CN107783934B - Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method - Google Patents

Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method Download PDF

Info

Publication number
CN107783934B
CN107783934B CN201610780863.4A CN201610780863A CN107783934B CN 107783934 B CN107783934 B CN 107783934B CN 201610780863 A CN201610780863 A CN 201610780863A CN 107783934 B CN107783934 B CN 107783934B
Authority
CN
China
Prior art keywords
field
data
lable
mapping table
filtering
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201610780863.4A
Other languages
Chinese (zh)
Other versions
CN107783934A (en
Inventor
李国星
高志远
李盘文
安都勋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chinese Flight Test Establishment
Original Assignee
Chinese Flight Test Establishment
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chinese Flight Test Establishment filed Critical Chinese Flight Test Establishment
Priority to CN201610780863.4A priority Critical patent/CN107783934B/en
Publication of CN107783934A publication Critical patent/CN107783934A/en
Application granted granted Critical
Publication of CN107783934B publication Critical patent/CN107783934B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F15/00Digital computers in general; Data processing equipment in general
    • G06F15/16Combinations of two or more digital computers each having at least an arithmetic unit, a program unit and a register, e.g. for a simultaneous processing of several programs
    • G06F15/163Interprocessor communication
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F13/00Interconnection of, or transfer of information or other signals between, memories, input/output devices or central processing units
    • G06F13/38Information transfer, e.g. on bus
    • G06F13/40Bus structure
    • G06F13/4004Coupling between buses
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F13/00Interconnection of, or transfer of information or other signals between, memories, input/output devices or central processing units
    • G06F13/38Information transfer, e.g. on bus
    • G06F13/40Bus structure
    • G06F13/4063Device-to-bus coupling
    • G06F13/4068Electrical coupling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02DCLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D10/00Energy efficient computing, e.g. low power processors, power management or thermal management

Abstract

The invention relates to the field of test flight data acquisition of an airborne ARINC429 bus, in particular to a real-time acquisition and data filtering method of an airborne multi-channel ARINC429 bus. A traditional ARINC429 bus acquisition module usually adopts a separated component or a pure FPGA logic circuit, the separated component circuit is large in size, large in power consumption and expensive in protocol chip, and the pure FPGA logic circuit is poor in user programmable flexibility and brings inconvenience to practical application. The invention provides a solution scheme taking a DSP and an FPGA as core architectures, which fully utilizes the flexibility of the DSP and the rapid parallelism of the FPGA, realizes the real-time processing and screening of multi-channel ARINC429 bus data, and sends the data to a back board bus in a test flight test system according to a specific format and a sampling rate for the test flight test system to call. And the processing speed of screening the multichannel ARINC429 data words is greatly increased in a space exchange speed mode by a table look-up mode.

