CN104699544A - BIT communication method for redundancy computer system - Google Patents

BIT communication method for redundancy computer system Download PDF

Info

Publication number
CN104699544A
CN104699544A CN201310682895.7A CN201310682895A CN104699544A CN 104699544 A CN104699544 A CN 104699544A CN 201310682895 A CN201310682895 A CN 201310682895A CN 104699544 A CN104699544 A CN 104699544A
Authority
CN
China
Prior art keywords
passage
computer system
bit
command
communication
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.)
Granted
Application number
CN201310682895.7A
Other languages
Chinese (zh)
Other versions
CN104699544B (en
Inventor
佘刚
武方方
冯博
谢卫
董强
郑勇
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.)
No 618 Research Institute of China Aviation Industry
Original Assignee
No 618 Research Institute of China Aviation Industry
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 No 618 Research Institute of China Aviation Industry filed Critical No 618 Research Institute of China Aviation Industry
Priority to CN201310682895.7A priority Critical patent/CN104699544B/en
Publication of CN104699544A publication Critical patent/CN104699544A/en
Application granted granted Critical
Publication of CN104699544B publication Critical patent/CN104699544B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Maintenance And Management Of Digital Transmission (AREA)
  • Debugging And Monitoring (AREA)

Abstract

The invention belongs to a computer communication technology, and relates to improvement on a BIT communication method for a redundancy computer. The communication method is based on the application of a redundancy computer system with more than two channels. A common communication manner is to connect ground test equipment with each channel of the redundancy computer system in a point-to-point manner and transmit a command request to multiple channels in one time by virtue of ground test software, and transmission time differences easily cause the problems of loss of synchronization between the channels of the redundancy computer, channel failures and the like, and even cause the incapability of smoothly finishing BIT work. In order to solve the problem, the conventional point-to-point multi-line connection communication manner is replaced by a manner of connecting a communication bus to any bus board of the redundancy computer and forwarding a command by bus board software in a one-to-many manner, and then effective command passages are pre-identified by redundancy computer system software, so that command responding is simplified, and the problem is well solved.

Description

The means of communication that a kind of redundance computer system BIT tests
Technical field
The invention belongs to computer communication technology field, relate to the improvement to the means of communication that redundance computer system BIT tests.
Background technology
The means of communication that existing redundance computer system BIT tests all are adopted many rigid lines and are connected to each channel bus plate of redundance computer system, and method is as follows:
Ground checkout equipment is connected to redundance computer system passage A, B bus board by many rigid lines by step one;
Step 2 ground checkout equipment sends the effective item test command of BIT to passage A, B, and passage A, B bus board receives test command;
Effective for the BIT received in step 2 item test command is sent to the host CPU plate of passage A, B by step 3 passage A, B bus board simultaneously;
The host CPU plate of step 4 passage A, B receives respectively from passage A, B effective BIT test command to bus board, judge passage A, B test command effectively and consistent after start BIT test, otherwise this subcommand failure, wait for test command next time.
The object of the invention is: propose a kind of reliable communicating method connecting simple, applicable redundancy computer system BIT and test.
Technical scheme of the present invention is:
The means of communication that redundance computer system BIT tests, is characterized in that:
The communication port of ground checkout equipment with redundance computer system passage A bus board is connected by a rigid line by step 1;
Step 2 ground checkout equipment sends the effective item test command of BIT, enters redundance computer system bus plate by passage A;
Effective for the BIT received in step 2 item test command is sent to the host CPU plate of passage A, B by step 3 bus board simultaneously;
The host CPU plate of step 4 passage A, B receives and after identifying effective BIT test command, starts BIT test.
Advantage of the present invention is:
A) rigid line connects simple
Redundance computer system was when carrying out BIT test in the past, all needed many rigid lines to be connected to, and the method only needs a rigid line to connect, and simplifies signal wiring complexity;
B) synchronism, real-time are good
An event command sends to redundance computing machine by bus board software simultaneously, and the synchronism of computing machine significantly improves, more timely to the response of order.At multiplicated system synchronism detection, during channel combined test, measuring stability obviously improves;
C) Airborne Software command recognition simplifies
The method, redundance computer software is after starting to recognize effective command channel, catching of follow-up all event command, effective order passage only need be inquired about just passable at each duty cycle, no longer need to carry out catching of effective order to each passage, prevent and need hyperchannel command recognition and issuable mistake, running software sequential is clear.
Accompanying drawing explanation
Fig. 1 is General Implementing step schematic diagram
Fig. 2 is idiographic flow schematic diagram
Fig. 3 is connection diagram
Embodiment
Be described in further detail this method below in conjunction with accompanying drawing, as shown in Figure 1, idiographic flow step as shown in Figure 2, is described in detail as follows General Implementing step:
The identification of 1 passage effective order
A) connect a notebook computer (ground checkout equipment) and 2 redundancy computer passage A bus board serial ports with a Serial Port Line, connection diagram is as Fig. 3;
B) system power-up starts, and whether this passage of the equal periodic queries of passage A, B bus board software has the BIT test command meeting communications protocol.After notebook computer sends BIT test instruction, passage A bus board receives this BIT test command;
C) after passage A bus board software recognizes this order effective order, namely by data bus, this BIT test command is sent to this passage host CPU plate, also be forwarded to channel B host CPU plate, such passage A, B host CPU plate receives BIT test command simultaneously simultaneously.
2 host CPU plate identification effective orders
Because passage A, B host CPU plate software first time recognizes effective order, now all recording channel A is the command channel of BIT test, and for preventing follow-up test from occurring disable instruction, after this order from passage A only inquired about by passage A, B host CPU plate software.
3 response test orders also send test data
A) passage A, B receives and after identifying effective BIT test command, starts BIT test simultaneously, complete the execution to test command by topworks;
B), after having tested, passage A, B host CPU plate software all sends to passage A bus board software by data bus each self-test data;
4 Synthetic Measuring Data are also uploaded to ground checkout equipment
A) passage A bus board software the test result data receiving A, B two passages all after, passage A bus board software carries out comprehensively to the test result data of passage A, B according to communications protocol, be uploaded to ground checkout equipment after comprehensively completing, complete the test assignment that this redundance computer system BIT tests.
B) passage A bus board software continues periodically to wait for new test command, until complete all test jobs.

