多旋翼式无人飞行器系统设计研究  

Design of Multiple Rotor Unmanned Aerial Vehicle System

作　　者：程荣涛[1] 马恒[2] 王荣颖[2] 范松伟 

机构地区：[1]海军驻武汉四三八厂军事代表室,武汉430060 [2]海军工程大学导航工程系,武汉430033

出　　处：《舰船电子工程》2017年第4期1-4,17,共5页Ship Electronic Engineering

摘　　要：多旋翼式无人飞行器相对其他飞行器具有能够垂直起降以及操控简单等优点,在军事任务中具有很大的应用前景。为此,论文设计了一种舰用多旋翼无人飞行器系统。首先提出了多旋翼式无人飞行器的设计指标,然后按照该设计指标对多旋翼式无人飞行器系统进行总体的设计,最后通过半实物仿真实验以及原型样机飞行试验,验证了所设计系统的可行性。Comparing with other unmanned aerial vehicles,multiple rotor unmanned aerial vehicles have the advantages that it has the ability of vertical take-off and landing and can be controlled easily,thus having great application prospect in military tasks.As a result,this paper designs a system of multiple rotor unmanned aerial vehicle.At first,the design indicators of rotor unmanned spacecraft are presented in this paper.Then according to the design index,the overall design of multiple rotor unmanned aircraft system is carried out.Finally through the simulation experiment and the prototype flight test,the feasibility of the designed system is verified.

关 键 词：多旋翼式无人飞行器 设计指标 系统设计 飞行试验 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]