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

Citation Link: https://doi.org/10.15480/882.3470
Publikationstyp
Journal Article
Date Issued
2019-11-25
Sprache
English
Author(s)
Sedlmair, Nicolas  
Theis, Julian  orcid-logo
Thielecke, Frank  
Institut
Flugzeug-Systemtechnik M-7  
TORE-DOI
10.15480/882.3470
TORE-URI
http://hdl.handle.net/11420/4365
Journal
IFAC-PapersOnLine  
Volume
52
Issue
12
Start Page
316
End Page
321
Citation
IFAC-PapersOnLine 12 (52): 316-321 (2019)
Contribution to Conference
21st IFAC Symposium on Automatic Control in Aerospace ACA 2019  
Publisher DOI
10.1016/j.ifacol.2019.11.262
Scopus ID
2-s2.0-85077399712
Publisher
Elsevier
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
Publication version
publishedVersion
Lizenz
https://creativecommons.org/licenses/by-nc-nd/4.0/
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