Abstract
The problem of rotorcraft system identification is considered and a novel, two step technique is proposed, which combines the advantages of time domain and frequency domain methods. In the first step, the identification of a black-box model using a subspace model identification method is carried out, using a technique which can deal with data generated under feedback; subsequently, in the second step, a-priori information on the model structure is enforced in the identified model using an H ∞ model matching method. A simulation study is used to illustrate the proposed approach.
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Bergamasco, M., Lovera, M. (2013). Rotorcraft System Identification: An Integrated Time-Frequency Domain Approach. In: Chu, Q., Mulder, B., Choukroun, D., van Kampen, EJ., de Visser, C., Looye, G. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38253-6_11
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DOI: https://doi.org/10.1007/978-3-642-38253-6_11
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