CN110069030A - A kind of unmanned aerial vehicle (UAV) control core buckle - Google Patents
A kind of unmanned aerial vehicle (UAV) control core buckle Download PDFInfo
- Publication number
- CN110069030A CN110069030A CN201910304904.6A CN201910304904A CN110069030A CN 110069030 A CN110069030 A CN 110069030A CN 201910304904 A CN201910304904 A CN 201910304904A CN 110069030 A CN110069030 A CN 110069030A
- Authority
- CN
- China
- Prior art keywords
- xazu5ev
- 1sfvc784q
- uav
- aerial vehicle
- unmanned aerial
- 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
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/24—Pc safety
- G05B2219/24215—Scada supervisory control and data acquisition
Abstract
The invention discloses a kind of unmanned aerial vehicle (UAV) control core buckles, it include: the core processor of model XAZU5EV-1SFVC784Q, the I/O pin of the XAZU5EV-1SFVC784Q connects USB3.0, Gen3 × 4 PCIe, PCIe 2 × 4, USB2.0 PHYs, Gigabit Ethernet PHYs, high speed interface, LVDS I/O port, the I/O pin of the XAZU5EV-1SFVC784Q connects FX10-168 connector, the FX10-168 connector connects 8 pairs of MGT differential signals, core buckle veneer configuration includes: the DDR4 of 8GB+2GB, the EMMC fla of 64GB The QSPI flash of sh, 512Mb, wherein the EMMC flash of the QSPI flash and 64GB of 64MB are connected to the DDR4 SDRAM of DDR4 SDRAM and PLProgrammable the Logic programmable logic of Processing System processing system, when specifically used, the buckle is buckled on bottom plate, the buckle input power 5-12V.It is to solve the problems such as expansion I/O interface is not few, complete using function, design buckle area is larger.
Description
Technical field
The present invention relates to unmanned aerial vehicle (UAV) control technical field, in particular to a kind of unmanned aerial vehicle (UAV) control core buckle.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.With section
The application field of the development of skill, unmanned plane is more and more extensive, for example is used as reconnaissance plane, target drone, takes photo by plane, disaster relief etc..But
It is that unmanned aerial vehicle (UAV) control hardware structure in the prior art also has the disadvantage that the I/O interface of 1. extensions is few, is unable to satisfy increasingly
More application interface demands；2. it is not complete enough using function, it is unable to satisfy the demand of user's multifunctional use；3. designing buckle face
Product is larger, cannot achieve in small space and works；4. design is incomplete, subsequent upgrade is inconvenient, may bring production cost
The problems such as high and wasting of resources.
Summary of the invention
For above-mentioned deficiency in the prior art, the present invention provides a kind of unmanned aerial vehicle (UAV) control core buckles, with solution
The problems such as certainly expansion I/O interface is not few, complete using function, design buckle area is larger.
In order to achieve the above object of the invention, the technical solution adopted by the present invention are as follows:
A kind of unmanned aerial vehicle (UAV) control core buckle, comprising: the core processor of model XAZU5EV-1SFVC784Q, it is described
XAZU5EV-1SFVC784Q I/O pin connection USB3.0, PCIe Gen3 × 4, PCIe 2 × 4, USB2.0 PHYs,
The I/O pin of Gigabit Ethernet PHYs, high speed interface, LVDS I/O port, the XAZU5EV-1SFVC784Q connects
FX10-168 connector is connect, the FX10-168 connector connects 8 pairs of MGT differential signals, and core buckle veneer configuration includes:
The QSPI flash of EMMC flash of DDR4,64GB of 8GB+2GB, 512Mb, wherein the QSPI flash and 64GB of 64MB
EMMC flash be connected to the DDR4 SDRAM and PLProgrammable of Processing System processing system
When specifically used, which is buckled on bottom plate by the DDR4 SDRAM of Logic programmable logic, the described buckle input power
5-12V。
Further, the XAZU5EV-1SFVC784Q QSPI flash can start out of plate, can also be from EMMC
Flash or external SD card starting.
