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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Spacecraft digital controller


    Additional title:

    SAE-NASA Aerospace Vehicle Flight Control Conference -- Proc


    Contributors:

    Conference:

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



    Publication date :

    1965


    Size :

    7 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    A Spacecraft Digital Controller

    Daubert, Henry C. | SAE Technical Papers | 1965


    A spacecraft digital controller.

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


    Design of a digital controller for spinning flexible spacecraft

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


    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