Description

Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method
Technical Field
The invention relates to the field of test flight data acquisition of an airborne ARINC429 bus, in particular to a real-time acquisition and data filtering method of an airborne multi-channel ARINC429 bus.
Background
In flight tests, an airborne ARINC429 bus is widely applied to various civil airplanes and military airplanes, test flight data acquisition often involves real-time acquisition and data filtering of the multichannel ARINC429 bus, and processing results are often sent to the ground through a telemetry link for real-time monitoring. Therefore, how to efficiently collect the multichannel ARINC429 bus signals is a research subject with practical engineering value.
In a test flight test system, an ARINC429 bus acquisition is often a module in the system. The test system can incorporate ARINC429 bus data into a data link of the test flight test system, and data sharing among devices is achieved. However, the traditional ARINC429 bus acquisition module usually adopts a separate component or a pure FPGA logic circuit, the separate component circuit has large volume, large power consumption and expensive protocol chip, and the pure FPGA logic circuit has poor user-programmable flexibility and brings inconvenience to practical application.
Disclosure of Invention
Under the framework of the test flight test system, the invention provides a solution taking the DSP and the FPGA as core frameworks, fully utilizes the flexibility of the DSP and the rapid parallelism of the FPGA, realizes the real-time processing and screening of the multichannel ARINC429 bus data, and sends the data to a back board bus in the test flight test system according to a specific format and a sampling rate for the test flight test system to call. In the architecture of the test flight test system, data can be transmitted to the next-level device through the backplane bus under the scheduling of the main control device.
An airborne multi-channel ARINC429 bus real-time acquisition and data filtering method is realized by a hardware platform with a DSP and an FPGA as a framework, the front end of the method is composed of 8 ARINC429 bus driving chips and used for converting ARINC429 level codes, and the data filtering method comprises the following steps:
first, a mapping configuration table is preset
Constructing 4 mapping tables according to the field values of a Lable field, an SDI field and an SSM field of an ARINC429 bus configured by a user, wherein the mapping table 1 stores the Lable configured by the user and a corresponding filtering mode, and comprises the steps of writing a Lable identification value into an address pointed by the value of the Lable and combining and filtering the SDI field and the SSM field; mapping table 2 stores the configuration of filtering the lab field, the SDI field and the SSM field; the mapping table 3 stores the configuration of filtering the Lable field and the SSM field; the mapping table 4 stores the configuration of filtering the Lable field and the SDI field;
then, data filtering
According to the value of a Lable field extracted from real-time data, searching whether a Lable configuration value exists in a mapping table 1, and if the identification value is false, discarding the data; if the identification value is true, entering a corresponding mapping table 2, a mapping table 3 or a mapping table 4 by combining a combined filtering mode of SDI fields and SSM fields; when the filtering mode is that the Lable field, the SDI field and the SSM field are required to be filtered, addressing in a mapping table 2 by taking data combined by the Lable field, the SDI field and the SSM field as an address, discarding the data if the value obtained by addressing is false, and keeping the data if the value obtained by addressing is true; when the filtering mode is that a Lable field and an SSM field need to be filtered, addressing in a mapping table 3 according to data combined by the Lable field and the SSM field as an address, if the value obtained by addressing is false, discarding the data, and if the value obtained by addressing is true, retaining the data; when the filtering mode is that the Lable field and the SDI field need to be filtered, addressing in a mapping table 4 by taking data combined by the Lable field and the SDI field as an address, if the value obtained by addressing is false, discarding the data, and if the value obtained by addressing is true, retaining the data;
and re-sending the filtered ARINC429 data back to a cache circuit of the FPGA according to a specified format and address, and reading by a back board bus of the standby load test system, thereby completing the real-time acquisition and filtration of the onboard eight-channel ARINC429 data words.
The invention utilizes the characteristics of rapidness and flexibility of a DSP program, and greatly accelerates the processing speed of screening the multichannel ARINC429 data words in a space exchange speed mode by a table look-up mode.
Drawings
FIG. 1 is a system framework diagram of the present invention;
FIG. 2 is a diagram of a mapping table structure according to the present invention.
Detailed Description
A real-time acquisition and data filtering method for an airborne multichannel ARINC429 bus is realized by a hardware platform with a DSP and an FPGA as a framework, the front end of the hardware platform is composed of 8 ARINC429 bus driving chips, an ARINC429 level code is converted into an LVTTL level, the analysis of an ARINC429 data word is completed by an ARINC429 protocol IP in the FPGA, the analyzed data is stored in an FPGA cache circuit according to a channel, a DSP program inquires the storage condition of the ARINC429 data word in each channel cache circuit in turn through an XINTF bus, and the ARINC429 data word is read into the cache of the DSP.
In order to improve the filtering efficiency, the invention provides a data filtering method with space exchange efficiency, which is used for quickly filtering ARINC429 data words according to the judgment condition preset by a user, namely, filtering the data by taking the data as an address to be quickly looked up, and screening the ARINC429 data words required by the user from an ARINC429 bus in real time.
The data filtering method comprises the following steps:
first, a mapping configuration table is preset
And constructing 4 mapping tables according to the ARINC429 bus Lable field, the SDI field and the SSM field value configured by the user, and storing ARINC429 bus data word information configured by the user. The mapping table 1 stores the Lable configured by the user and the corresponding filtering mode, including writing the Lable identification value in the address pointed by the value of the Lable, and the combined filtering mode of the SDI field and the SSM field. Mapping table 2 stores the configuration of filtering the lab field, the SDI field and the SSM field; the mapping table 3 stores the configuration of filtering the Lable field and the SSM field; the mapping table 4 stores the configuration of filtering the lab field and the SDI field.
Then, data filtering
According to the value of a Lable field extracted from real-time data, searching whether a Lable configuration value exists in a mapping table 1, and if the identification value is false, discarding the data; and if the identification value is true, combining a combined filtering mode of SDI fields and SSM fields, and entering a corresponding mapping table 2, a mapping table 3 or a mapping table 4. When the filtering mode is that all the Lable field, the SDI field and the SSM field need to be filtered, combining the fields of the Lable field, the SDI field and the SSM field in the data, addressing in a mapping table 2 by taking the combined data as an address, discarding the data if the value obtained by addressing is false, and keeping the data if the value obtained by addressing is true; when the filtering mode is that the Lable field and the SSM field need to be filtered, combining the Lable field and the SSM field value in the data, addressing in a mapping table 3 by taking the combined data as an address, discarding the data if the value obtained by addressing is false, and keeping the data if the value obtained by addressing is true; when the filtering mode is that the Lable field and the SDI field need to be filtered, the fields of the Lable field and the SDI field in the data are combined, the combined data is used as an address to be addressed in the mapping table 4, if the value obtained by addressing is false, the data is discarded, and if the value obtained by addressing is true, the data is retained.
And re-sending the filtered ARINC429 data back to a cache circuit of the FPGA according to a specified format and address, and reading by a back board bus of the standby load test system, thereby completing the real-time acquisition and filtration of the onboard eight-channel ARINC429 data words.

