CN108228221A - A kind of programmable logic online upgrading method based on 1553B buses - Google Patents
A kind of programmable logic online upgrading method based on 1553B buses Download PDFInfo
- Publication number
- CN108228221A CN108228221A CN201611153202.5A CN201611153202A CN108228221A CN 108228221 A CN108228221 A CN 108228221A CN 201611153202 A CN201611153202 A CN 201611153202A CN 108228221 A CN108228221 A CN 108228221A
- Authority
- CN
- China
- Prior art keywords
- logic
- missile
- prom
- fpga
- online upgrading
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F8/00—Arrangements for software engineering
- G06F8/60—Software deployment
- G06F8/65—Updates
Abstract
The present invention is to solve the problems, such as shooting missile-borne computer fpga logic online upgrading, proposes to carry out online upgrading to missile-borne computer inside FPGA by the external 1553B bus interface of guided missile.Belong to missile-borne computer fpga logic online upgrading technical field.This method effectively prevents the problem of maintenance cost caused by removing guided missile increases, guided missile reliability reduces.
Description
Technical field
The invention belongs to missile-borne computer fpga logic online upgrading technical fields.
Background technology
Guided missile volume is limited, and the compact-sized size of on-board electronics is small, is solidified as a whole after guided missile is packed into guided missile, is led to
It cannot often dismantle, dismounting usually requires to return factory's progress, of high cost, and guided missile reliability can be caused to reduce, service life decline, no
Conducive to the permanent storage and maintenance of guided missile.In addition, guided missile has a storage life requirement, and general 16 years to 21 years, certain guided missile storages
Time is longer, and turning over the phase in head can be to having initial workpiece or wearing detail to replace, to having the storage chip of data hold time again
Carry out programming.The configuration of field programmable gate array (FPGA) is manufactured with PROM generally use CMOS NOR FLASH techniques, is had
Data hold time requirement, then must programming again more than data hold time.It can be by the jtag interface of PROM chips to it
The logical versions of storage carry out online upgrading, but guided missile externally provides 1553B bus interface at present, does not provide internal unit
Jtag interface.Therefore, how to be realized under the conditions of guided missile is not torn open aobvious to the online upgrading of missile-borne computer fpga logic and detection
It obtains particularly important.
Invention content
The present invention is to solve the problems, such as shooting missile-borne computer fpga logic online upgrading, propose to pass through
The external 1553B bus interface of guided missile carries out online upgrading to missile-borne computer inside FPGA.
It is as follows to implement step:
First, in the air under state, missile-borne computer is established by missile-borne 1553B bus interface and external detection equipment to be connected
It connects, waits fpga logic online upgrading order to be received;
Secondly, missile-borne computer receives fpga logic online upgrading order, and missile-borne computer is connect by processor GPIO
Mouth control FPGA carries out logic switch, and switching fpga logic is basic logic;
Again, processor receives function logic object code to be upgraded by 1553B buses;
Then, processor, will be to be upgraded by the PROM jtag interface control logics inside local bus access FPGA
Function logic code is by the programming of PROM jtag interfaces into Memory inside PROM;
Then, the PROM jtag interfaces control logic that processor is accessed by local bus inside FPGA is read in PROM
Portion Memory cures information, is verified;
Then, if verified successfully, programming success, processor is upgraded by 1553B bus feedbacks to be completed, and otherwise report rises
Grade failure;
Finally, system reset, the function logic automatic running after upgrading.
As previously mentioned, used PROM chips are Xilinx companies XCFP PROM or domestic compatible chips, it is used
FGPA chip Xilinx company's chips or compatible chip, the fpga logic object code that missile-borne computer receives are IEEE Std
1149.1Boundary-Scan (JTAG) Serial Vector Format (SVF) file.
Description of the drawings
Fig. 1 is a kind of programmable logic online upgrading method schematic based on 1553B buses.
Specific embodiment
First, in the air under state, missile-borne computer is established by missile-borne 1553B bus interface and external detection equipment to be connected
It connects, waits fpga logic online upgrading order to be received;
Secondly, missile-borne computer receives fpga logic online upgrading order, controls PROM chip EX_EXT_SEL# signals
For low, REV_SEL [0] signal be low, REV_SEL [1] signal it is low, and enabled fpga chip PROG_G signals are low, are started
FPGA is reloaded, and switching fpga logic is determined function logic online upgrading for basic logic;
Again, processor receives function logic object code to be upgraded by 1553B buses;
Then, processor, will be to be upgraded by the PROM jtag interface control logics inside local bus access FPGA
Function logic code is by the programming of PROM jtag interfaces into Memory inside PROM;
Then, the PROM jtag interfaces control logic that processor is accessed by local bus inside FPGA is read in PROM
Portion Memory cures information, is verified;
Then, if verified successfully, programming success, processor is upgraded by 1553B bus feedbacks to be completed, and otherwise report rises
Grade failure;
Finally, system reset, the function logic automatic running after upgrading.
In one embodiment of the present of invention, certain model missile-borne computer project, processor uses Power PC Processor,
FPGA uses the XC2V3000 of Xilinx companies production, PROM to use XCF32P, and 1553B bus control protocols are real using logic
Existing, 1553B interface drivers use 1553 transceiver of HKA32201 binary channels, and data transmission rate supports 1Mbps and 2Mbps.Through
Overtesting verifies that system run all right is reliable.
Claims (2)
1. the programmable logic online upgrading method based on 1553B buses, it is characterised in that comprise the steps of:
Step 1:In the air under state, missile-borne computer is established by missile-borne 1553B bus interface and external detection equipment and connected,
Etc. fpga logic online upgrading order to be received;
Step 2:Missile-borne computer receives fpga logic online upgrading order, and missile-borne computer passes through processor GPIO interface control
FPGA processed carries out logic switch, and switching fpga logic is basic logic;
Step 3:Processor receives function logic object code to be upgraded by 1553B buses;
Step 4:Processor accesses the PROM jtag interface control logics inside FPGA by local bus, by work(to be upgraded
Can logical code by the programming of PROM jtag interfaces into Memory inside PROM;
Step 5:The PROM jtag interfaces control logic that processor accesses inside FPGA by local bus is read inside PROM
Memory cures information, is verified;
Step 6:If verified successfully, programming success, processor is upgraded by 1553B bus feedbacks to be completed, otherwise report upgrading
Failure;
Step 7:System reset, the function logic automatic running after upgrading.
2. the programmable logic online upgrading method according to claim 1 based on 1553B buses, it is characterised in that:Institute
The PROM chips used is Xilinx companies XCFP PROM or domestic compatible chips, used FGPA chips Xilinx companies
Chip or compatible chip, the fpga logic object code that missile-borne computer receives are IEEE Std 1149.1Boundary-Scan
(JTAG) Serial Vector Format (SVF) file.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611153202.5A CN108228221A (en) | 2016-12-14 | 2016-12-14 | A kind of programmable logic online upgrading method based on 1553B buses |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611153202.5A CN108228221A (en) | 2016-12-14 | 2016-12-14 | A kind of programmable logic online upgrading method based on 1553B buses |
Publications (1)
Publication Number | Publication Date |
---|---|
CN108228221A true CN108228221A (en) | 2018-06-29 |
Family
ID=62638432
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611153202.5A Pending CN108228221A (en) | 2016-12-14 | 2016-12-14 | A kind of programmable logic online upgrading method based on 1553B buses |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108228221A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114036097A (en) * | 2021-10-09 | 2022-02-11 | 中国航空工业集团公司洛阳电光设备研究所 | Domestic FPGA (field programmable Gate array) logic online upgrading method for improving maintainability of photoelectric product |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030023771A1 (en) * | 2001-07-30 | 2003-01-30 | Erickson Michael John | Method for accessing scan chains and updating EEPROM-resident FPGA code through a system mangement processor and JTAG bus |
