Need for systems applied to commercial aircraft, drone and research vehicles, manned space craft, and recoverable missile boosters, is shown; automatic landing problems and limitations of exponential flare and path program systems; concept of 2-condition terminal flare controller, using altitude and altitude rate predictor; real time synthesis procedure provides direct design method for servo problems of terminal control type.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Automatic flare systems for aircraft, missiles, and space vehicles


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1958 Landing



    Publication date :

    1958


    Size :

    18 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :




    Automatic control of aircraft and missiles

    Blakelock, John H. | TIBKAT | 1991


    Automatic control of aircraft and missiles

    Blakelock, John H. | TIBKAT | 1965


    Ground support systems for missiles and space vehicles

    Brown, Kenneth ;Weiser, Peter | TIBKAT | 1961