Claims (1)

1. An airborne multi-channel ARINC429 bus real-time acquisition and data filtering method is characterized in that: the data filtering method is realized by a hardware platform with a DSP and an FPGA as a framework, the front end of the data filtering method is composed of 8 ARINC429 bus driving chips and used for converting ARINC429 level codes, and the data filtering method comprises the following steps:
first, a mapping configuration table is preset
Constructing 4 mapping tables according to the field values of a Lable field, an SDI field and an SSM field of an ARINC429 bus configured by a user, wherein the mapping table 1 stores the Lable configured by the user and a corresponding filtering mode, and comprises the steps of writing the field value of the Lable into an address pointed by the value of the Lable and combining and filtering the SDI field and the SSM field; mapping table 2 stores the configuration of filtering the lab field, the SDI field and the SSM field; the mapping table 3 stores the configuration of filtering the Lable field and the SSM field; the mapping table 4 stores the configuration of filtering the Lable field and the SDI field;
then, data filtering
According to the Lable field value extracted from the real-time data, whether the Lable field value exists or not is searched in a mapping table 1, and if the field value is false, the data is discarded; if the field value is true, entering a corresponding mapping table 2, a mapping table 3 or a mapping table 4 by combining with a combined filtering mode of SDI and SSM fields; when the filtering mode is that the Lable field, the SDI field and the SSM field are required to be filtered, addressing in a mapping table 2 by taking data combined by the Lable field, the SDI field and the SSM field as an address, discarding the data if the value obtained by addressing is false, and keeping the data if the value obtained by addressing is true; when the filtering mode is that a Lable field and an SSM field need to be filtered, addressing in a mapping table 3 according to data combined by the Lable field and the SSM field as an address, if the value obtained by addressing is false, discarding the data, and if the value obtained by addressing is true, retaining the data; when the filtering mode is that the Lable field and the SDI field need to be filtered, addressing in a mapping table 4 by taking data combined by the Lable field and the SDI field as an address, if the value obtained by addressing is false, discarding the data, and if the value obtained by addressing is true, retaining the data;
and re-sending the filtered ARINC429 data back to a cache circuit of the FPGA according to a specified format and address, and reading by a back board bus of the standby load test system, thereby completing the real-time acquisition and filtration of the onboard eight-channel ARINC429 data words.
CN201610780863.4A 2016-08-30 2016-08-30 Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method Active CN107783934B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610780863.4A CN107783934B (en) 2016-08-30 2016-08-30 Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610780863.4A CN107783934B (en) 2016-08-30 2016-08-30 Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method

Publications (2)

Publication Number Publication Date
CN107783934A CN107783934A (en) 2018-03-09
CN107783934B true CN107783934B (en) 2021-05-28

Family

ID=61450404

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610780863.4A Active CN107783934B (en) 2016-08-30 2016-08-30 Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method

Country Status (1)

Country Link
CN (1) CN107783934B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109445325A (en) * 2018-10-15 2019-03-08 四川九洲空管科技有限责任公司 A kind of high speed ARINC429 data processing method based on FPGA
CN111163116B (en) * 2020-04-08 2020-07-10 成都新动力软件有限公司 Equipment for extracting large-flow network data parameters
CN112765069B (en) * 2021-01-14 2022-11-01 凌云科技集团有限责任公司 ARINC429 bus ICD back-solving method, device and system
CN114968892B (en) * 2022-06-17 2023-10-20 北京润科通用技术有限公司 Scheduling hardware circuit and scheduling method

