Satellite-borne X-frequency band data transmission out-of-band rejection device and satellite-borne X-frequency band data transmission out-of-band rejection method

Abstract

The invention relates to a satellite-borne X-frequency band data transmission out-of-band rejection device and a satellite-borne X-frequency band data transmission out-of-band rejection method. The satellite-borne X-frequency band data transmission out-of-band rejection device comprises a level converter, a base band filter, a BPSK (Binary Phase Shift Keying) modulator, an X-frequency band carrier signal generator, an amplifier and an isolator. By converting the level of inputted low-frequency base band data, the satellite-borne X-frequency band data transmission out-of-band rejection device outputs a bipolar level signal, the data and an X-frequency band carrier signal are sent into the BPSK modulator to be modulated together after base band shaping filtration is performed by the base band filter, and therefore the data are modulated into the X frequency band. The output frequency spectrum of the BPSK modulator can meet the out-of-band rejection requirement, and the modulated data sequentially pass through the amplifier and the isolator and are then outputted to a solid-state amplifier or an antenna. The satellite-borne X-frequency band data transmission out-of-band rejection device can meet the out-of-band rejection requirement without affecting data transmission modulation characteristics and the data transmission communication error rate and with the same size, power consumption and weight, and is particularly applicable to projects with high working frequency and low data transmission bit rates, such as lunar exploration projects.

Description

technical field [0001] The invention relates to an out-of-band suppression technology for satellite-borne digital transmission, in particular to an out-of-band suppression device and method for satellite-borne X-band digital transmission. Background technique [0002] In order to better promote international cooperation and avoid spectrum interference, the Space Data Advisory Committee (CCSDS) has divided the frequency bands of satellite monitoring and control. With the increasing frequency of international space exploration activities, the X-band is used more and more, and the spectrum interferes with each other. It is becoming more and more serious, so there are corresponding requirements for the width of the satellite downlink spectrum. According to the 21-2R2 (SFCG21-2R2) template suggested by the Space Spectrum Coordination Group, such as figure 1 As shown, and the requirements of the measurement and control digital transmission subsystem, the allowable spectrum frame ...

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Problems solved by technology

The former method uses an X-band cavity filter. According to the requirements, its bandwidth should be 2×R MHz, and the suppression at the center frequency ±R×1.4MHz must be greater than 30dB. Due to the narrow bandwidth, the rectangularity factor and quality factor are extremely demanding High, currently the cavity filter cannot meet the requirements in engineering

The latter method takes advantage of the high square coefficient of the SAW filter to filter the output spectrum of the digital transmission modulation at the intermediate frequency to achieve the required out-of-band suppression and mix the modulation signal to the X frequency band. This method avoids the X frequency cavity The design bottleneck of the body filter, although it can realize the out-of-band suppression of digital transmission, but it uses a lot of components, so it needs to use the cavity filter to suppress the local oscillator and image frequency in the X frequency band, and also needs to perform gain compensation, which has complex circuit and volume Disadvantages of large size, high power consumption and heavy debugging workload

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