2. Application to civil aircraft piloting
In this main part of the article, we will now detail the implementation of modal control techniques to solve our problem of piloting a civil aircraft in the vertical plane during the approach phase.
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2.1.1 Non-linear modeling
For this study, a non-linear model of the plane's motion in the vertical plane is used. This motion is governed by a set of six differential equations
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Application to civil aircraft piloting
Bibliography
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(1) - BIANNIC (J.-M.) -
Commande robuste des systèmes à paramètres variables
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Thèse SUPAÉRO, Toulouse (Octobre 1996).
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(2) - BIANNIC (J.-M.), ROOS (C.), KNAUF (A.) -
Design and analysis of fighter aircraft flight...
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