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5119482A (en) * 1989-12-18 1992-06-02 The United States Of America As Represented By The Secretary Of The Air Force Flight system for converting 12 volts 32-bit INS data into 5 volts 8-bit data pattern in real time
CA2502815A1 (en) * 2004-04-13 2005-10-13 Pratt & Whitney Canada Corp. Method and apparatus for isolating aircraft equipment
US8219888B2 (en) * 2002-11-26 2012-07-10 Qualcomm Incorporated Multi-channel transmission and reception with block coding in a communication system
CN102932489A (en) * 2012-10-28 2013-02-13 中国电子科技集团公司第十研究所 Multi-channel ARINC429 bus interface
CN202854804U (en) * 2012-09-06 2013-04-03 中国航空工业集团公司第六三一研究所 Military onboard bus interface conversion system based on SOC technology
CN203117756U (en) * 2013-02-27 2013-08-07 陕西千山航空电子有限责任公司 Airplane-mounted real-time fault diagnosis unit
CN103823785A (en) * 2014-03-25 2014-05-28 北京航空航天大学 Multi-way ARINC429 data transmit-receive circuit structure based on development of DSP and CPLD
CN103914888A (en) * 2014-03-31 2014-07-09 四川九洲空管科技有限责任公司 Data recording and analyzing method for airborne collision avoidance system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5119482A (en) * 1989-12-18 1992-06-02 The United States Of America As Represented By The Secretary Of The Air Force Flight system for converting 12 volts 32-bit INS data into 5 volts 8-bit data pattern in real time
US8219888B2 (en) * 2002-11-26 2012-07-10 Qualcomm Incorporated Multi-channel transmission and reception with block coding in a communication system
CA2502815A1 (en) * 2004-04-13 2005-10-13 Pratt & Whitney Canada Corp. Method and apparatus for isolating aircraft equipment
CN202854804U (en) * 2012-09-06 2013-04-03 中国航空工业集团公司第六三一研究所 Military onboard bus interface conversion system based on SOC technology
CN102932489A (en) * 2012-10-28 2013-02-13 中国电子科技集团公司第十研究所 Multi-channel ARINC429 bus interface
CN203117756U (en) * 2013-02-27 2013-08-07 陕西千山航空电子有限责任公司 Airplane-mounted real-time fault diagnosis unit
CN103823785A (en) * 2014-03-25 2014-05-28 北京航空航天大学 Multi-way ARINC429 data transmit-receive circuit structure based on development of DSP and CPLD
CN103914888A (en) * 2014-03-31 2014-07-09 四川九洲空管科技有限责任公司 Data recording and analyzing method for airborne collision avoidance system

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
Arinc429 Bus-based Multi-Dsp, Fpga Component Program Serial Load;Yongchao Zeng 等;《National Conference on Information Technology and Computer Science》;20121231;第1026-1029页 *
ARINC-429总线信号源电路设计与开发;李国星 等;《硅谷》;20111231(第10期);第88-93页 *
基于DSP与FPGA多路ARINC429数据通信系统设计;侯翔昊 等;《电力电子技术》;20130831;第47卷(第8期);第107-108页 *
多通道ARINC429 总线检查仪;高志远;《电子设计工程》;20150430;第23卷(第8期);第55页 *

Also Published As

Publication number Publication date
CN107783934A (en) 2018-03-09

Similar Documents

Publication Publication Date Title
CN107783934B (en) Airborne multi-channel ARINC429 bus real-time acquisition and data filtering method
CN106444505B (en) A kind of multi-channel synchronous signal acquiring system
DE602006010986D1 (en) SPATIAL-TIME SELF-ORGANIZING CARD
CN103107923A (en) Fiber channel (FC) network data monitoring system and method based on system on chip (SOC) technology
CN103957136A (en) Moonlet CAN bus monitoring system
CN106019350A (en) Nuclear pulse signal acquisition device and system
CN208795371U (en) A kind of multi-photon coincidence counting device
CN111190048A (en) Multichannel lightning current information acquisition board card
CN1909499B (en) Multi-path data collecting device and method
CN109215657A (en) A kind of grain depot monitoring voice robot and its application
CN204945685U (en) A kind of air sampler with tele-control system
CN212364596U (en) Three-system eight-frequency-point satellite receiver board and satellite receiver
CN101067639A (en) De-excitation system performance test analysing method and test analyzer thereof
CN211453476U (en) Full-waveform ultrasonic flaw detector
CN207339867U (en) A kind of time information synchronization system
CN204423422U (en) Based on the information collection apparatus of Internet of Things
CN204576136U (en) A kind of parallel data high speed acquisition device
CN105653207A (en) Real-time analysis method and system of flash memory interface information
CN202939602U (en) Parallel data collection system based on VXI bus
US20200355729A1 (en) Changing the Manner in which an Electronic Test Instrument Filters an Input Signal based on a Characteristic of the Electronic Test Instrument
CN201398223Y (en) High-speed data simulation source processing device
CN105702301A (en) Method and system for fetching effective signal of flash memory, and logic analyzer
CN106603951A (en) Airborne video data recording equipment
CN211979033U (en) Multichannel lightning current information acquisition board card
CN104200540B (en) Data recording equipment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant