FIELD: aviation.SUBSTANCE: method includes the construction of the inertial solar orientation of the space vehicle with a system of power gyroscopes, measurement of vectors and their kinetic moments, maintenance of this orientation with simultaneous unloading of gyroscopes. At the same time, in certain parts of the orbit, the operations of spinning the spacecraft, measuring and comparing with the maximum permissible level of the accumulator battery (AB) charge, monitoring the power balance of the spacecraft, unloading the power gyroscopes, charging the accumulator batteries from solar batteries are carried out in a certain combination with each other. These operations are linked to the processes of planned and unplanned Earth surface survey.EFFECT: increase of the spacecraft resource.6 dwg


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    Title :

    СПОСОБ УПРАВЛЕНИЯ КОСМИЧЕСКИМ АППАРАТОМ ДИСТАНЦИОННОГО ЗОНДИРОВАНИЯ ЗЕМЛИ


    Publication date :

    2017-03-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS