Automatic three-point landing of a UAV with H∞-control in D-implementation

A multivariable flight control law for automatic landing of an unmanned aircraft with tailwheel gear configuration is developed in this paper. The control law is obtained using H∞-synthesis and implemented in a differential form to facilitate bumpless transfer, i.e. correct initialization when switching control laws, and anti-windup compensation. The controller is evaluated using a validated high-fidelity model of the aircraft and Monte-Carlo simulations.

Subjects

Flight control

Multivariable control systems

Robust control applications

DDC Class

600: Technik

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publishedVersion

Lizenz

https://creativecommons.org/licenses/by-nc-nd/4.0/

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1-s2.0-S2405896319312133-main.pdf

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815.78 KB

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Adobe PDF

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Automatic three-point landing of a UAV with H∞-control in D-implementation