直升机飞行模拟器通用型操纵负荷系统设计

doi:10.16182/j.issn1004731x.joss.19-FZ0333

系统仿真学报 ›› 2019, Vol. 31 ›› Issue (11): 2408-2412.doi: 10.16182/j.issn1004731x.joss.19-FZ0333

直升机飞行模拟器通用型操纵负荷系统设计

陈珍¹, 杨海宽¹, 姜南¹, 王元诚¹, 江天娇²

1. 93199部队轰运飞行人员改装系,黑龙江哈尔滨 150001;
2. 95801部队,北京 100843

收稿日期:2019-05-30 修回日期:2019-07-16 出版日期:2019-11-10 发布日期:2019-12-13
作者简介:陈珍(1989-),女,内蒙古巴彦淖尔,硕士,研究方向为飞机动力装置、飞行模拟器仿真;杨海宽(1983-),男,河北保定,硕士,研究方向为飞行模拟器仿真。

Design of Universal Control Load System of Helicopter Flight Simulator

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

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

摘要/Abstract

摘要： 为解决直升机飞行模拟器操纵负荷系统的通用性及操纵品质问题,设计了适用于直升机飞行模拟器的通用型操纵负荷系统。提出了动态反馈控制模式,解决了控制刚度与系统稳定性、控制精度与响应频率之间的矛盾,有效提高了控制刚度及运动精度;研发了力加载机构,结合三阶平滑算法,简化了系统机械结构和传动环节,改善了力感平滑度;采用了三阶平滑算法和基于EtherCAT现场总线的数字控制技术,提高了系统的抗干扰能力及响应速度,增强了系统控制的灵活性。

关键词: 直升机飞行模拟器, 操纵负荷系统, 动态反馈控制, 力加载机构, 三阶平滑算法

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

中图分类号:

TP29

陈珍, 杨海宽, 姜南, 王元诚, 江天娇. 直升机飞行模拟器通用型操纵负荷系统设计[J]. 系统仿真学报, 2019, 31(11): 2408-2412.

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.

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直升机飞行模拟器通用型操纵负荷系统设计

Design of Universal Control Load System of Helicopter Flight Simulator

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