CN102053850A (en) * | 2010-12-17 | 2011-05-11 | 天津曙光计算机产业有限公司 | Method for on-line FPGA logic upgrade |
CN104035803A (en) * | 2014-06-25 | 2014-09-10 | 浪潮(北京)电子信息产业有限公司 | Method, device and programmer for updating CPLD/FPGA firmware |
CN105279127A (en) * | 2015-11-25 | 2016-01-27 | 哈尔滨工业大学 | FPGA program downloading system based on PCI or PCIe bus, and method |
CN105955783A (en) * | 2016-05-09 | 2016-09-21 | 浙江大学 | Method for downloading remote FPGA logic codes on basis of FPGA control |
-
2016
- 2016-12-14 CN CN201611153202.5A patent/CN108228221A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030023771A1 (en) * | 2001-07-30 | 2003-01-30 | Erickson Michael John | Method for accessing scan chains and updating EEPROM-resident FPGA code through a system mangement processor and JTAG bus |
CN102053850A (en) * | 2010-12-17 | 2011-05-11 | 天津曙光计算机产业有限公司 | Method for on-line FPGA logic upgrade |
CN104035803A (en) * | 2014-06-25 | 2014-09-10 | 浪潮(北京)电子信息产业有限公司 | Method, device and programmer for updating CPLD/FPGA firmware |
CN105279127A (en) * | 2015-11-25 | 2016-01-27 | 哈尔滨工业大学 | FPGA program downloading system based on PCI or PCIe bus, and method |
CN105955783A (en) * | 2016-05-09 | 2016-09-21 | 浙江大学 | Method for downloading remote FPGA logic codes on basis of FPGA control |
Non-Patent Citations (2)
Title |
---|
朱艳芳: "一种基于RS422的DSP应用程序的在线升级方法", 《航天制造技术》 * |
邱育杰等: "DSP和JTAG接口的FPGA系统在线编程方法", 《新器件新技术》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114036097A (en) * | 2021-10-09 | 2022-02-11 | 中国航空工业集团公司洛阳电光设备研究所 | Domestic FPGA (field programmable Gate array) logic online upgrading method for improving maintainability of photoelectric product |
CN114036097B (en) * | 2021-10-09 | 2024-03-01 | 中国航空工业集团公司洛阳电光设备研究所 | Domestic FPGA logic online upgrading method for improving maintenance of photoelectric product |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105938450B (en) | The method and system that automatic debugging information is collected | |
US11775320B2 (en) | Overflow detection and correction in state machine engines | |
CN107562437B (en) | FPGA (field programmable Gate array) online upgrading system and method based on MicroBlaze soft core | |
US9213552B2 (en) | Device for reprogramming an embedded system that modifies a boot loader of the embedded system to accept larger amounts of data per singular write event | |
CN204028898U (en) | The server of a kind of hard disk, any mixed insertion of compatible multiple solid state hard disc | |
CN104035803A (en) | Method, device and programmer for updating CPLD/FPGA firmware | |
US9552279B2 (en) | Data bus network interface module and method therefor | |
CN102955474A (en) | Measurement control method and system of automobile ECU (electronic control unit) | |
CN103941619A (en) | Reconfigurable microcomputer protection development platform based on FPGA | |
CN103970569A (en) | Server BIOS offline upgrading method | |
CN110413298A (en) | The method that single-chip microcontroller serially upgrades and debugs is carried out based on Labwindows platform | |
CN104199707A (en) | System and method for upgrading FPGAs | |
CN101604248B (en) | Embedded system for correcting programs in read only memory and realization method thereof | |
CN108228221A (en) | A kind of programmable logic online upgrading method based on 1553B buses | |
CN106354598A (en) | One-time programmable microcontroller debugging method based on flash memory | |
US20190271740A1 (en) | Non-intrusive on-chip debugger with remote protocol support | |
CN101763324B (en) | Method for realizing equipment simulating and device thereof | |
CN101788946B (en) | Method and device for sintering firmware connected with E2PROM (Electrically Erasable Programmable Read-Only Memory) on CPLD (Complex Programable Logic Device) | |
CN103544079B (en) | Flash memory chip data recovery achieving system and method based on programmable logic controller | |
US8976801B2 (en) | Short packet transmission | |
CN104572515B (en) | Tracking module, method, system and on-chip system chip | |
CN105138379A (en) | Method for on-line upgrading based on Ymodem protocol | |
CN203909780U (en) | Vehicle remote upgrading device | |
CN105868042B (en) | A kind of watchdog circuit | |
CN201378317Y (en) | Codes download system adopting JTAG mode |
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 | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180629 |