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System identification uncertainty quantification using orthogonal excitations the Semi-span SuperSonic Transport (S~4T) model

机译:使用正交激励和半跨超音速输运(S〜4T)模型进行系统识别和不确定性量化

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Orthogonal harmonic multisine excitations were utilized in a wind tunnel test and in simulation, of the SemiSpan Supersonic Transport model to assess aeroservoelastic characteristics. Fundamental issues associated with analyzing sinusoidal signals were examined, including spectral leakage, excitation truncation, and uncertainties on frequency response functions and mean-square coherence. Simulation allowed for evaluation of these issues relative to a truth model, while wind tunnel data Introduced real-world implementation issues.
机译:在SemiSpan超音速输运模型的风洞测试和模拟中使用正交谐波多正弦激励来评估航空弹性特性。研究了与分析正弦信号相关的基本问题,包括频谱泄漏,激励截断以及频率响应函数和均方相干性的不确定性。通过仿真可以评估与真模型相关的这些问题,而风洞数据则介绍了实际的实现问题。

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