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A Simple Approach to Quadrocopter Formation Flying Test Setup for Education and Development

Zitieren Sie bitte immer diese URN: urn:nbn:de:bvb:20-opus-114495
  • A simple test setup has been developed at Institute of Aerospace Information Technology, University of Würzburg, Germany to realize basic functionalities for formation flight of quadrocopters. The test environment is planned to be utilized for developing and validating the algorithms for formation flying capability in real environment as well as for education purpose. An already existing test bed for single quadrocopter was extended with necessary inter-communication and distributed control mechanism to test the algorithms for formation flightsA simple test setup has been developed at Institute of Aerospace Information Technology, University of Würzburg, Germany to realize basic functionalities for formation flight of quadrocopters. The test environment is planned to be utilized for developing and validating the algorithms for formation flying capability in real environment as well as for education purpose. An already existing test bed for single quadrocopter was extended with necessary inter-communication and distributed control mechanism to test the algorithms for formation flights in 2 degrees of freedom (roll / pitch). This study encompasses the domain of communication, control engineering and embedded systems programming. Bluetooth protocol has been used for inter-communication between two quadrocopters. A simple approach of PID control in combination with Kalman filter has been exploited. MATLAB Instrument Control Toolbox has been used for data display, plotting and analysis. Plots can be drawn in real-time and received information can also be stored in the form of files for later use and analysis. The test setup has been developed indigenously and at considerably low cost. Emphasis has been placed on simplicity to facilitate students learning process. Several lessons have been learnt during the course of development of this setup. Proposed setup is quite flexible that can be modified as per changing requirements.zeige mehrzeige weniger

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Metadaten
Autor(en): Qasim Ali, Sergio Montenegro
URN:urn:nbn:de:bvb:20-opus-114495
Dokumentart:Konferenzveröffentlichung
Institute der Universität:Fakultät für Mathematik und Informatik / Institut für Informatik
Sprache der Veröffentlichung:Englisch
Titel des übergeordneten Werkes / der Zeitschrift (Englisch):INTED2015 Proceedings
ISSN:2340-1079
Erscheinungsjahr:2015
Verlag:International Academy of Technology, Education and Development (IATED)
ISBN:978-84-606-5763-7
Erste Seite:2776
Letzte Seite:2784
Originalveröffentlichung / Quelle:INTED2015 Proceedings: 9th International Technology, Education and Development Conference Madrid, Spain. 2-4 March, 2015., S. 2776 - 2784, ISBN 978-84-606-5763-7.
Allgemeine fachliche Zuordnung (DDC-Klassifikation):0 Informatik, Informationswissenschaft, allgemeine Werke / 00 Informatik, Wissen, Systeme / 004 Datenverarbeitung; Informatik
Normierte Schlagworte (GND):Flugkörper; Quadrocopter
Freie Schlagwort(e):Design and Development; Formation Flight; Instrument Control Toolbox; Quadrocopter; Unmanned Aerial Vehicle
Fachklassifikation Informatik (CCS):B. Hardware
D. Software
J. Computer Applications
Datum der Freischaltung:18.06.2015
Lizenz (Deutsch):License LogoDeutsches Urheberrecht