  
Vol 30 (5) ◽  
pp. 04017023 ◽  
Author(s):  
Yanning Guo ◽  
Hutao Cui ◽  
Guangfu Ma ◽  
Chuanjiang Li

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