[1]秦 勇,祖家奎,位士超,等.复合式高速无人直升机纵向通道控制律设计[J].机械与电子,2025,(10):57-63.
　QIN Yong,ZU Jiakui,WEI Shichao,et al.Design for Longitudinal Channel Control Law of Compound Unmanned High-speed Helicopter[J].Machinery & Electronics,2025,(10):57-63.
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复合式高速无人直升机纵向通道控制律设计()
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《机械与电子》[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2025年10期
页码:
57-63
栏目:
智能制造
出版日期:
2025-10-25

文章信息/Info

Title:
Design for Longitudinal Channel Control Law of Compound Unmanned High-speed Helicopter
文章编号:
1001-2257 ( 2025 ) 10-0057-07
作者:
秦 勇; 祖家奎; 位士超; 叶晓宇
南京航空航天大学自动化学院,江苏 南京 211106
Author(s):
QIN Yong ;  ZU Jiakui ;  WEI Shichao ;  YE Xiaoyu
( College of Automation Engineering , Nanjing University of Aeronautics and Astronautics , Nanjing 211106 , China )
关键词:
复合式高速无人直升机; 特性分析; 操纵分配; 控制律设计
Keywords:
: compound high-speed unmanned helicopter ;  characteristics analysis ;  control allocation ;  control law design
分类号:
V249.1 ;TP391.9
文献标志码:
A
摘要:
针对复合式高速无人直升机前飞速度控制中的操纵舵面冗余问题,以某型复合式高速无人直升机为研究对象,建立其纵向通道动力学模型。分析纵向通道的飞行特性和纵向周期变距、螺旋桨平均桨距 2 种操纵舵面的差异,提出基于前飞速度的纵向通道操纵分配策略。分别对 2 种操纵舵面进行相关的控制律设计,并采用内外环并联的总体控制结构,以兼顾其机动性和稳定性。最后通过 MATLAB 仿真验证和实际飞行测试,证明该方法能够优化复合式高速直升机的纵向通道控制律,为其飞行控制系统的技术实现提供了理论支持和设计参考。
Abstract:
To address the control surface redundancy issue in forward speed control of compound high-speed unmanned helicopters , this study takes a specific model of a compound high-speed unmanned helicopter as the research object and establishes a longitudinal channel dynamic model.The flight characteristics of the longitudinal channel are analyzed , and the differences between two types of control surfaces longitudinal cyclic pitch and the average pitch of the propeller are compared.A control allocation strategy for the longitudinal channel based on forward speed is proposed.Control laws for two types of control surfaces are designed individually , and an integrated control structure with parallel inner and outer loops is adopted to balance maneuverability and stability.Finally , MATLAB simulations and actual flight tests are conducted to validate the effectiveness of the proposed method.The results demonstrate that the proposed approach optimizes the longitudinal control law of the compound high-speed helicopter and provides theoretical support and design references for the implementation of its flight control system.

参考文献/References:

[ 1 ] CHEN L B , LI T , LIU L J , et al.Trajectory tracking anti-disturbance control for unmanned aerial helicopter based on disturbance characterization index [ J ] . Control theory and technology , 2023 , 21 ( 2 ): 233-245.

[ 2 ] 何伟 . 复合式共轴高速直升机贴地飞行控制技术研究[ D ] . 南京:南京航空航天大学,2020.
[ 3 ] LAURIANE L , VIANNEY N , J?R?ME D , et al.Experi- mental velocity fields evaluation of the rotor / propeller interactions for high-speed helicopters with different propeller positions [ J ] .Experiments in fluids , 2022 , 63 ( 12 ): 1-3.
[ 4 ] CHEN C , YANG H X.Heading rate controller for unmanned helicopters based on modified ADRC [ J ] .Science China technological sciences , 2023 , 66 ( 5 ): 1255-1262.
[ 5 ] 李建波 . 复合式直升机技术发展分析[ J ] . 南京航空航天大学学报,2016 , 48 ( 2 ): 149-158.
[ 6 ] YANG K L , HAN D , SHI Q P.Study on the lift and propulsive force shares to improve the flight performance of a compound helicopter [ J ] .Chinese journal of aeronautics , 2022 , 35 ( 1 ): 149-158.
[ 7 ] BAGAI A.Aerodynamic design of the X2 technology demonstrator main rotor blade [ C ] ∥Proceeding of 64th Annual Forum of the American Helicopter Society , 2008 : 29-44.
[ 8 ] PERRY D.Battle of the Xs for airbus helicopters [ J ] . Flight international , 2019 , 195 : 12-30.
[ 9 ] 林李李 . 一种复合推力高速直升机操纵及控制技术研究[ D ] . 南京:南京航空航天大学,2020.
[ 10 ] 刘晓昕 . 一种复合推力高速直升机总体设计研究[ D ] .南京:南京航空航天大学,2020.
[ 11 ] 陆雅兰,曹东 . 复合式直升机过渡段横航向姿态解耦控制[ J ] . 电光与控制, 2023 , 30 ( 12 ): 86-92.
[ 12 ] 刘少兵 . 直升机自动向心回转控制律设计[ J ] . 中国科技信息,2022 , 676 ( 11 ): 105-109.
[ 13 ] 赵丹莉,王磊 . 直升机纵向姿态控制回路设计仿真[ J ] .中国科技信息,2020 ( 8 ): 44-45.
[ 14 ] 国防科学技术工业委员会 . 军用直升机飞行品质规范: GJB 902-90 [ S ] . 北京:国防科工委军标出版发行部,1990.

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备注/Memo

备注/Memo:
收稿日期: 2025-01-10
作者简介:秦 勇 ( 1999- ),男,安徽合肥人,硕士研究生,研究方向为飞行控制;祖家奎 ( 1974- ),男,江苏徐州人,博士,副研究员,研究方向为为无人机飞行控制与仿真技术、嵌入式系统。
更新日期/Last Update: 2025-11-13