Modeling and Simulation of Wing Bending Simulation System

ZHAO Mengwen; FAN Zeming

doi:10.13433/j.cnki.1003-8728.20230337

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Modeling and Simulation of Wing Bending Simulation System

更新时间：2026-07-10

- Modeling and Simulation of Wing Bending Simulation System
- Mechanical Science and Technology for Aerospace Engineering Vol. 43, Issue 2, Pages: 305-311(2024)
- 作者机构：
  
  1. 西安航空学院机械工程学院,西安,710077
  2. 西北工业大学自动化学院,西安,710072
- 作者简介：
- 基金信息：
- DOI：10.13433/j.cnki.1003-8728.20230337
  CLC：
- Online First：01 February 2024，
  
  Published：2024
- 稿件说明：
移动端阅览
ZHAO Mengwen, FAN Zeming. Modeling and Simulation of Wing Bending Simulation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2024, 43(2): 305-311.
DOI：

ZHAO Mengwen, FAN Zeming. Modeling and Simulation of Wing Bending Simulation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2024, 43(2): 305-311. DOI： 10.13433/j.cnki.1003-8728.20230337.

摘要

某型飞机在飞行过程中，机翼将产生最大可达3米的变形，该变形将严重影响安装在飞机机翼上钢索传动装置的操控性能，同时考虑操控性能在真实飞行过程中的成本、难度、风险问题，构建了地面机翼弯曲模拟系统。首先，构建了由16套机构组成的全机翼半物理仿真模型

各机构均安装有一套位移伺服控制系统和一套角度伺服控制系统。然后对系统的角度控制及位移控制进行了建模、仿真研究，提出了有效的前馈和模糊控制相结合的控制策略。最后搭建了实验验证系统并进行了验证。结果表明：该系统设计合理，实用性强，满足钢索在机翼弯曲变形下的操控性能测试。

Abstract

In the flight of a certain aircraft

the maximum deformation of the wing will be up to 3 meters

which will seriously affect the handling performance of the steel cable transmission device installed on the aircraft wing. Considering the cost

difficulty and risk of handling performance in the real flight

a ground wing bending simulation system is constructed. Firstly

a semi-physical simulation model for the whole wing is constructed

which consists of 16 sets of mechanisms. Each mechanism is equipped with a set of displacement servo control system and an angle servo control system. Then

the angle control and displacement control of the wing bending simulation system are modeled and simulated

and an effective control strategy by combining feedforward and fuzzy control is put forward. Finally

an experimental verification system is built to verify the rationality of the simulation system. The results show that this system is reasonable in design and strong in practicability

and can meet the test of steel cable handling performance under wing bending deformation.

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Related Author

戴永彬

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ZHAO Mingji

WANG Fazhan

HUANG Kepeng

Related Institution

College of New Energy, Liaoning University of Technology

School of Mechanical and Electrical Engineering, Xi'an University of Architecture and Technology

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