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Aerodynamic Model Analysis and Flight Simulation Research of UAV Based on Simulink

机译:基于Simulink的无人机气动模型分析与飞行仿真研究。

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摘要

Mathematical simulation method can be adopted to check flight characteristic of UAV, also can be adopted to simulate hardware experiments of unmanned aerial vehicle (UAV), then related flight experiments can be performed. The simulation method can reduce the flight periods, cost and risk. UAV flight model research play an important role in simulation and modeling in initialize periods of the UAV producing. The study of the paper focuses on the aerodynamic force modeling work of UAV based on Simulink. The designed model not only can afford mathematics simulation experiment but also will do benefits to the research of flight control, navigation guidance of UAV.
机译:可以采用数学模拟的方法来检查无人机的飞行特性,也可以采用模拟的方法对无人机进行硬件实验,然后进行相关的飞行实验。仿真方法可以减少飞行时间,成本和风险。无人机飞行模型研究在无人机生产初始化阶段的仿真和建模中起着重要作用。本文的研究重点是基于Simulink的无人机的空气动力建模工作。设计的模型不仅可以进行数学模拟实验,而且对无人机的飞行控制,导航制导等方面的研究也将有利。

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