Abstract
The practical problem of constructing a model, from which to design a helicopter vibration control system, is presented. This is done to provide a rather extreme example of the interaction between the modelling objective and the control design. This is done to reinforce the messages of earlier chapters dealing with modelling for control design and the need to concentrate on the ultimate model application in assessing the quality of model fit. The approach relies on the tight fitting of frequency response values across a region of interest using experimental data. This is demonstrated in the experiment design and in the data pre-filtering as was discussed in Chapter 3.
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© 2002 Springer-Verlag London
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Bitmead, R.R. (2002). Helicopter Vibration Control. In: Albertos, P., Sala, A. (eds) Iterative Identification and Control. Springer, London. https://doi.org/10.1007/978-1-4471-0205-2_10
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DOI: https://doi.org/10.1007/978-1-4471-0205-2_10
Publisher Name: Springer, London
Print ISBN: 978-1-4471-1098-9
Online ISBN: 978-1-4471-0205-2
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