Position control by feedback linearization for a simplified helicopter model
- 20 January 2003
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- Vol. 1, 143-145
- https://doi.org/10.1109/cca.1999.806165
Abstract
In this paper we describe a method for angular pitch control with feedback linearization for a laboratory helicopter model. Linear angular control can only be applied in a small angle interval. Better control can be obtained by using a linearizing transformation. This transformation tends to be very complex. For the application in this paper it can be shown that a simplified transformation can be sufficient for achieving good control results.Keywords
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