Aircrafts are desired to be more energy efficient and safer due to the increasing demand for air transportations. However, generally speaking, nowadays commercial airplanes tend to loss stability under wind disturbances, especially during landing. On the other hand, electric airplanes (EAs) are believed to satisfy the two demands because electric motors are used for the propulsion. Especially, as the actuators, electric motors can improve the control performances of EAs compared with internal combustion engines (ICEs). In this paper, by utilizing electric motors' advantages, lift control method using propeller slipstream is proposed for safe landing, which might be a key technology to innovate the design of EAs. Moreover, simulations and experiments are conducted to verify the effectiveness of the proposed method.


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    Titel :

    Lift control of electric airplanes by using propeller slipstream for safe landing


    Beteiligte:


    Erscheinungsdatum :

    01.03.2015


    Format / Umfang :

    1181941 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Propeller Slipstream Development

    Roosenboom, E. / Heider, A. / Schroder, A. et al. | British Library Conference Proceedings | 2007


    Propeller Slipstream Development

    Roosenboom, Eric / Heider, André / Schröder, Andreas | AIAA | 2007




    Lift on wing in propeller slipstream as related to low-speed flight

    Rethorst, S. | Engineering Index Backfile | 1956