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Quadrotor UAV dynamics modeling based on subspace identification system

机译:基于子空间识别系统的四旋翼无人机动力学建模

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This paper proposes the development of a dynamic model of a quadrotor UAV through input/output data sets using Subspace identification as a black-box identification type. Subspace identification is suitable for Multi Input-Multi-Output (MIMO) systems. After the identification, the resulting model will be used in an LQR control scheme. Due to the instability nature of quadrotor UAV's, the identification has been performed in close loop conditions. In order to validate the presented identification technique, simulations were carried out on a model of a real quadrotor and a comparison was made against real data taken from operating the real quadrotor. The data used in the simulations are real data collected by real experimentation.
机译:本文提出了使用子空间识别作为黑匣子识别类型通过输入/输出数据集开发四旋翼无人机动力学模型的方法。子空间识别适用于多输入多输出(MIMO)系统。识别后,结果模型将用于LQR控制方案中。由于四旋翼无人机的不稳定性,已经在闭环条件下进行了识别。为了验证所提出的识别技术,对真实四旋翼飞机的模型进行了仿真,并与实际四旋翼飞机的实际数据进行了比较。在模拟中使用的数据是通过真实实验收集的真实数据。

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