Function of any guidance system selecged for Europa rocket is to generate steering demands so that trajectory flown results in minimum consumption of fuel and that required orbital velocity and height at injection are achieved with maximum accuracy; responsibilities for design and manufacture of system are listed; description of system, sources and magnitudes of error in radio guidance system and method of operation of inertial guidance system. Presented before -- All-Day Symposium on ELDO, held by Astronautics and Guided Flight Sec of Roy Aeronautical Soc on Feb 7 1968.


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    Titel :

    Problems of guidance, in particular -- Inertial guidance


    Weitere Titelangaben:

    Aeronautical J


    Beteiligte:
    Mattin, R.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Inertial guidance

    Emerald Group Publishing | 1964


    Inertial guidance

    Stark Draper, Charles / Wrigley, Walter / Hovorka, John | TIBKAT | 1960


    Inertial guidance

    Wrigley, W. / Woodbury, R.G. / Hovorka, J. | Engineering Index Backfile | 1957


    ICBM inertial guidance

    Goetz, E.A. | Engineering Index Backfile | 1958


    Inertial guidance engineering

    Fernandez, Manuel / Macomber, George R. | TIBKAT | 1962