Method for providing stable, inertially derived altitude indication is described; this method utilizes compensation technique based on inertial acceleration and velocity measurements and using stored density altitude relationships; application to guidance of hypersonic glide vehicles and to use in conjunction with Schuler loops of such vehicles is described, and results of REAC study are presented.


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    Titel :

    Internal altitude technique for hypersonic glide vehicle guidance


    Weitere Titelangaben:

    IRE -- East Coast Conference Aerospace Navigational Electronics -- Tech Paper


    Beteiligte:
    Gordon, R.L. (Autor:in)

    Kongress:

    IRE East Coast Conference on Aerospace and Navigational Electronics ; 1961 Control



    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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