Further, which has 6 user lamps, and two of them user lamp connects Processing System
Processing system, 1 user lamp connection Processing System processing system and PLProgrammable Logic can
The coupling part of programmed logic, 3 user lamps are connected to PLProgrammable Logic programmable logic.
Further, EMMC flash uses MTFC64GAKAEYF-4M IT, memory space 64GB, EMMC Flash signal
Line is connected to the PS MIO pin of XAZU5EV-1SFVC784Q.
Further, 0.85V, 0.9V, 1.2V, 1.8V, 2.5V, 3.3V, 0.6V voltage are produced in the buckle, 1.8V,
2.5V, 3.3V can supply bottom plate by FX10A-168S-SV connector, and XAZU5EV-1SFVC784Q electrifying timing sequence is on veneer
0.85V, 0.9V, 1.8V, 1.2V, 1.8V_bank, 1.8V_bank be available to XAZU5EV-1SFVC784Q bank500 and
The voltage of bank502.
Further, the quantity of the DDR4 SDRAM is two, and a channel connects XAZU5EV-1SFVC784Q's
Processing System processing system, a channel meet the PLProgrammable in XAZU5EV-1SFVC784Q
Logic programmable logic, the DDR4 SDRAM use MT40A1G16KNR-075, and a DDR4 SDRAM is 16 data
Position, 2GB memory space, another DDR4 SDRAM is 64 data bit, 8GB memory space.
Further, the XAZU5EV-1SFVC784Q leads ends connection is for FPGA starting of oscillation, the single-ended crystalline substance of 33.33MHz
Vibration, FPGA bank64 connection 100MHz LVDS crystal oscillator, as PL DDR4 reference clock, FPGA PS GTR connection 100MHz
LVDS crystal oscillator, bank505 connection 27MHz difference crystal oscillator, USB2.0 PHY chip USB3320C connection 24MHz crystal oscillator, network core
Piece KSZ9031 connection 25MHz crystal oscillator.
Further, QSPI Flash uses MT25QU512ABB8E12-0SIT, capacity 512Mbit, QSPI Flash letter
The PS MIO pin and FX10A-168S-SV connector of number line connection XAZU5EV-1SFVC784Q.
Further, the quantity of 2.0 PHY chip of USB is 2, and two are all connected to PS, and USB PHY0 can match
It is set to host and is also configurable to equipment use, USB PHY1 can only be used as host, and 2.0 PHY chip of USB uses
USB3320C。
Further, the buckle is equipped with 2 10/100/1000Mbit network PHY chips, and 1 is connected to by RGMII
The part PS, 1 is connected to the part PL by RGMII.10/100/1000Mbit network PHY chip uses KSZ9031RNXIC.
The invention has the benefit that
1. versatility is extremely strong, unmanned plane can be used not only for, moreover it can be used to unmanned vehicle direction；2. this buckle size is small, it is applicable in very much
In the small situation of working space；3. this buckle is multiple functional, the demand in common work can satisfy completely；4. PS+PL pin
Distribution；5. the end PS DDR forms 8G by four particles and stores；6. scalability is good, stability is good.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the structural schematic diagram of FX10-168 connector of the present invention.
Specific embodiment
In order that the present invention can be more clearly and readily understood, following will be combined with the drawings in the embodiments of the present invention,
Technical scheme in the embodiment of the invention is clearly and completely described.
As shown in Figure 1, 2, a kind of unmanned aerial vehicle (UAV) control core buckle, comprising: the core of model XAZU5EV-1SFVC784Q
Heart processor, the XAZU5EV-1SFVC784Q I/O pin connection USB3.0, PCIe Gen3 × 4, PCIe 2 × 4,
USB2.0 PHYs, Gigabit Ethernet PHYs, high speed interface, LVDS I/O port, the XAZU5EV-
The I/O pin of 1SFVC784Q connects FX10-168 connector, and the FX10-168 connector connects 8 pairs of MGT differential signals, should
The configuration of core buckle veneer includes: the QSPI flash of EMMC flash of DDR4,64GB of 8GB+2GB, 512Mb, wherein
The EMMC flash of the QSPI flash and 64GB of 64MB are connected to the DDR4 of Processing System processing system
The buckle when specifically used, is buckled in bottom by the DDR4 SDRAM of SDRAM and PLProgrammable Logic programmable logic
On plate, the buckle input power 5-12V.
