Evaluation program was performed to apply digital techniques to stabilization and control problem; selection of mathematical techniques for system analysis and development of fabrication methods for hardware implementation; discrete state model of spacecraft reaction wheel and jet attitude control system was developed and computer simulations were performed; electronic control unit was constructed with semiconductor integrated microelectronics, and tested on air bearing simulator; mathematical model of system is presented and experimental performance compared with computer simulation.


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    Titel :

    Spacecraft digital controller


    Weitere Titelangaben:

    SAE-NASA Aerospace Vehicle Flight Control Conference -- Proc


    Beteiligte:

    Kongress:

    SAE-NASA -- Proceedings of the Aerospace Vehicle Flight Control Conference ; 1965 Control



    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A spacecraft digital controller.

    Daubert, H. C., Jr. | NTRS | 1965


    A Spacecraft Digital Controller

    Daubert, Henry C. | SAE Technical Papers | 1965


    Design of a Digital Controller for Spinning Flexible Spacecraft

    B. C. KUO / S. M. SELTZER / G. SlNGH AND R. A. YACKEL | AIAA | 1974


    Design of a digital controller for spinning flexible spacecraft

    KUO, B. / SINGH, G. / YACKEL, R. et al. | AIAA | 1973


    Design of a digital controller for spinning flexible spacecraft

    Kuo, B. C. / Seltzer, S. B. / Singh, G. et al. | NTRS | 1974