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Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions

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

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Abstract

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°.

Item URL in elib:https://elib.dlr.de/201274/
Document Type:Article
Title:Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schwithal, JanaUNSPECIFIEDhttps://orcid.org/0000-0003-3554-0560UNSPECIFIED
Fezans, NicolasUNSPECIFIEDhttps://orcid.org/0000-0003-4351-3474UNSPECIFIED
Date:10 March 2023
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:60
DOI:10.2514/1.C037062
Page Range:pp. 1290-1301
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:1533-3868
Status:Published
Keywords:flight control, wake vortex encounter, Doppler lidar sensor
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Aircraft Technologies and Integration
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Institute of Flight Systems
Deposited By: Schwithal, Jana
Deposited On:25 Jan 2024 13:12
Last Modified:11 Nov 2024 13:30

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