Guidance System Performance analysis; consideration of methodology of system performance analysis which forms principles and techniques of direct applicability in assessing guidance system performance and requirements; methodology is directly applicable to guidance system dependent upon particular mission considerations; concern is with mathematical framework; particular application is considered in terms of error model and analysis of Inertial Measurement Unit which is of direct usefulness in guidance and navigation system performance analyses.


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    Title :

    Guidance, flight mechanics and trajectory optimization -- 17


    Additional title:

    NASA CR


    Contributors:
    Grier, D.R. (author)

    Published in:

    Publication date :

    1968


    Size :

    215 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Guidance, flight mechanics and trajectory optimization -- 16

    Robertson, R.L. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 5

    Townsend, G.E. / Grier, D.R. / Palmer, R.R. et al. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 11

    Townsend, G.E. / Grier, D.R. / Blackford, A.L. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 15

    Abbott, A.S. / Blackford, A.L. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 6

    Allione, M.S. / Blackford, A.L. / Mendez, J.C. et al. | Engineering Index Backfile | 1968