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DESIGN CONSIDERATIONS AND TEST OF THE FLIGHT CONTROL ACTUATORS FOR A DEMONSTRATOR FOR AN UNMANNED FREIGHT TRANSPORTATION AIRCRAFT

Bierig, Andreas und Lorenz, Sven und Rahm, Malte und Gallun, Patrick (2018) DESIGN CONSIDERATIONS AND TEST OF THE FLIGHT CONTROL ACTUATORS FOR A DEMONSTRATOR FOR AN UNMANNED FREIGHT TRANSPORTATION AIRCRAFT. In: Recent Advances in Aerospace Actuation Systems and Components 2018 Conference Proceedings. Recent Advances in Aerospace Actuation Systems and Components 2018, 2018-05-30 - 2018-06-01, Toulouse, Frankreich.

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Kurzfassung

Unmanned Aircraft Systems (UAS) becoming increasingly attractive to airfreight transportation duties. The Automated Low Altitude Air Delivery (ALAADy) UAS is a Technology demonstrator for an innovative concept of delivering freight by means of a low cost solution. The demonstrator is based on an AutoGyro MTOFree gyroplane. The development of this demonstrator aircraft is aligned to upcoming innovative rules for certification of UAS for operation in civil airspace. Hereby, safety assessment is based on a mission centric approach, which focusses on the risks resulting from the operational scenario, to determine the necessary safety assurance level. The higher the risk of causing fatalities or significant damage to property in case of uncontrolled operation, the higher will be the rigor of safety assurance. The paper focusses on the design and test of the electromechanical actuation system for the ALAADy demonstrator. The paper starts with an overview about the project and the demonstrator aircraft including the Mission and most relevant objectives. Subsequently, the requirements on the actuation system as well as main design considerations are introduced. Further, a section is dedicated to the testing activities of the actuation system to demonstrate compliance with the requirements. Besides the test results, an automated test bench will be described, which was utilized to conduct most of the test procedures. The paper concludes with a summary and an outlook to the next steps in the ALAADy demonstrator project.

elib-URL des Eintrags:https://elib.dlr.de/120476/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:DESIGN CONSIDERATIONS AND TEST OF THE FLIGHT CONTROL ACTUATORS FOR A DEMONSTRATOR FOR AN UNMANNED FREIGHT TRANSPORTATION AIRCRAFT
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Bierig, AndreasAndreas.Bierig (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Lorenz, SvenSven.Lorenz (at) dlr.dehttps://orcid.org/0000-0002-2133-227XNICHT SPEZIFIZIERT
Rahm, MalteMalte.Rahm (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Gallun, PatrickPatrick.Gallun (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:31 Mai 2018
Erschienen in:Recent Advances in Aerospace Actuation Systems and Components 2018 Conference Proceedings
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Unmanned aircraft system, electromechanical actuators, flight termination system, automated actuator testing
Veranstaltungstitel:Recent Advances in Aerospace Actuation Systems and Components 2018
Veranstaltungsort:Toulouse, Frankreich
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:30 Mai 2018
Veranstaltungsende:1 Juni 2018
Veranstalter :INSA Toulouse
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Systeme und Kabine (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Flugsystemtechnik > Sichere Systeme und System Engineering
Institut für Flugsystemtechnik > Unbemannte Luftfahrzeuge
Hinterlegt von: Bierig, Andreas
Hinterlegt am:26 Jun 2018 09:46
Letzte Änderung:24 Apr 2024 20:24

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