Designing Electric Propulsion Systems for UAVs

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Designing Electric Propulsion Systems for UAVs

Designing Electric Propulsion Systems for UAVs

Mohamed, Mohamed Kara / Patra, Sourav / Lanzon, Alexander

Due to the advantages of electric motors and electric batteries, the electric propulsion systems are widely used in UAVs. The UAV's performance and endurance, the payload capacity and the flight time of the vehicle are affected highly by the structure and design of the electric propulsion system. In this paper, a new systematic design methodology for electric propulsion system (propeller, electric motor and battery pack) is proposed based on the design specifications given in terms of the required thrust, permissible propulsion system's weight and required flight time.

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Title :

Designing Electric Propulsion Systems for UAVs

Contributors:

Mohamed, Mohamed Kara (author) / Patra, Sourav (author) / Lanzon, Alexander (author)

Published in:

TAROS, Towards Autonomous Robotic Systems. Annual Conference, 12 ; 388-389

Lecture Notes in Computer Science ; 6856

Publication date :

2011

Size :

2 Seiten

ISBN :

978-3-642-23231-2 , 978-3-642-23232-9

ISSN :

DOI :

https://doi.org/10.1007/978-3-642-23232-9_41

Type of media :

Conference paper

Type of material :

Print

Language :

English

Keywords :

elektromotorischer Antrieb , Systemdesign , elektrischer Motor , Propeller , elektrische Batterie , Werkzeugkonstruktion , Ausrüstungsentwurf , Maschinendesign , Propulsionssystem , unbemanntes Luftfahrzeug , Nutzlast , galvanische Batterie

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