航空工程进展2026，Vol.17Issue(1)：39-50,12.DOI:10.16615/j.cnki.1674-8190.2026.01.04
新型双轴倾转旋翼飞行器总体设计与控制分析
Overall design and control analysis of a novel dual-axis tilt-rotor aircraft
摘要
Abstract
The tilt-rotor aircraft combines the capabilities of vertical takeoff and landing with efficient high-speed cruising,making it suitable for short-haul low-altitude transportation.However,the overall design of existing tilt-rotor aircraft does not consider the safety of forced landings during short-haul transport,and both the overall layout and control strategies need optimization.This paper presents the design of a novel dual-axis tilt-rotor aircraft.By comprehensively considering the integration of rotor blades and multiple flight modes,the overall layout of the air-craft is optimized.This enables the aircraft to perform a forced landing in fixed-wing mode on a single lane of a ground roadway with minimal impact on ground traffic,while still carrying a sufficiently large payload.Furthermore,a six-degree-of-freedom dynamic and kinematic model of the aircraft is established.A control analysis of the six-degree-of-freedom flight under the new layout of the aircraft is conducted,and a new control strategy is proposed.The feasibility of the new control strategy is verified through dynamic simulation.The results show that the proposed aircraft,with a properly optimized configuration,exhibits the potential to enhance aerodynamic efficiency,leverage the advantages of rotor-wing integration,and demonstrates favorable control characteristics.The aircraft design scheme can provide a reference for the development of tilt-rotor aircraft designed for low-altitude operations.关键词
倾转旋翼飞行器/桨翼融合/总体布局设计/飞行力学/飞行控制Key words
tilt-rotor aircraft/blade-wing integration/overall layout design/flight mechanics/flight control分类
航空航天引用本文复制引用
邓礼,陆冬平,张伟,王楠,雷宗霖,颜郡泽,杨剑挺..新型双轴倾转旋翼飞行器总体设计与控制分析[J].航空工程进展,2026,17(1):39-50,12.基金项目
云南省兴滇人才青年人才及其后续支持项目(YNQR-QNRC-2019-047) （YNQR-QNRC-2019-047）
