In clause process of program support of a space vehicle antenna system during carrying out of a session of reception of the information of remote sounding the Earth is considered. The technique of synthesis of PWM-signal of-management is offered by the engine of a direct current of independent excitation which is based on definition of an auxiliary analog signal. The model of digital regulator is got in a vectorial form. Possibility of method to provide optimum on duration and amount of over-fluctuation transitional process is marked.
Keywords:
remote sensing of Earth, space vehicle, power watching drive, terminal management
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