摘要
针对倾转旋翼飞行器气动布局、桨翼融合及控制策略的优化问题,提出一种单轴倾转旋翼飞行器新型总体布局设计。在对飞行器进行六自由度建模的基础上,对飞行器飞行全过程进行了控制分析,并给出控制策略。对所设计飞行器的飞行全过程新型控制策略进行了仿真验证。研究结果表明,基于控制/气动一体化设计的单轴倾转旋翼飞行器新型布局,具有优良飞行控制性能的同时气动性能也得到了优化,可为未来单轴倾转旋翼飞行器的设计提供参考。
To address the optimization issues of tilt-rotor aircraft regarding aerodynamic configuration,propeller-wing fusion,and control strategies,a new overall layout design for a single-axis tiltrotor aircraft is proposed.On the basis of the six-degree-of-freedom modeling of the aircraft,the control analysis of the whole flight process of the aircraft was further carried out and the control strategy was presented.Simulation verification was carried out on the new control strategy for the entire flight process of the designed aircraft.The research results show that the new layout of the single-axis tiltrotor aircraft based on the control/aerodynamic integrated design not only achieves excellent flight control performance but also optimizes aerodynamic performance.This can provide a reference for the design of single-axis tilt-rotor aircraft in the future.
作者
黄雅婷
邓礼
张伟
田鏖
杨剑挺
HUANG Yating;DENG Li;ZHANG Wei;TIAN Ao;YANG Jianting(Faculty of Civil Aviation and Aeronautics,Kunming University of Science and Technology,Kunming 650500,China;Mile Hao Xiang Technology Co.,Ltd.,Mile 652300,China)
出处
《飞行力学》
北大核心
2026年第1期8-13,19,共7页
Flight Dynamics
基金
云南省兴滇人才青年人才及其后续支持项目资助(YNQR-QNRC-2019-047)。
关键词
倾转旋翼飞行器
总体布局设计
桨翼融合
飞行控制
tilt-rotor aircraft
general layout design
propeller-wing fusion
flight control
