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基于鲁棒显模型跟踪的共轴高速直升机飞/发综合控制OA

Integrated flight/propulsion control of coaxial high-speed helicopter based on robust explicit model following control

中文摘要英文摘要

多飞行模态和高机动性是共轴高速直升机的典型特征,常规的飞/发分离控制策略难以满足高性能控制需求;同时,全包线范围内的高动态耦合、强外部干扰与时变飞行特性对控制策略的鲁棒性提出了严峻挑战.因此,提出了一种基于鲁棒显模型跟踪控制(REMFC)的飞/发综合控制架构.首先,基于旋翼与发动机的扭矩/转速关系,构建了包含共轴直升机、涡轴发动机和传动系统的飞/发综合仿真模型.其次,通过重构显模型跟踪控制前馈-反馈结构并引入扩张状态观测器(ESO),提出了一种鲁棒显模型跟踪控制策略,实现了对未建模动态、气动干扰及参数不确定性的在线估计与补偿,并证明了闭环跟踪误差一致有界.最后,基于鲁棒显模型跟踪控制策略,设计了飞/发综合控制律并实现了飞行操纵与发动机转速的综合控制与动态协调.全飞行包线内的多任务仿真结果表明,基于鲁棒显模型跟踪的共轴高速直升机飞/发综合控制方法在参考指令跟踪、扰动抑制和转速稳定性方面均优于传统方法,显著提升了共轴高速直升机在复杂飞行条件下的飞行性能与鲁棒性.

Multiple flight modes and high maneuverability are typical characteristics of coaxial high-speed helicopters,making conventional separated flight/propulsion control strategies insufficient to satisfy high-performance control re-quirements.Meanwhile,the pronounced dynamic coupling across the entire flight envelope,together with strong ex-ternal disturbances and time-varying flight characteristics,poses severe challenges to the robustness of control strate-gies.To address these issues,this paper proposes an integrated flight/propulsion control architecture based on Ro-bust Explicit Model Following Control(REMFC).First,based on the torque-speed relationships between the rotor and the engine,an integrated flight/propulsion simulation model is established,incorporating the coaxial helicopter,turbo-shaft engine,and transmission system.Subsequently,by reconstructing the feedforward-feedback structure of explicit model following control and introducing an Extended State Observer(ESO),a robust explicit model following control strategy is developed.The proposed method achieves online estimation and compensation of unmodeled dynamics,aerodynamic disturbances,and parameter uncertainties,and the uniform boundedness of the closed-loop tracking er-ror is theoretically guaranteed.Finally,based on the proposed REMFC strategy,an integrated flight/propulsion control law is designed to realize coordinated control and dynamic regulation of flight manipulation and engine speed.Multi-mission simulation results over the entire flight envelope demonstrate that the REMFC-based integrated control ap-proach for coaxial high-speed helicopters outperforms conventional methods in reference command tracking,distur-bance rejection,and rotor speed stabilization,significantly improving flight performance and robustness under complex flight conditions.

王重;任众孚;白俊强;郎金溪;李俨

西北工业大学 自动化学院,西安 710072西北工业大学 自动化学院,西安 710072西北工业大学 无人系统技术研究院,西安 710072西北工业大学 自动化学院,西安 710072西北工业大学 自动化学院,西安 710072

航空航天

共轴高速直升机鲁棒控制显模型跟踪控制扩张状态观测器飞/发综合控制

coaxial high-speed helicopterrobust controlexplicit model tracking controlextended state observerintegrated flight/propulsion control

《航空学报》 2026 (7)

80-100,21

国家自然科学基金(62403385,62573353)中央高校基本科研业务费专项资金飞行器数字敏捷设计全国重点实验室开放基金 National Natural Science Foundation of China(62403385,62573353)Fundamental Research Funds for the Central UniversitiesOpen Funding of National Key Laboratory of Digital and Agile Aircraft Design

10.7527/S1000-6893.2026.32745

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