Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft  

小型无人倾转旋翼机飞行控制系统设计(英文)

作　　者：宋彦国[1] 王焕瑾[1] 

机构地区：[1]南京航空航天大学航空宇航学院直升机旋翼动力学国家级重点实验室

出　　处：《Chinese Journal of Aeronautics》2009年第3期250-256,共7页中国航空学报（英文版）

基　　金：National Natural Science Foundation of China (60705034)

摘　　要：A tilt rotor is an aircraft of a special kind, which possesses the characteristics of a helicopter and a fixed-wing airplane. However, there are a great number of important technical problems waiting for settlements. Of them, the flight control system might be a critical one. This article presents the progresses of the research work on the design of flight control system at Nanjing University of Aeronautics and Astronautics (NUAA). The flight control law of the tilt rotor aircraft is designed with the help ...A tilt rotor is an aircraft of a special kind, which possesses the characteristics of a helicopter and a fixed-wing airplane. However, there are a great number of important technical problems waiting for settlements. Of them, the flight control system might be a critical one. This article presents the progresses of the research work on the design of flight control system at Nanjing University of Aeronautics and Astronautics (NUAA). The flight control law of the tilt rotor aircraft is designed with the help ...

关 键 词：tilt rotor aircraft CONTROL aircraft models flight dynamics 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]