Please use this identifier to cite or link to this item: https://doi.org/10.15480/882.3470
Publisher DOI: 10.1016/j.ifacol.2019.11.262
Title: Automatic three-point landing of a UAV with H∞-control in D-implementation
Language: English
Authors: Sedlmair, Nicolas 
Theis, Julian  
Thielecke, Frank 
Keywords: Flight control;Multivariable control systems;Robust control applications
Issue Date: 25-Nov-2019
Publisher: Elsevier
Source: IFAC-PapersOnLine 12 (52): 316-321 (2019)
Journal: IFAC-PapersOnLine 
Abstract (english): 
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.
Conference: 21st IFAC Symposium on Automatic Control in Aerospace ACA 2019 
URI: http://hdl.handle.net/11420/4365
DOI: 10.15480/882.3470
ISSN: 2405-8963
Institute: Flugzeug-Systemtechnik M-7 
Document Type: Article
License: CC BY-NC-ND 4.0 (Attribution-NonCommercial-NoDerivatives) CC BY-NC-ND 4.0 (Attribution-NonCommercial-NoDerivatives)
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