This paper is focused on the model identification of a Micro Air Vehicle (MAV) in straight steady flight condition. The identification is based on input-output data collected from flight tests using both frequency and time domain techniques. The vehicle is an in-house 40 cm wingspan airplane. Because of the complex coupled, multivariable and nonlinear dynamics of the aircraft, linear SISO structures for both the lateral and longitudinal models around a reference state were derived. The aim of the identification is to provide models that can be used in future development of control techniques for the MAV. © 2007 Jilin University.
CITATION STYLE
Niño, J., Mitrache, F., Cosyn, P., & De Keyser, R. (2007). Model Identification of a Micro Air Vehicle. Journal of Bionic Engineering, 4(4), 227–236. https://doi.org/10.1016/S1672-6529(07)60036-5
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