| 倾转旋翼机过渡飞行阶段控制律设计研究 |
| |
| 引用本文： | 赖水清,严峰,徐珂.倾转旋翼机过渡飞行阶段控制律设计研究[J].直升机技术,2009(3). |
| |
| 作者姓名： | 赖水清 严峰 徐珂 |
| |
| 作者单位： | 中国直升机设计研究所,景德镇,333001 |
| |
| 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。
|
| 关 键 词： | 倾转旋翼机 过渡飞行段控制律 |
Design and Research of Control law for TiltRotor in Transition Flight Phase |
| |
| Authors: | LAI Shuiqing YAN Feng XU Ke |
| |
| Institution: | LAI Shuiqing; YAN Feng; XU Ke(China Helicopter Research and Development Institute; Jingdezhen; 333001); |
| |
| Abstract: | 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... |
| |
| Keywords: | tiltRotor control law in transition flight phase |
| 本文献已被 维普 万方数据 等数据库收录！ |
|
