[1]祖 鹏,唐宏清,李 康.旋翼操纵装置动力学建模与仿真分析[J].机械与电子,2026,44(08):96-102.
　ZU Peng,TANG Hongqing,LI Kang.Dynamic Modeling and Simulation Analysis of a Rotor Control Mechanism[J].Machinery & Electronics,2026,44(08):96-102.
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旋翼操纵装置动力学建模与仿真分析()
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《机械与电子》[ISSN:1001-2257/CN:52-1052/TH]

卷:
44
期数:
2026年08期
页码:
96-102
栏目:
飞行控制与导航
出版日期:
2026-08-25

文章信息/Info

Title:
Dynamic Modeling and Simulation Analysis of a Rotor Control Mechanism
文章编号:
1001-2257(2026)08-0096-07
作者:
祖 鹏; 唐宏清; 李 康
中国飞行试验研究院飞机所,陕西 西安 710089
Author(s):
ZU Peng; TANG Hongqing; LI Kang
(Aircraft Institute,Chinese Flight Test Establishment,Xi’an 710089,China)
关键词:
永磁同步电机; 线性自抗扰控制; 伺服电缸; 刚度模型
Keywords:
permanent magnet synchronous motor; linear active disturbance rejection control; servo electriccylinder; stiffness model
分类号:
V249.1
文献标志码:
A
摘要:
为进一步提升旋翼系统的控制精度,基于线性自抗扰控制(LADRC)理论,设计了一套针对集成同步带减速器的伺服电缸的半闭环控制系统。研究中分别建立了伺服电机的数学模型与含同步带传动环节的电缸动力学模型,并在MATLAB/Simulink环境中构建了完整的系统仿真平台。通过数值算例系统分析了同步带预紧力与电缸轴向负载对自动倾斜器运动行为的影响。仿真结果表明,在对旋翼进行总距操纵过程中,自动倾斜器会产生附加的倾斜角度,该附加倾角的大小与同步带预紧力及电缸轴向负载密切相关,揭示了柔性传动部件对旋翼桨叶操纵角操纵精度的影响机制。
Abstract:
To further enhance the control accuracy of rotor systems,a semi-closed-loop control system for a servo electric cylinder integrated with a synchronous belt reducer is designed,based on the Linear Active Disturbance Rejection Control (LADRC) theory.The mathematical model of servo motor and the dynamic model of electric cylinder,incorporating the synchronous belt transmission,are established,and a complete simulation platform is subsequently constructed in the MATLAB/Simulink environment.Numerical simulations are conducted to systematically investigate the effects of the synchronous belt preload and the axial load of the electric cylinder on the motion behavior of the swashplate.The simulation results reveal that during collective pitch control of the rotor,the swashplate produces an additional tilt angle,the magnitude of which is closely correlated with the synchronous belt preload and the axial load,thereby elucidating the influence mechanism of the flexible transmission components on the control accuracy of the rotor blade pitch angle.

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备注/Memo

备注/Memo:
收稿日期:2026-04-26
作者简介:祖 鹏 (2000-),男,山西灵丘人,硕士,工程师,研究方向为直升机试飞,通信作者,E-mail:2080186656@qq.com。
更新日期/Last Update: 2026-08-28