The XAZU5EV-1SFVC784Q QSPI flash can start out of plate, can also be from EMMC flash or outer
The starting of portion's SD card.The buckle has 6 user lamps, and two of them user lamp connects Processing System processing
System, 1 user lamp connection Processing System processing system and PLProgrammable Logic are programmable
The coupling part of logic, 3 user lamps are connected to PLProgrammable Logic programmable logic.EMMC flash is adopted
With MTFC64GAKAEYF-4M IT, memory space 64GB, EMMC Flash signal wire is connected to XAZU5EV-1SFVC784Q's
PS MIO pin.Produce 0.85V, 0.9V, 1.2V, 1.8V, 2.5V, 3.3V, 0.6V voltage in the buckle, 1.8V, 2.5V,
3.3V can supply bottom plate by FX10A-168S-SV connector, on veneer XAZU5EV-1SFVC784Q electrifying timing sequence be 0.85V,
0.9V, 1.8V, 1.2V, 1.8V_bank, 1.8V_bank are available to XAZU5EV-1SFVC784Q bank500 and bank502
Voltage.The quantity of the DDR4 SDRAM is two, and a channel meets the Processing in XAZU5EV-1SFVC784Q
System processing system, a channel connect to may be programmed in the PLProgrammable Logic of XAZU5EV-1SFVC784Q and patrol
Volume, it is 16 data bit, 2GB memory space that the DDR4 SDRAM, which uses MT40A1G16KNR-075, a DDR4 SDRAM,
Another DDR4 SDRAM is 64 data bit, 8GB memory space.The XAZU5EV-1SFVC784Q leads ends connection is used for
FPGA starting of oscillation, 33.33MHz single-end crystal oscillator, FPGA bank64 connection 100MHz LVDS crystal oscillator, as PL DDR4 reference when
Clock, FPGA PS GTR connection 100MHz LVDS crystal oscillator, bank505 connection 27MHz difference crystal oscillator, USB2.0 PHY chip
USB3320C connection 24MHz crystal oscillator, network chip KSZ9031 connection 25MHz crystal oscillator.QSPI Flash is used
MT25QU512ABB8E12-0SIT, capacity 512Mbit, QSPI Flash signal wire connect the PS of XAZU5EV-1SFVC784Q
MIO pin and FX10A-168S-SV connector.The quantity of 2.0 PHY chip of USB is 2, and two are all connected to PS,
USB PHY0 is configurable to host and is also configurable to equipment use, and USB PHY1 can only be used as host, USB 2.0
PHY chip uses USB3320C.The buckle is equipped with 2 10/100/1000Mbit network PHY chips, and 1 is connected by RGMII
It is connected to the part PS, 1 is connected to the part PL by RGMII.10/100/1000Mbit network PHY chip uses
KSZ9031RNXIC.After buckle, which is connected to bottom plate, to be powered on, crystal oscillator starting of oscillation, buckle is started to work.
The present invention is applied not only to unmanned plane, and unmanned vehicle can also be used, and is a general core control panel, and other clients can be with
Core board is designed without oneself, directly purchases general core board, and Service control program, each user are developed based on core board
Application scenarios are different, it is desirable that control application is also different, has general-purpose platform, unmanned plane, unmanned vehicle Related product client can
To save the project development time, it is absorbed in respective Service control software development
The above description is only a preferred embodiment of the patent of the present invention, is not intended to limit the invention patent, all in the present invention
Made any modifications, equivalent replacements, and improvements etc., should be included in the guarantor of the invention patent within the spirit and principle of patent
Within the scope of shield.
