Identification of quadcopter hovering using experimental data

Iyad Salameh, Emad M. Ammar, T. Tutunji
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引用次数: 14

Abstract

Obtaining the plants' mathematical models using physical laws is essential in the development and design of suitable controllers. However, sometimes these models can be complex, inaccurate, or difficult to find. In such cases, mathematical models can be build using experimental data that approximate the real system's behavior. The quadcopter is one such example where the relationship between its inputs and outputs is nonlinear, complex, and dependent on several difficult-to-measure parameters. In this paper, a quadcopter is assembled, tested, and used in several flight experiments where the Input-Output (I/O) data is collected and used to develop accurate mathematical models of the quadcopter for hovering operation. Auto-Regressive with eXogenous (ARX) based models, for both Single-Input Single-Output (SISO) and Multi-Input Multi-Output (MIMO), are developed and analyzed. Results show that the developed models provide good accuracy when compared to the experimental measurements.
利用实验数据识别四轴飞行器悬停
利用物理定律获得被控对象的数学模型对于开发和设计合适的控制器至关重要。然而,有时这些模型可能是复杂的、不准确的或难以找到的。在这种情况下,可以使用接近真实系统行为的实验数据建立数学模型。四轴飞行器就是这样一个例子,它的输入和输出之间的关系是非线性的,复杂的,并且依赖于几个难以测量的参数。在本文中,四轴飞行器组装,测试,并在几个飞行实验中使用,其中输入输出(I/O)数据被收集并用于开发四轴飞行器悬停操作的精确数学模型。针对单输入单输出(SISO)和多输入多输出(MIMO)模型,开发并分析了基于外生(ARX)的自回归模型。结果表明,所建立的模型与实验测量值相比具有较好的精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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