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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    Title :

    Internal altitude technique for hypersonic glide vehicle guidance


    Additional title:

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


    Contributors:

    Conference:

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



    Publication date :

    1961


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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