– The purpose of this article is to evaluate performance of minimum energy controllers thoroughly on a tiltrotor aircraft.

    Approach

    – Minimum energy controllers are designed for tiltrotor aircraft models for helicopter and airplane modes. Performance of minimum energy controllers is evaluated with respect to several criteria.

    Findings

    – Minimum energy controllers can be used for tiltrotor aircraft flight control system design. These controllers show satisfactory performance when noise intensities and variance bounds vary.

    Practical implications

    – Minimum energy controllers can be implemented for tiltrotor aircraft flight control system design.

    Originality/value

    – In this paper, minimum energy controllers are applied for tiltrotor aircraft flight control system design and the performance of minimum energy controllers is evaluated deeply on a complex physical system (i.e. tiltrotor aircraft).


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    Title :

    Performance of minimum energy controllers on tiltrotor aircraft


    Contributors:


    Publication date :

    2014-08-26


    Size :

    14 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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