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multifunctional airborne navigation equipment

A kind of navigation equipment and multi-functional technology, applied in the direction of instruments, measuring devices, electrical components, etc., can solve the problems of high aircraft flight safety risks, reduce flight safety risks, and not widely used by aircraft, so as to reduce safety risks and strengthen execution capabilities , The effect of reducing the cost of modification

Active Publication Date: 2022-03-11
四川荣川通用航空有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to overcome the disadvantages of the prior art airborne navigation equipment, which are not widely used on aircraft due to the high cost of refitting and incomplete functions, resulting in a relatively high risk of aircraft flight safety, and provide a multifunctional airborne navigation system. Equipment, through the navigation equipment, effectively strengthen the information interaction between the various modules on the aircraft, and integrate each module to reduce the modification cost, so that the airborne navigation equipment can be configured more widely, and data exchange can be carried out more effectively, thus effectively reduce flight safety risks

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0075] Such as Figure 1~4 As shown, the multifunctional airborne navigation equipment, the navigation equipment includes a signal processing unit, a service module, an ADS-B communication unit and an antenna, wherein,

[0076] The signal processing unit is used to process all relevant business data onboard, and encode the business data and send it to the ADS-B communication unit as a radio frequency signal; it is used to receive the radio frequency signal sent by the ADS-B communication unit, and analyze the ADS-B The message is sent to the service module after parsing; the signal processing unit includes peripheral hardware and interface circuit, ARM processor and FPGA hardware module, wherein,

[0077] The peripherals and the interface circuit are connected to the service module for information interaction with the service module;

[0078] The ARM processor is used to respond to the information of peripherals and interface circuits, and to comprehensively schedule the info...

Embodiment 2

[0095] Such as Figure 1~5 As shown, on the basis of Embodiment 1, in the FPGA hardware module, the input processing of the radio frequency signal includes the following steps:

[0096] S1: Use a high-speed A / D sampling chip to collect the input RF signal;

[0097] S2: FPGA performs amplitude correlation, preamble detection, and deinterleaving and decoding processing on the sampled data to obtain the value of each bit and add confidence to each bit;

[0098] S3: Send the signal to the CRC verification circuit for CRC verification. When the number of low confidence bits is within the allowable range of the threshold, the bit recovery operation can be performed, otherwise the received message is discarded;

[0099] S4: Send the message after the bit recovery into the FIFO inside the FPGA, and send an interrupt request at the same time, and the ARM processor reads the message from the FIFO.

Embodiment 3

[0101] Such as Figure 1~5 As shown, on the basis of Embodiment 1 or 2, the business module includes a navigation information processing module, an altitude information processing module and a Beidou short message processing module, and the navigation information processing module, an altitude information processing module and a Beidou short message processing module The text data processing modules are all connected with the ARM processor.

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Abstract

The invention discloses a multifunctional airborne navigation device and a signal processing unit, which is used to process all relevant business data onboard, and send the business data to an ADS-B communication unit with a radio frequency signal after encoding, and receive the ADS-B The radio frequency signal sent by the communication unit is parsed into an ADS‑B message, and sent to the service module after parsing; the service module is used to receive the ADS‑B message of the signal processing unit and make a relevant response to the control executive agency; ADS ‑B communication unit, used to receive the radio frequency signal of the signal processing unit, and send it to the radio frequency processing unit by the antenna, receive the radio frequency signal through the antenna and send it to the signal processing unit; strengthen the information flow between services, so that the airborne navigation equipment It can be configured more extensively and communicate data more effectively, thereby effectively reducing flight safety risks.

Description

technical field [0001] The invention relates to the field of aircraft airborne equipment, in particular to multifunctional airborne navigation equipment. Background technique [0002] With the development of my country's civil aviation, the demand for airborne communication and navigation equipment for large, medium and small aircraft is gradually increasing. Since different models have different requirements for this type of equipment, it is mainly affected by factors such as cost, modification and function. For large aircraft, cost is not a major factor, but a matter of functionality and modifications. Because the large aircraft are mainly transport aircraft, the installed on-board navigation equipment only has the function of ADS-B OUT, and lacks the function of ADS-B IN; while the small and medium-sized aircraft are affected by cost and modification factors, and some even do not have on-board navigation equipment. Navigation equipment is not conducive to the management...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B1/04H04B1/16G01S19/38
CPCH04B1/04H04B1/16G01S19/38
Inventor 赵泽荣
Owner 四川荣川通用航空有限责任公司