CAJ | 학술논문

针对某型无人机飞行设计要求，对无人机空中飞行进行模拟仿真，并综合测试仿真状态下的控制律运行情况。根据仿真试验的目的和要求，搭建适合无人机半实物仿真系统，介绍半实物仿真系统的组成；设计无人机的基本控制规律和逻辑，在此基础上建立某型无人机的简化数学模型，确定相关模型参数；对飞行控制系统进行仿真，构造某型无人机半实物仿真系统，并对无人机全飞行控制双机进行仿真试验、分析。试验结果表明：无人机飞行控制系统具有良好的控制效果，满足飞行控制要求。
침대모형무인궤비행설계요구，대무인궤공중비행진행모의방진，병종합측시방진상태하적공제률운행정황。근거방진시험적목적화요구，탑건괄합무인궤반실물방진계통，개소반실물방진계통적조성；설계무인궤적기본공제규률화라집，재차기출상건립모형무인궤적간화수학모형，학정상관모형삼수；대비행공제계통진행방진，구조모형무인궤반실물방진계통，병대무인궤전비행공제쌍궤진행방진시험、분석。시험결과표명：무인궤비행공제계통구유량호적공제효과，만족비행공제요구。
For a certain type of UAV design requirements, carry out the simulation of the UAV flight, and synthetically test the operation of the control law in simulation state. Firstly, according to the purpose and requirements of the simulation, set up a suitable UAV semi-physical simulation system and introduce the composition of the simulation system. Secondly, design a UAV control law and logic, and establish a simplified mathematical model of a UAV on this basis, and determine the relevant model parameters based on simulation requirements. Finally, construct a UAV semi-physical simulation system, underway the dual-UAV flight control simulation and analyze the simulation results. The test result shows that UAV flight control system has good control to meet the flight control requirements.