Title: On the Identification of a Highly Augmented Airplane
Abstract: The results of applying linear least squares and maximum likelihood estimation procedures to flight data from the AFTI/F-16 airplane are presented. Data from two flight control system modes are analyzed. It is shown that though a simple aerodynamic model structure Is adequate for the simple mode, a more complicated model is necessary to adequately describe the highly augmented mode. The effect of augmentation of roll control is shown to be visible in the control parameters.
Publication Year: 1985
Publication Date: 1985-07-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 1
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