A sounding rocket attitude control system is reported that uses rate integrated gyros operating in both closed loop and open loop modes at very low drift rates. In normal operation the gyros are zeroed on a nearby star and torqued to the proper location in the closed loop mode; rate output is electronically integrated to provide a position displacement signal. Once closed loop torquing is completed, the caging loop is opened and the gyro is operated as angular displacement sensor to provide limit cycle control while viewing the target.


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    Titel :

    STRAP 4 sounding rocket attitude control system


    Beteiligte:


    Erscheinungsdatum :

    01.01.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Stellar Tracking Rocket Attitude Positioning /STRAP/ System

    Greeb, M. E. / Shrewsberry, D. J. | NTRS | 1970


    Stellar Tracking Rocket Attitude Positioning (STRAP) System

    GREEB, M. / SHREWSBERRY, D. | AIAA | 1970


    Application of Adaptive Control - Sounding Rocket Attitude

    Leite Filho, W. C. / International Federation of Automatic Control / Beijing Institute of Control Engineering | British Library Conference Proceedings | 1997


    Gyroless solar pointing attitude control system for aerobee sounding rocket

    Hansen, Q.M. / Gabris, E.A. / Pearson, M.D. et al. | Engineering Index Backfile | 1967