Satellite-borne dual-mode transmitter

A transmitter and spaceborne technology, applied in radio transmission systems, advanced technologies, electrical components, etc., can solve the problems of reducing satellite carrying capacity and operation capacity, limiting the overall design of satellites, increasing satellite costs, etc., to reduce the circuit scale. , The effect of reducing cost and weight, and low power consumption

Inactive Publication Date: 2019-10-11
SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The existing technology has the following defects: the separate design of the telemetry transmitter and the digital transmission transmitter has high cost, high power consumption, and heavy weight, which reduces the carrying capacity and operating capacity of the satellite in disguise, increases the cost of the satellite, and limits the overall capacity of the satellite. design

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  • Satellite-borne dual-mode transmitter
  • Satellite-borne dual-mode transmitter
  • Satellite-borne dual-mode transmitter

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Embodiment Construction

[0026] A spaceborne dual-mode transmitter proposed by the present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments. Advantages and features of the present invention will be apparent from the following description and claims.

[0027] see figure 1 , the present embodiment provides a space-borne dual-mode transmitter, including: a power supply controller, a constant temperature crystal oscillator, a temperature-compensated crystal oscillator, a frequency multiplier, an amplifier, a telemetry modulator, a digital transmission modulator, and a space-borne dual-mode transmitter. The working mode of the transmitter includes the working mode of the digital transmission transmitter and the working mode of the telemetry transmitter;

[0028] The output end of the constant temperature crystal oscillator and the output end of the temperature compensated crystal oscillator are both electrically connected to the inp...

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Abstract

The invention discloses a satellite-borne dual-mode transmitter which comprises a power supply controller, a constant temperature crystal oscillator, a temperature compensation crystal oscillator, a frequency multiplier, an amplifier, a telemetry modulator and a data transmission modulator. The satellite-borne transmitter can work in a telemetry transmitter mode and a data transmission transmittermode, the power supply controller controls power supply of all circuits in the transmitter according to a control instruction, and when the satellite-borne transmitter needs to work in the telemetrytransmitter mode, the power supply controller supplies power to the temperature compensated crystal oscillator, the frequency multiplier, the telemetry modulator and the amplifier; when the system needs to work in a data transmission transmitter mode, power is supplied to the constant temperature crystal oscillator, the frequency multiplier, the data transmission modulator and the amplifier; and when the transmitter does not work, all circuits are not powered. The invention has the technical characteristics of simple design, low cost, easy integration, low power consumption, light weight and strong universality.

Description

technical field [0001] The invention belongs to the field of space-borne measurement and control digital transmission transmitters, in particular to a space-borne dual-mode transmitter. Background technique [0002] At present, in my country's satellite measurement and control digital transmission subsystem, the transmitter is generally required to output telemetry and digital transmission signals to the ground station. It's not any different than the original way of working. [0003] The existing technology has the following defects: the separate design of the telemetry transmitter and the digital transmission transmitter has high cost, high power consumption, and heavy weight, which reduces the carrying capacity and operating capacity of the satellite in disguise, increases the cost of the satellite, and limits the overall capacity of the satellite. design. Contents of the invention [0004] The technical purpose of the present invention is to provide a spaceborne dual-...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04B7/185H04B1/04
CPCH04B1/04H04B7/1851Y02D30/70
Inventor 王文伟刘婧查晓晨
Owner SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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