FIELD: astronautics.SUBSTANCE: invention relates to systems for stabilizing and controlling the orientation of spacecraft and can be applied for controlling the angular motion of a small spacecraft. Device is a combined control system consisting of a self-extracting gravity rod with an end load and a two-stage gyro with a torque sensor on the suspension axis performing the function of this load. To control the spacecraft on-course, the specified gyro is used as a gyrodyne, and for controlling the roll and pitch angles – as an electromechanical actuator (flywheel).EFFECT: technical result of the invention is expansion of the system functionality and the increase in the accuracy of the spacecraft orientation.1 cl, 3 dwg


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    Title :

    КОМБИНИРОВАННАЯ ГРАВИТАЦИОННАЯ СИСТЕМА ОРИЕНТАЦИИ МАЛОГО КОСМИЧЕСКОГО АППАРАТА


    Publication date :

    2017-10-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS