Requirements of the longitudinal control augmentation system are presented through studying the 25th China Civil Aviation Regulations and C* flight quality evaluation criterion; The C* control augmentation scheme commonly used in modern large airliners is adopted to design the control augmentation system due to the stability and handling problems for the flying wing aircraft; The particle swarm optimization algorithm is proposed due to the parameter-scheduling difficulties in the designed control augmentation system. Numerical simulation shows that the designed C* control augmentation scheme is feasible.


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    Titel :

    Research on Control Augmentation System for a Flying Wing Aircraft



    Erschienen in:

    Advanced Materials Research ; 1049-1050 ; 953-956


    Erscheinungsdatum :

    2014-10-10


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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