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Autor(en):
M. Hanel, M. Haimerl, T. Bienert
Zusammenfassung:
This paper describes the flight control functionality for the Quadcruiser remotely piloted air vehicle (RPA). The Quadcruiser is a hybrid air vehicle featuring both an electrically powered lift system for a vertical takeoff, landing and hover capability and a combustion engine powered cruise flight capability with wing, empennage and conventional control surfaces. For transition between hover and cruise both the lift system and the cruise control system are active. The flight control functionality features stability augmentation and attitude control for hover, cruise and transition and flight guidance functionality for altitude, speed and direction control. The functionality has been implemented and flight-test-demonstrated on a fully electric subscale experimental vehicle, the QC11.
Veranstaltung:
Deutscher Luft- und Raumfahrtkongress 2018, Friedrichshafen
Verlag, Ort:
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2018
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 10 Seiten
URN:
urn:nbn:de:101:1-2018121411473061783224
DOI:
10.25967/480033
Stichworte zum Inhalt:
Flight Control , Electric VTOL UAV
Verfügbarkeit:
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Kommentar:
Zitierform:
Hanel, M.; Haimerl, M.; Bienert, T. (2018): Flight Control Laws for the Quadcruiser RPA. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.. (Text). https://doi.org/10.25967/480033. urn:nbn:de:101:1-2018121411473061783224.
Veröffentlicht am:
14.12.2018