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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.
2.1 Model and specifications
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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Systèmes aéronautiques et spatiaux
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Application to civil aircraft piloting
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The Ultimate Scientific and Technical Reference