FIELD: aviation, astronautic science.
SUBSTANCE: in the telemetry control method the signals from each of the telemetry sensors output are compared to the signal level user defined threshold of the key elements. When exceeding the threshold values, the key signal is given to pulse duration generator, which starts up the defined pulse width signal. When the key signal and the signal with defined pulse width coincides, they form a common positional coincidence signal with onboard time signal and convert it into a digital signal, corresponding to the control command number. In the on-board radio system the outputs of telemetry sensors are additionally series-connected with the key elements, the AND circuits, the position code into the digital code converter and the digital code into the control command converter.
EFFECT: spacecraft control efficiency and reliability increase.
2 cl, 2 dwg
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Authors
Dates
2017-03-01—Published
2015-07-23—Filed