Claims (1)

1. means of communication for redundance computer system BIT test, is characterized in that,
The communication port of ground checkout equipment with redundance computer system passage A bus board is connected by a rigid line by step 1;
Step 2 ground checkout equipment sends the effective item test command of BIT, and passage A bus board receives test command;
Effective for the BIT received in step 2 item test command is sent to the host CPU plate of passage A, B by step 3 bus board simultaneously;
The host CPU plate of step 4 passage A, B receives and after identifying effective BIT test command, starts BIT test.
CN201310682895.7A 2013-12-10 2013-12-10 A kind of means of communication of redundance computer system BIT tests Active CN104699544B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310682895.7A CN104699544B (en) 2013-12-10 2013-12-10 A kind of means of communication of redundance computer system BIT tests

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310682895.7A CN104699544B (en) 2013-12-10 2013-12-10 A kind of means of communication of redundance computer system BIT tests

Publications (2)

Publication Number Publication Date
CN104699544A true CN104699544A (en) 2015-06-10
CN104699544B CN104699544B (en) 2017-10-31

Family

ID=53346706

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310682895.7A Active CN104699544B (en) 2013-12-10 2013-12-10 A kind of means of communication of redundance computer system BIT tests

Country Status (1)

Country Link
CN (1) CN104699544B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106873355A (en) * 2015-12-14 2017-06-20 中国航空工业第六八研究所 A kind of selection of multipriority maintenance test instruction with control law instruction and changing method
CN112596976A (en) * 2020-12-17 2021-04-02 中国航空工业集团公司沈阳飞机设计研究所 Method for monitoring effectiveness of processor between redundancies

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7657789B1 (en) * 2005-06-10 2010-02-02 Microsoft Corporation Multi-machine testing system and method for testing software

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7657789B1 (en) * 2005-06-10 2010-02-02 Microsoft Corporation Multi-machine testing system and method for testing software

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
韩建军: "基于BIT的双通道容错电子控制器设计及验证", 《中国优秀硕士学位论文全文数据库》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106873355A (en) * 2015-12-14 2017-06-20 中国航空工业第六八研究所 A kind of selection of multipriority maintenance test instruction with control law instruction and changing method
CN106873355B (en) * 2015-12-14 2019-12-24 中国航空工业第六一八研究所 Method for selecting and switching multi-priority maintenance test instruction and control law instruction
CN112596976A (en) * 2020-12-17 2021-04-02 中国航空工业集团公司沈阳飞机设计研究所 Method for monitoring effectiveness of processor between redundancies

Also Published As

Publication number Publication date
CN104699544B (en) 2017-10-31

Similar Documents

Publication Publication Date Title
CN202285113U (en) Power distribution unit control system
CN104199796B (en) IIC communication means and the embedded system for realizing IIC communications
CN103490959B (en) A kind of dual-redundant CAN bus fault detection method
CN104615401A (en) FPGA (field programmable gate array) based KVM (kernel-based virtual machine) implementing method
US20160313727A1 (en) Method and system for interacting master and slave information in real time
CN104731007A (en) Backboard communication assembly and communication method for function security PLC
CN104375923A (en) Hard disk drive (HDD) running state detection system
CN110427283B (en) Dual-redundancy fuel management computer system
CN104951421B (en) A kind of automatic numbering of serial bus communication equipment and kind identification method and device
CN101170438A (en) A remote serial port debugging method and its system
CN103573281A (en) Hydraulic support electrohydraulic control system
CN103186440B (en) Detect subcard method, apparatus and system in place
CN104699544A (en) BIT communication method for redundancy computer system
CN103929424A (en) Hardware and software combined two-out-three safety data processing and arbitration method and device thereof
CN104483960A (en) Automobile diagnosis communication module data transceiving parallel processing method
CN104461800A (en) Hard disk running state detection system
CN102255766B (en) Server system
CN202548753U (en) Computer and shielding protection system thereof
CN206460446U (en) A kind of supervising device for ruggedized computer mainboard
CN105573141A (en) Touch-type photoelectric pod system emulator
CN113253652A (en) Unit communication control device, method and unit
CN105620515A (en) Railway signal power source remote monitoring system
CN108011791A (en) A kind of airborne dual-redundancy CAN communication system configuration
CN104062530A (en) Mobile terminal hardware fault detecting device and method
CN103517307B (en) A kind of remote debugging system based on TD-SCDMA

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant