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  4. Robust autopilot design for crosswind landing
 
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Robust autopilot design for crosswind landing

Citation Link: https://doi.org/10.15480/882.3500
Publikationstyp
Journal Article
Date Issued
2017-10-18
Sprache
English
Author(s)
Theis, Julian  orcid-logo
Ossmann, Daniel  
Pfifer, Harald  
Institut
Flugzeug-Systemtechnik M-7  
TORE-DOI
10.15480/882.3500
TORE-URI
http://hdl.handle.net/11420/3806
Journal
IFAC-PapersOnLine  
Volume
50
Issue
1
Start Page
3977
End Page
3982
Citation
IFAC-PapersOnLine 1 (50): 3977-3982 (2017)
Contribution to Conference
20th IFAC World Congress 2017  
Publisher DOI
10.1016/j.ifacol.2017.08.770
Scopus ID
2-s2.0-85031810537
Publisher
Elsevier
A comprehensive autolanding design for the representative model of a twin-engined commercial aircraft is presented in this paper. A cascaded structure is selected to facilitate the design task and to minimize control law switching. Classical loopshaping and robust control techniques are used to design the individual control loops. The emphasis is on design parameters with a clear relation to design objectives, resulting in an intuitive tuning procedure. The control system's ability to safely land the aircraft despite strong crosswind in a variety of possible scenarios is demonstrated in an industry-grade verification campaign. Monte Carlo simulations are used to assess the risk of unsafe landing conditions and provide insight into the performance characteristics and limitations of the proposed control system.
Subjects
Flight control
Robust control applications
DDC Class
600: Technik
620: Ingenieurwissenschaften
Publication version
publishedVersion
Lizenz
https://creativecommons.org/licenses/by-nc-nd/4.0/
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