SATELLITE TRANSMITTER Russian patent published in 2018 - IPC H04B7/185 

FIELD: communication equipment.

SUBSTANCE: invention relates to communication techniques and can be used to relay information via satellite repeaters. In a satellite repeater comprising a switching unit, sequentially coupled a receiving subscriber antenna unit and a subscriber receiver unit, connected to the first inputs of the switching unit, the inter-satellite antenna receiving unit and the inter-satellite receiver unit connected in series, also connected to the first inputs of the switching unit, wherein the switching unit is connected to the inputs of the transmitter unit, the signaling separation unit is connected to the outputs of the receiver unit and the first inputs of the signaling unit, the sequentially connected navigation unit, the service message generation unit and the blocking signal generator, the outputs of the latter of them are connected to the second inputs of the switching unit, the third inputs of which are connected to the outputs of the service message generation unit, and the fourth inputs are connected to the outputs of the navigation unit, unlike the known ones, a solar sensor and an orientation unit, in the transmitting antenna unit, the subscriber antennas are configured for the radio range, the inter-satellite antennas are designed for the optical range, in the receiving antenna unit, the subscriber antennas are designed for the radio range, and the inter-satellite antennas are designed for the optical range, the outputs of the signaling signal separation unit via the series-connected bearing signal separation unit, the bearing signal analyzer unit and the first inputs of the modulator control unit are connected to the first inputs of the modulator unit and are connected to the second inputs of the service message generation unit via the second inputs of the modulator control unit, the outputs of the inter-satellite transmitter unit are connected to the inputs of the block of transmitting inter-satellite antennas through the second inputs of the modulator block, in the modulator control unit, the clock input is connected to the clock output of the signal conditioning unit, and the third input is connected to the output of the solar sensor, which is also connected to the first input of the orientation unit, the second inputs of which are connected to the outputs of the navigation unit, in the modulator control unit, the correction code selection unit, the control signal generating unit, the correction code generation unit, and the register unit are connected in series, the second inputs of the control signal generating unit are the first inputs of the modulator control unit, the inputs of the correction unit of the guidance correction code and the inputs of the register block are its second inputs, the second input of the register block is its clock input, the third input of the control signal generating unit is connected to the output of the signaling unit, and the output of the control signal generating unit is the output of the modulator control unit.

EFFECT: technical result consists in increasing the throughput of the inter-satellite path through the use of laser communications.

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