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Multiexperiment data processing in identifying model helicopter's yaw dynamics

机译:识别模型直升机偏航动力学中的多因素数据处理

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The multi-experiment data is usually needed in identifying a model helicopter's yaw dynamics. In order to strengthen the information of the dynamics and reduce the effect of the noise, a new kind of least square method by using a weighted criterion is investigated to estimate the model parameters. To calculate the factors of the weighted criterion, a neural perceptron is trained to determine the factors automatically. The simulated outputs of the model derived by this kind of method fit the measured outputs well. It is suggested that this kind of data processing method is useful in identifying the yaw dynamics and processing the multi-experiment data for the system identification.
机译:通常需要多实验数据识别模型直升机的偏航动态。为了加强动力学的信息并降低噪声的效果,研究了使用加权标准的新种类最小二乘法以估计模型参数。为了计算加权标准的因素,培训了神经的Perceptron以自动确定因素。通过这种方法导出的模型的模拟输出适合测量的输出。建议这种数据处理方法可用于识别偏航动力学并处理用于系统识别的多实验数据。

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