Journal of System Simulation ›› 2019, Vol. 31 ›› Issue (11): 2408-2412.doi: 10.16182/j.issn1004731x.joss.19-FZ0333

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Design of Universal Control Load System of Helicopter Flight Simulator

Chen Zhen1, Yang Haikuan1, Jiang Nan1, Wang Yuancheng1, Jiang Tianjiao2   

  1. 1. Training Department of Bomber and Transport Aircraft Pilots, 93199 Troops, Harbin 150001, China;
    2. 95801 Troops, Beijing 100843, China
  • Received:2019-05-30 Revised:2019-07-16 Online:2019-11-10 Published:2019-12-13

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.

Key words: helicopter flight simulator, control load system, dynamic feedback, operating load mechanism, third order smoothing algorithm

CLC Number: