Small strapdown inertial system employing dry tuned rotary suspension gyroscopes for application to aircraft and ship navigation, high-accuracy space attitude reference and booster guidance. Two gyros provide for 3 axis sensing, leaving the 4th axis available from the pair of 2 axis instruments redundant.


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    Title :

    Strapdown guidance system developed


    Published in:

    Publication date :

    1972


    Size :

    1 Seite


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Strapdown guidance component research

    Hayes, R. J. | NTRS | 1968


    Strapdown Guidance Error Analysis

    Mortensen, R.E. | IEEE | 1974


    Strapdown Laser-Seeker Guidance Simulation

    R. E. Gallagher / R. D. Ehrich | NTIS | 1971


    Development tools for a strapdown guidance system

    DAWSON, W. / PARKE, IV, N. | AIAA | 1968


    Tactical guidance requirements for strapdown inertial

    Mueller, C.E. / Phelps, R.K. / Scheidenhelm, R. | Tema Archive | 1977