An attitude control system is described in which angular rate signals are generated by rate gyros mounted closely adjacent to gimbaled engines at the rear of a vehicle. Error signals representative of a commanded change in vehicle angle or attitude are obtained from a precision inertial platform located in the nose region of the vehicle. The rate gyro derived signals dominate at high frequencies where dynamic effects become significant, and platform signals dominate at low frequencies where precision signals are required for a steady vehicle attitude. The blended signals are applied in a conventional manner to control the gimbaling of vehicle engines about control axes.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Attitude control system


    Beteiligte:
    Vonpragenau, G. L. (Autor:in) / Rupp, C. C. (Autor:in)

    Erscheinungsdatum :

    05.10.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    ATTITUDE CONTROL SYSTEM, ATTITUDE CONTROL METHOD, AND ATTITUDE CONTROL PROGRAM

    TAMAKOSHI HIROSHI | Europäisches Patentamt | 2023

    Freier Zugriff

    Attitude control system

    CARLSON RUSSELL / BARR DUSTIN / YAN ALLEN | Europäisches Patentamt | 2020

    Freier Zugriff

    Attitude Control System

    KIMURA SHUUJI | Europäisches Patentamt | 2018

    Freier Zugriff

    Attitude control system

    KIMURA SHUUJI | Europäisches Patentamt | 2020

    Freier Zugriff

    Artificial satellite, attitude control system, and attitude control method

    KITAMURA KENJI / SHIMA TAKEYA / YAMADA KATSUHIKO | Europäisches Patentamt | 2021

    Freier Zugriff