固定翼航模智能飞行控制系统  

Intelligent flight control system of fixed-wing aeromodel

作　　者：薛昕惟 黄彦淳 王祎[1] 夏秋粉[1] XUE Xinwei;HUANG Yanchun;WANG Yi;XIA Qiufen(International School of Information and Software Engineering,Dalian University of Technology,Dalian 116600,China)

机构地区：[1]大连理工大学国际信息与软件学院,辽宁大连116600

出　　处：《实验技术与管理》2020年第5期111-115,共5页Experimental Technology and Management

基　　金：大连理工大学教学改革基金项目(YB2019099,YB2019100);国家自然科学基金(61806036);辽宁省博士科研启动基金(201601051)。

摘　　要：根据对固定翼无人机飞行控制系统的实际民用需求,本文设计了固定翼航模智能飞行控制系统。详细说明了控制系统中飞行控制算法的设计与建立过程,以及从硬件和软件两方面对系统的设计和实现过程。该系统实现了两种飞行控制方式,即人工遥控控制飞行模式和控制系统自主控制飞行模式。其中人工遥控控制飞行模式是指操控者通过遥控控制模块对固定翼航模飞行姿态进行无限制的操控,从而完成各个飞行姿态的转换;控制系统自主控制飞行模式则是指固定翼航模在控制系统的控制下,自主进行稳定的直向飞行。该系统是一种低成本、高性能、高鲁棒性的通用固定翼航模飞控系统。According to the actual civil requirements of the flight control system of the fixed wing UAV(unmanned aerial vehicle),this paper designs the intelligent flight control system of the fixed-wing model.The design and establishment process of the flight control algorithm in the control system,as well as the design and implementation process of the system from the hardware and software aspects are described in detail.The system realizes two kinds of flight control modes,i.e.manual remote control flight mode and control system autonomous control flight mode.The manual remote control flight mode means that the controller controls the flight attitude of the fixed-wing model through the remote control module,so as to complete the conversion of each flight attitude,and the autonomous control flight mode of control system means that the fixed-wing model can independently and stably fly in a straight direction under the control system.This system is a general fixed-wing model flight control system with low cost,high performance and high robustness.

关 键 词：无人机 固定翼 飞行控制 

分 类 号：TP242.3[自动化与计算机技术—检测技术与自动化装置] G642.0[自动化与计算机技术—控制科学与工程]