Flight testing that is planned for October 2010 will provide an opportunity to evaluate rotorcraft trajectory optimization techniques. The flight test will involve a fully instrumented MD-902 helicopter, which will be flown over an array of microphones. In this work, the helicopter approach trajectory is optimized via a multiobjective genetic algorithm to improve community noise, passenger comfort, and pilot acceptance. Previously developed optimization strategies are modified to accommodate new helicopter data and to increase pilot acceptance. This paper describes the MD-902 trajectory optimization plus general optimization strategies and modifications that are needed to reduce the uncertainty in noise predictions. The constraints that are imposed by the flight test conditions and characteristics of the MD-902 helicopter limit the testing possibilities. However, the insights that will be gained through this research will prove highly valuable.


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    Titel :

    Design of Quiet Rotorcraft Approach Trajectories: Verification Phase


    Beteiligte:
    S. L. Padula (Autor:in)

    Erscheinungsdatum :

    2010


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design of Quiet Rotorcraft Approach Trajectories: Verification Phase

    Padula, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010



    Design of Quiet Rotorcraft Approach Trajectories

    Padula, Sharon L. / Burley, Casey L. / Boyd, D. Douglas, Jr. et al. | NTRS | 2009


    Design of Quiet Rotorcraft Approach Trajectories

    S. L. Padula / C. L. Burley / D. D. Boyd et al. | NTIS | 2009