A generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics over its entire flight envelope was developed. Implicit in this simulation development are the data reviews and analyses which support the equations of motion and the calculation of forces and moments acting on the vehicle. The simulation, HYBRDS, is addressed to the broad requirements and is intended for use as a synthesis and analysis tool for the evaluation of competing HLA design concepts.


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    Title :

    Flight Dynamics Analysis and Simulation of Heavy Lift Airships. Volume 1: Executive Summary


    Contributors:
    R. F. Ringland (author) / M. B. Tischler (author) / H. R. Jex (author) / R. D. Emmen (author) / I. L. Ashkenas (author)

    Publication date :

    1982


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Flight dynamics analysis and simulation of heavy lift airships. Volume 1: Executive summary

    Ringland, R. F. / Tischler, M. B. / Jex, H. R. et al. | NTRS | 1982


    Flight dynamics analysis and simulation of heavy lift airships. Volume 5: Programmer's manual

    Ringland, R. F. / Tischler, M. B. / Jex, H. R. et al. | NTRS | 1982


    Flight dynamics analysis and simulation of heavy lift airships. Volume 2: Technical manual

    Ringland, R. F. / Tischler, M. B. / Jex, H. R. et al. | NTRS | 1982



    Flight Dynamics Analysis and Simulation of Heavy Lift Airships. Volume 5: Programmer's Manual

    R. F. Ringland / M. B. Tischler / H. R. Jex et al. | NTIS | 1982