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| Date: | 2020-03-25 |
| Type of work: | Project |
| Advisor / Examiner: | Dieter Scholz |
| Published by: | Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences |
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Digital Library - Projects & Theses - Prof. Dr. Scholz ---
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AERO_POS_DLRK2025_Flightradar24_for_Aircraft_Performance_2025-09-23.pdf
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| Persistent Identifier: | https://doi.org/10.48441/4427.2892 |
| PERSISTENT IDENTIFIER: | |
| URN: | https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2020-03-25.02 (to reach this page) |
| DOI: | https://doi.org/10.15488/20721 |
| ARK: | https://n2t.net/ark:/13960/s2s9370681z |
| Associated research data: | https://doi.org/10.7910/DVN/D2DCBF (Data) |
| URLs registered with URN: | Show all links associated with this text! |
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| Keywords, German (GND): | Luftfahrt, Luftfahrzeug, Flugbetrieb, Mode-S-Radar |
| Keywords, English (LCSH): | Aeronautics, Airplanes, Flight, Electronic surveillance |
| Keywords, free: | Radar, Flugleistung, Flugmechanik, Flugzeug, Surveillance, Überwachung, Rundfunk, Radar, Air Traffic Control, ATC, Flightradar24, ADS-B, Mode S, aircraft performance, flight tracking services, Comm-B messages, python |
| DDC: | 629.13, 629.133340423, 629.135, 629.1366 |
| RVK: | ZO 7600 |
© This work is protected by copyright
The work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License
CC BY-NC-SA
https://creativecommons.org/licenses/by-nc-sa/4.0
Any further request may be directed to:
Prof. Dr.-Ing. Dieter Scholz, MSME
E-Mail see: http://www.ProfScholz.de
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Quote this text:
| ISO 690: JANSEN, Tim Maximilian, 2020. Flightradar24, ADS-B and Mode S Data for Aircraft Performance Analysis. Project. Hamburg University of Applied Sciences, Aircraft Design and Systems Group (AERO). Available from: https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2020-03-25.02 [viewed YYYY-MM-DD]. |
Major results / graphical abstract:
Rate of Climb (ROC) during step climbs. The horizontal red line shows the median while the blue box indicates the first and third quartile. Black whiskers are used to show the range of values that are not considered outliers. The red pluses mark outliers, i. e. their value is lower or greater than 2.7 σ of the sample data.
Initial Cruise Altitude (ICA) versus Great Circle Distance (GCD) of selected Airbus wide-body aircraft.
| dGC | Great Circle Distance (GCD) between origin and destination airport |
| hic | Initial Cruise Altitude (ICA) |
Prof. Dr. Scholz
Aircraft Design and Systems Group (AERO)
Aeronautical Engineering
Department of Automotive and Aeronautical Engineering
Faculty of Engineering and Computer Science
Hamburg University of Applied Sciences