NASA NTRS · 19740054734
Computer experiments on periodic systems identification using rotor blade transient flapping-torsion responses at high advance ratio
Abstract
Computer experiments are described which used transient responses in flap-bending and torsion of a rotor blade at high advance ratio. It was found that a simple system identification method applying a linear sequential estimator also called equation of motion estimator, is suitable for this periodic system and can be used directly, if only the acceleration data are noise-polluted. In the case where noise is also present in the state-variable data, the direct application of the estimator gave poor results. However after prefiltering the data with a digital Graham filter having a cutoff frequency above the natural blade torsion frequency, the linear sequential estimator successfully recovered the parameters of the periodic coefficient analytical model.
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Hohenemser, K. H., Prelewicz, D. A.. 1974-01-01. Computer experiments on periodic systems identification using rotor blade transient flapping-torsion responses at high advance ratio. https://ntrs.nasa.gov/citations/19740054734
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