The paper presents the design and performance of the flight stabilisation system onboard computer developed in Łukasiewicz Research Network – Institute of Aviation. The presented unit is an electronic block performing automatic flight stabilisation of an aeroplane using trimmers. It was designed based on the launch platform PZL-130 Orlik aircraft requirements. The article contains the unit’s hardware and software design description, unit performance, tests results and conclusions with improvements possibilities.


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    Title :

    Hardware and Software Design of Onboard Computer Controlling the Flight Stabilisation System


    Additional title:

    Advs in Intelligent Syst., Computing



    Conference:

    Conference on Automation ; 2022 ; Warsaw, Poland May 25, 2022 - May 27, 2022



    Publication date :

    2022-04-16


    Size :

    7 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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