This paper presents piloted flight test results of a sliding mode fault tolerant control scheme implemented on the Japan Aerospace Exploration Agency's MuPAL-$\alpha$ research aircraft. These results represent unique piloted validation tests of a sliding mode fault tolerant control allocation scheme on a full-scale aircraft operating in the presence of actuator faults. The control law used here does not require the presence of a fault detection and isolation unit and therefore in the event of faults/failures, the actuator effectiveness levels are unknown. In the absence of this information, a fixed control allocation mechanism has been used in order to retain nominal fault-free performance. The control scheme has been implemented on the lateral-directional motion and incorporated within the experimental fly-by-wire system. Piloted flight test results show that close to nominal tracking performance can be maintained despite the presence of unknown actuator faults as well as actuator uncertainties.


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    Title :

    Evaluation of a Sliding Mode Fault Tolerant Controller on the MuPAL-$\alpha$ Research Aircraft


    Contributors:
    Chen, L. (author) / Alwi, H. (author) / Edwards, C. (author) / Sato, M. (author)


    Publication date :

    2018-08-01


    Size :

    1657015 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English