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Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data

机译:联合翼SensorCraft气弹风洞数据的实时频率响应估计

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A new method is presented for estimating frequency responses and their uncertainties from wind-tunnel data in real time. The method uses orthogonal phase-optimized multi-sine excitation inputs and a recursive Fourier transform with a least-squares estimator. The method was first demonstrated with an F-16 nonlinear flight simulation and results showed that accurate frequency responses of the short period mode were obtained within 10 seconds. The method was then applied to wind-tunnel data from a previous aeroelastic test of the Joined-Wing SensorCraft. Frequency responses describing bending strains from simultaneous control surface excitations were estimated in a time-efficient manner.
机译:提出了一种从风洞数据实时估计频率响应及其不确定性的新方法。该方法使用正交相位优化的多正弦激励输入和带有最小二乘估计量的递归傅里叶变换。该方法首先通过F-16非线性飞行仿真进行了验证,结果表明,在10秒内可获得短周期模式的准确频率响应。然后将该方法应用于来自先前对联翼SensorCraft进行的空气弹性测试的风洞数据。以省时的方式估算了描述同时发生的控制面激励引起的弯曲应变的频率响应。

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