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 subspacemodel identificationmethod is carried out, using a techniquewhich 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 Hinf model matchingmethod. A simulation study is used to illustrate the proposed approach.

Rotorcraft system identification: an integrated time-frequency domain approach

LOVERA, MARCO
2013-01-01

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 subspacemodel identificationmethod is carried out, using a techniquewhich 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 Hinf model matchingmethod. A simulation study is used to illustrate the proposed approach.
2013
2nd CEAS Specialist Conference on Guidance, Navigation & Control
AUT
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/825530
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