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An atc response processing method based on an integrated avionics platform

A processing method and integrated avionics technology, applied in the direction of reflection/re-radiation of radio waves, radio wave measurement systems, instruments, etc., can solve the problems such as the inability to meet the response delay requirements of Mode S transponders, and achieve guaranteed delay. desired effect

Active Publication Date: 2020-06-23
四川九洲空管科技有限责任公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The difference between the ATC response equipment under the integrated avionics platform and the ATC response equipment under the discrete avionics platform is that the output of the general transceiver module to the signal processing FPGA is an intermediate frequency signal, and the FPGA needs to perform intermediate frequency signal processing (mixing, Filtering and threshold judgment), it takes 0.7us to output ASK pulse from intermediate frequency signal demodulation, so after applying the processing method on the existing discrete ATC answering equipment to the ATC answering equipment under the integrated avionics platform, calculate The total response delay is 4.1us, which cannot meet the requirements of the S-mode transponder for the response delay of the conventional mode (the index requirement of the response delay of the conventional mode is 3±0.5us)

Method used

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  • An atc response processing method based on an integrated avionics platform
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  • An atc response processing method based on an integrated avionics platform

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Embodiment Construction

[0013] An ATC response processing method based on an integrated avionics platform, the processing sequence is as follows figure 2 As shown, the processing flow is as follows image 3 shown.

[0014] The present invention designs and outputs two channels of TTL signals for the input of intermediate frequency signals. The first channel obtains the ask signal through frequency mixing and filtering, which takes 0.7us, and the second channel obtains the ask_pre signal through envelope detection, which takes 0.2us. One way is used for standard pulse decoding (including normal mode decoding and pre-decoding), and the second way is used to judge whether there is a P4 pulse.

[0015] It takes 1.1us for the response code pulse to reach the input port of the power amplifier after being up-converted from the output of the FPGA. It takes 0.5us for the power amplifier to fully start from the switch on. Pulse encoding needs to advance the power amplifier switch 0.6us.

[0016] In order n...

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Abstract

The invention discloses an ATC response processing method based on a comprehensive avionics platform. An ask signal is obtained by intermediate-frequency signal input through respective frequency mixing and filtering, and an ask_pre signal is obtained through envelope detection; and the ask signal is used for standard pulse decoding including conventional decoding and pre-decoding. According to the method, the response signal can be output in advance through pre-decoding processing, then a power amplifier switch and a transceiver switching switch are turned on in advance in matching a timing requirement of a transmission path, and the response signal is turned off if it is detected, at a P4 judgment position, that a P4 pulse exists or a conventional-decoding flag is invalid. Compared withexisting ATC response processing methods, the ATC response processing method under the comprehensive avionics platform provided by the invention considers each processing process and asking signal input-response signal output of an antenna port, calculates total response delay time as 3.4 us, and meets a delay time requirement of conventional-mode response of a response machine of the comprehensive avionics platform under an S mode.

Description

technical field [0001] The invention relates to an ATC response processing method based on an integrated avionics platform. Background technique [0002] The ATC response function under the integrated avionics platform is composed of antenna interface unit, general transceiver module, general signal processing module, integrated display and control terminal and other parts. The ATC response processing program resides in the FPGA of the general signal processing module, and is responsible for completing The signal is transferred to the baseband signal, the inquiry signal is decoded, the response signal is encoded, and the general transceiver module and the antenna interface unit are controlled to send the response signal. [0003] The existing ATC response processing method is suitable for the secondary radar response equipment in the discrete avionics platform. Under the integrated avionics platform, the output of the general transceiver module to the signal processing FPGA ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S13/76
CPCG01S13/765
Inventor 蒋鑫王华军邹亮陈思
Owner 四川九洲空管科技有限责任公司