1) tiltrotor aircraft
倾转旋翼飞机
1.
Flight control of tiltrotor aircraft in helicopter mode with nacelle tilting;
倾转旋翼飞机直升机模态短舱倾转飞行控制
2.
This paper introduces the VTOL technology and studies the helicopter mode and the airplane mode of the tiltrotor aircraft.
对倾转旋翼飞机的技术基础——推力矢量技术进行了介绍,分析了倾转旋翼飞机直升机模态和固定翼飞机模态的工作特点;针对倾转旋翼飞机的概念、方案进行了论述,并提出了倾转旋翼飞机的技术规格要求;总结了倾转旋翼飞机的技术发展历程、技术方案演变及各发展阶段的特点,并展望了其应用前景。
2) tiltrotor
倾转旋翼机
1.
The parameter uncertainty in tiltrotor model caused by the variation of nacelle angle was considered in controller designing for flight mode conversion of tiltrotor.
针对倾转旋翼机过渡段模型参数摄动问题,在状态方程描述的框架下,用线性分式变换形式将模型参数摄动表示为对角块结构,采用μ综合方法设计了倾转旋翼机过渡段飞行控制器。
2.
The airplane mode s model of tiltrotor was founded.
建立倾转旋翼机飞机模式的分析模型,分析系统的频率和阻尼特性,揭示了对系统稳定性起主要作用的一些模态;分析了旋翼摆振运动、机翼气动力和自转状态假设对系统稳定性的影响;分析了系统一些重要参数,如桨叶固有频率和机翼固有频率,对系统回转颤振稳定性的影响。
3.
The multi-body analysis of the aeroelastic stability of the tiltrotor aircraft is presented.
通过多体动力学方法建立了倾转旋翼机动力学分析模型。
3) tiltrotor aircraft
倾转旋翼机
1.
Dynamic stability analysis of tiltrotor aircraft in forward flight;
倾转旋翼机前飞动力学稳定性分析
2.
Considering the characteristics of the thrust vector/aerodynamic force multiple control for tiltrotor aircraft, this paper,based on the model of the tiltrotor aircraft, designs the flight control system using variable structure control with sliding mode.
文中针对倾转旋翼机拉力矢量/气动力组合控制的特点,在完成倾转旋翼机建模的基础上,采用滑模变结构控制对飞行控制系统进行了设计。
3.
In this paper the flight control system of tiltrotor aircraft is designed by using linear model following method to resolve the coupling of lateral channel.
文中针对倾转旋翼机横侧向飞行控制系统的耦合问题,应用线性模型跟随法进行控制器的设计。
4) tilt-rotor
倾转旋翼机
1.
Natural characteristic analyse of the transmission of Tilt-Rotor;
某型倾转旋翼机传动系统固有特性分析
2.
Dynamic response analysis of the transmission of tilt-rotor in different modes;
倾转旋翼机传动系统多状态响应特性研究
3.
Modeling study on tilt-rotor's aeroelastic stability in cruise flight
前飞状态倾转旋翼机气弹稳定性建模
5) tilt rotor aircraft
倾转旋翼机
1.
Modeling of a tilt rotor aircraft platform;
倾转旋翼机模拟平台建模与仿真
2.
An adaptive neural networks controller is designed for tilt rotor aircraft platform.
采用自适应神经网络控制方法,设计出倾转旋翼机模拟平台姿态角控制器。
3.
The flight dynamic equations of tilt rotor aircraft are studied,and the flight dynamically mathematical model for the helicopter,tilting and airplane flight modes is established.
研究了倾转旋翼机的飞行数学方程,建立了小型无人倾转旋翼机在直升机、倾转及飞机飞行模式的飞行力学仿真模型,计算得出配平工作点处各通道的操纵量和飞行器的飞行姿态,通过各飞行模式的仿真结果确定了该飞行器的全模式飞行策略,飞行试验表明仿真结果符合倾转旋翼机的飞行特性。
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条