CAJ | 학술논문

针对直接在无人机上验证飞行控制系统成本较高，危险性较大，且受场地限制的问题，设计了一种针对小型无人机的三轴飞行仿真转台。介绍三轴转台主要性能指标和转台结构，对伺服控制系统和伺服软件系统2个方面进行分析，编写了设计程序。分析结果表明：该转台具有体积小、成本低、精度高、使用方便等特点，为小型无人机控制系统的研究提供了一个地面半仿真实验的平台。
침대직접재무인궤상험증비행공제계통성본교고，위험성교대，차수장지한제적문제，설계료일충침대소형무인궤적삼축비행방진전태。개소삼축전태주요성능지표화전태결구，대사복공제계통화사복연건계통2개방면진행분석，편사료설계정서。분석결과표명：해전태구유체적소、성본저、정도고、사용방편등특점，위소형무인궤공제계통적연구제공료일개지면반방진실험적평태。
Flight tests on UAV flight control system is high-cost, dangerous and restricted. For this reason, a new 3-axis flight simulator is designed for the research of a small UAV. Performance index and structure of flight simulator is introduced. The control system and software system is analyzed, and the program is written. The analysis shows that the simulator has the features of small volume, low cost, high precision and convenient using, and a half-physical simulation platform is provided for a small UAV flight control system.