The EU research Project Power Optimised Aircraft (POA) investigates the approach to replace primary hydraulic supply by extended electric power systems towards a More or All Electric Aircraft. This contribution presents an electrically powered actuation system for nose landing gears using an EHA (electrohydrostatic actuator) approach. One motor pump unit supplies door and gear actuation as well as the steering system. Different control strategies for the individual actuators are introduced. The effects of different control strategies are shown by simulation results.


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    Title :

    Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"


    Contributors:

    Publication date :

    2004



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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