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Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions

Schwithal, Jana und Fezans, Nicolas (2023) Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions. Journal of Aircraft, 60 (4), Seiten 1290-1301. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C037062. ISSN 1533-3868.

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Kurzfassung

The paper complements previous works of the authors on lidar-based active wake impact alleviation control functions by investigating the lidar sensor requirements for such systems. This control system can increase the safety during wake vortex encounters by preventing a dangerous sudden (in particular rolling) motion, which often characterizes wake-vortex encounters. Such technology could provide an opportunity to relax the current wake-vortex-based separation minima and thus lead to a capacity gain for airports and in the terminal area. The performance of this system obviously strongly depends on the performance of the lidar sensor, however in a nontrivial way. The direct problem, i.e. determining the system performance obtained with a given sensor configuration, already requires setting up a fully coupled simulation environment. The inverse problem, i.e. determining the best suited set of sensor parameters, is approached in this work through parameter variations and sensitivity studies. Key performance parameters for assessing the overall system performance, and providing trends for sensor requirements are defined. As for most technical systems, the best configurations are characterized by a good tradeoff of the relevant parameters, in this case field of view, measurement range, spatial resolution, and measurement noise. The coupled simulations revealed that, contrary to the authors’ expectations, very good results were already obtained with small ranges of 60 m and lateral fields of view of +/- 16°.

elib-URL des Eintrags:https://elib.dlr.de/201274/
Dokumentart:Zeitschriftenbeitrag
Titel:Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Schwithal, JanaJana.Schwithal (at) dlr.dehttps://orcid.org/0000-0003-3554-0560NICHT SPEZIFIZIERT
Fezans, NicolasNicolas.Fezans (at) dlr.dehttps://orcid.org/0000-0003-4351-3474NICHT SPEZIFIZIERT
Datum:10 März 2023
Erschienen in:Journal of Aircraft
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:60
DOI:10.2514/1.C037062
Seitenbereich:Seiten 1290-1301
Verlag:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:1533-3868
Status:veröffentlicht
Stichwörter:flight control, wake vortex encounter, Doppler lidar sensor
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Flugzeugtechnologien und Integration
Standort: Braunschweig
Institute & Einrichtungen:Institut für Flugsystemtechnik > Flugdynamik und Simulation
Institut für Flugsystemtechnik
Hinterlegt von: Schwithal, Jana
Hinterlegt am:25 Jan 2024 13:12
Letzte Änderung:11 Nov 2024 13:30

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