摘要
过渡段飞行控制技术是倾转旋翼机飞行控制系统的关键技术。本文在倾转旋翼机过渡静力平衡特性和力矩配平特性分析基础上,对倾转旋翼机过渡段基准飞行轨迹及短舱转角规律进行了设计。然后利用推力矢量技术,采用拉力矢量/空气舵组合操纵方法,对倾转旋翼机过渡飞行段控制律进行了设计与仿真研究。
Control techniques in transition flight phase is the key techniques of TiltRotor flight control system.On the bases of the characteristic analyse of staticl balancing and moment balancing in transition flight phase of TiltRotor,this paper research reference flight paths and nacelle turning law in transition flight phase of TiltRotor.Then by using TVC technique,adopting pull vector/flap combining control mode,research the design of control law for TiltRotor in transition flight phase,and validate feasibility...
出处
《直升机技术》
2009年第3期52-55,共4页
Helicopter Technique
关键词
倾转旋翼机
过渡飞行段控制律
tiltRotor
control law in transition flight phase
