Significant improvements in performance can be obtained if automatic flight control system is given task of improving handling qualities of basic aircraft and augmenting damping of flexible airframe; summary of data on passenger comfort obtained from motion simulators, routine airline operations, and military flight test data; passenger-comfort boundary that covers frequency range of .2-100 cps is defined; criteria for evaluating alleviation of structural fatigue are determined; recommendations made.


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    Titel :

    Requirements for flight control system of supersonic transport


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Notess, C.B. (Autor:in) / Gregory, P.C. (Autor:in)

    Kongress:

    SAE Meeting ; 1963 Control equipment



    Erscheinungsdatum :

    1963


    Format / Umfang :

    25 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Requirements for the Flight Control System of a Supersonic Transport*

    Notess, Charles B. / Gregory, Philip C. | SAE Technical Papers | 1963


    Effects of supersonic transport flight characteristics on performance requirements

    Tymczyszyn, J.J. / Spiess, P.C. | Engineering Index Backfile | 1963


    Flight Control System Design for Supersonic Transport

    Ostgaard, M. A. | SAE Technical Papers | 1962


    Supersonic transport propulsion requirements

    Nichols, M.R. | Engineering Index Backfile | 1961


    THE EFFECTS OF SUPERSONIC TRANSPORT FLIGHT CHARACTERISTICS ON PERFORMANCE REQUIREMENTS

    Tymczyszyn, Joseph J. / Spiess, Paul C. | SAE Technical Papers | 1963