[1]叶晓宇,祖家奎,秦 勇,等.倾转旋翼机直升机模式横航向通道解耦控制律设计[J].机械与电子,2025,(08):40-46.
　YE Xiaoyu,ZU Jiakui,QIN Yong,et al.Design of Decoupling Control Law of Lateral and Heading Channel for Tiltrotor Helicopter Mode[J].Machinery & Electronics,2025,(08):40-46.
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倾转旋翼机直升机模式横航向通道解耦控制律设计()
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《机械与电子》[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2025年08期
页码:
40-46
栏目:
自动控制与检测
出版日期:
2025-08-25

文章信息/Info

Title:
Design of Decoupling Control Law of Lateral and Heading Channel for Tiltrotor Helicopter Mode
文章编号:
1001-2257 ( 2025 ) 08-0040-07
作者:
叶晓宇; 祖家奎; 秦 勇; 位士超
南京航空航天大学自动化学院,江苏 南京 211106
Author(s):
YE Xiaoyu ;  ZU Jiakui ;  QIN Yong ;  WEI Shichao
( College of Automation Engineering , Nanjing University of Aeronautics and Astronautics , Nanjing 211106 , China )
关键词:
倾转旋翼机; 直升机模式; 横航向通道; 隐模型跟踪; 解耦控制
Keywords:
tiltrotor aircraft ;  helicopter mode ;  lateral and heading channel ;  implicit model following ;  decoupling control
分类号:
TP273 ;V249.1
文献标志码:
A
摘要:
针对倾转旋翼机独特的气动构型和复杂的气动特性带来的横航向通道强耦合问题,首先以 XV-15 倾转旋翼机为研究对象,建立其横航向数学模型,其次从定性和定量 2 个角度分析横航向通道的飞行特性与耦合特性。为保证倾转旋翼机直升机模式的飞行安全与控制性能,提出采用隐模型跟踪控制与经典 PID 控制相结合的方法进行横航向通道内外环控制律设计。最后基于 MATLAB / Simulink 搭建倾转旋翼机飞行控制仿真系统,将所设计的横航向通道控制律与常规 PID 控制方法进行仿真验证与对比分析。仿真结果表明,相比于常规 PID 控制,该控制系统可以实现横航向通道解耦控制,并具有更好的稳定性与动态响应特性。
Abstract:
In response to the strong coupling problem of the lateral and heading channel caused by the unique aerodynamic configuration and complex aerodynamic characteristics of tiltrotor aircraft , this paper first takes the XV-15 tiltrotor aircraft as the research object and establishes its lateral and heading mathematical model.Secondly , the flight characteristics and coupling characteristics of the lateral and heading channel are analyzed from both qualitative and quantitative perspectives.To ensure the flight safety and control performance of the tiltrotor helicopter mode , this paper proposes a method of combining implicit model following control with classical PID control for the design of control laws for the inner and outer loops of the lateral and heading channel.Finally , a tiltrotor aircraft flight control simulation system is built based on MATLAB / Simulink.The lateral and heading channel control law designed in this paper is verified and compared with the conventional PID control method through simulation and analysis.The simulation results show that compared with conventional PID control , this control system can achieve decoupling control of the lateral and heading channel and has better stability and dynamic response characteristics.

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备注/Memo

备注/Memo:
收稿日期: 2024-11-18
作者简介:叶晓宇 ( 2000- ),男,江苏苏州人,硕士研究生,研究方向为飞行控制、嵌入式系统;祖家奎 ( 1974- ),男,江苏徐州人,博士,副研究员,研究方向为飞行控制、嵌入式系统。
更新日期/Last Update: 2025-09-05