Journal of System Simulation
Abstract
Abstract: To improve the universality and handling quality of control system of helicopter flight simulator, a universal control load system of helicopter flight simulator suitable for helicopter flight simulator is designed. The dynamic feedback model is proposed to solve the contradiction between control rigidity and stability, control precision and response frequency, the control rigidity and kinematic accuracy are improved.The operating load mechanism is designed, the system structure and drive system are simplified, the smoothness of force perception is improved; the third order smoothing algorithm and fieldbus technology based on EtherCAT are applied to improve the anti-jamming capability and response speed, the flexibility of control system is enhanced.
Recommended Citation
Zhen, Chen; Yang, Haikuan; Nan, Jiang; Wang, Yuancheng; and Jiang, Tianjiao
(2019)
"Design of Universal Control Load System of Helicopter Flight Simulator,"
Journal of System Simulation: Vol. 31:
Iss.
11, Article 26.
DOI: 10.16182/j.issn1004731x.joss.19-FZ0333
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol31/iss11/26
First Page
2408
Revised Date
2019-07-16
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.19-FZ0333
Last Page
2412
CLC
TP29
Recommended Citation
Chen Zhen, Yang Haikuan, Jiang Nan, Wang Yuancheng, Jiang Tianjiao. Design of Universal Control Load System of Helicopter Flight Simulator[J]. Journal of System Simulation, 2019, 31(11): 2408-2412.
DOI
10.16182/j.issn1004731x.joss.19-FZ0333
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