Three axis electronic flight motion simulator real time control system design and implementation

2014 ◽  
Vol 85 (12) ◽  
pp. 125114 ◽  
Author(s):  
Zhiyuan Gao ◽  
Zhonghua Miao ◽  
Xuyong Wang ◽  
Xiaohua Wang
1995 ◽  
Author(s):  
N Coleman ◽  
A Paz ◽  
M DeVito ◽  
G Papanagopoulos ◽  
T-JLin, Yu, C-F

2011 ◽  
Author(s):  
Robin Hauser ◽  
Martin Kaegi ◽  
Dominik Gunsch ◽  
Mauritz van Schalkwyk ◽  
Peter Waelti ◽  
...  

2017 ◽  
Vol 40 (4) ◽  
pp. 1352-1361
Author(s):  
Zhonghua Miao ◽  
Chenglei Wei ◽  
Zhiyuan Gao ◽  
Xuyong Wang

Modelling of a three-axis electronic flight motion simulator with U-O-O structure is achieved in this paper, based on recursive Newton–Euler equations. To overcome the shortcomings of passive decoupling control methods, an active coupling torque suppression method is proposed using velocity internal feedback by analysing the influence of the coupling torque. Detailed control software and hardware implementation is given for the real-time control system. Experimental tests show the designed flight motion simulator system performs good dynamic and static performances.


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