The automatic reentry flight dynamics simulator, a nonlinear, six-degree-of-freedom simulation, digital computer program, has been developed. The program includes a rotating, oblate earth model for accurate navigation calculations and contains adjustable gains on the aerodynamic stability and control parameters. This program uses a real-time simulation system and is designed to examine entries of vehicles which have constant mass properties whose attitudes are controlled by both aerodynamic surfaces and reaction control thrusters, and which have automatic guidance and control systems. The program has been used to study the space shuttle orbiter entry. This report includes descriptions of the equations of motion used, the control and guidance schemes that were implemented, the program flow and operation, and the hardware involved.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A Real-Time Digital Computer Program for the Simulation of Automatic Spacecraft Reentries


    Beteiligte:
    J. T. Kaylor (Autor:in) / L. F. Powell (Autor:in) / R. W. Powell (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    136 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    A real-time digital computer program for the simulation of automatic spacecraft reentries

    Kaylor, Jack T. / Rowell, Lawrence F. / Powell, Richard W. | TIBKAT | 1977


    Unnecessary Risks Created by Uncontrolled Rocket Reentries

    Byers, Michael | British Library Conference Proceedings | 2022


    Comparison of Reentry Breakup Measurements for Three Atmospheric Reentries

    Feistel, A.S. / Weaver, M.A. / Ailor, W.H. et al. | British Library Conference Proceedings | 2013