Claims (10)
1. a kind of unmanned aerial vehicle (UAV) control core buckle characterized by comprising the core of model XAZU5EV-1SFVC784Q
Processor, the XAZU5EV-1SFVC784Q I/O pin connection USB3.0, PCIe Gen3 × 4, PCIe 2 × 4,
USB2.0 PHYs, Gigabit Ethernet PHYs, high speed interface, LVDS I/O port, the XAZU5EV-
The I/O pin of 1SFVC784Q connects FX10-168 connector, and the FX10-168 connector connects 8 pairs of MGT differential signals, should
The configuration of core buckle veneer includes: the QSPI flash of EMMC flash of DDR4,64GB of 8GB+2GB, 512Mb, wherein
The EMMC flash of the QSPI flash and 64GB of 64MB are connected to the DDR4 of Processing System processing system
The buckle when specifically used, is buckled in bottom by the DDR4 SDRAM of SDRAM and PLProgrammable Logic programmable logic
On plate, the buckle input power 5-12V.
2. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: the XAZU5EV-
1SFVC784Q QSPI flash can start out of plate, can also be from EMMC flash or external SD card starting.
3. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: the buckle has 6 users
Indicator light, two of them user lamp connect Processing System processing system, 1 user lamp connection
The coupling part of Processing System processing system and PLProgrammable Logic programmable logic, 3 users
Indicator light is connected to PLProgrammable Logic programmable logic.
4. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: EMMC flash is used
MTFC64GAKAEYF-4M IT, memory space 64GB, EMMC Flash signal wire are connected to the PS of XAZU5EV-1SFVC784Q
MIO pin.
5. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: produced in the buckle
0.85V, 0.9V, 1.2V, 1.8V, 2.5V, 3.3V, 0.6V voltage, 1.8V, 2.5V, 3.3V can be connected by FX10A-168S-SV
Device supply bottom plate is connect, XAZU5EV-1SFVC784Q electrifying timing sequence is 0.85V, 0.9V, 1.8V, 1.2V, 1.8V_bank on veneer,
1.8V_bank is available to the voltage of XAZU5EV-1SFVC784Q bank500 and bank502.
6. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: the DDR4 SDRAM's
Quantity is two, and a channel connects the Processing System processing system in XAZU5EV-1SFVC784Q, a channel
The PLProgrammable Logic programmable logic in XAZU5EV-1SFVC784Q is connect, the DDR4 SDRAM is used
MT40A1G16KNR-075, a DDR4 SDRAM are 16 data bit, 2GB memory space, another DDR4 SDRAM is 64
Position data bit, 8GB memory space.
7. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: the XAZU5EV-
The connection of 1SFVC784Q leads ends is for FPGA starting of oscillation, the single-end crystal oscillator of 33.33MHz, FPGA bank64 connection 100MHz LVDS
Crystal oscillator, as PL DDR4 reference clock, FPGA PS GTR connection 100MHz LVDS crystal oscillator, bank505 connection 27MHz difference
Crystal oscillator, USB2.0 PHY chip USB3320C connection 24MHz crystal oscillator, network chip KSZ9031 connection 25MHz crystal oscillator.
8. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: QSPI Flash is used
MT25QU512ABB8E12-0SIT, capacity 512Mbit, QSPI Flash signal wire connect the PS of XAZU5EV-1SFVC784Q
MIO pin and FX10A-168S-SV connector.
9. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: 2.0 PHY of USB
The quantity of chip is 2, and two are all connected to PS, and USB PHY0 is configurable to host and is also configurable to equipment use,
USB PHY1 can only be used as host, and 2.0 PHY chip of USB uses USB3320C.
10. a kind of unmanned aerial vehicle (UAV) control core buckle according to claim 1, it is characterised in that: the buckle is equipped with 2
10/100/1000Mbit network PHY chip, 1 is connected to the part PS by RGMII, and 1 is connected to the portion PL by RGMII
Point, 10/100/1000Mbit network PHY chip adopts KSZ9031RNXIC.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910304904.6A CN110069030A (en) | 2019-04-16 | 2019-04-16 | A kind of unmanned aerial vehicle (UAV) control core buckle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910304904.6A CN110069030A (en) | 2019-04-16 | 2019-04-16 | A kind of unmanned aerial vehicle (UAV) control core buckle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110069030A true CN110069030A (en) | 2019-07-30 |
Family
ID=67367843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910304904.6A Pending CN110069030A (en) | 2019-04-16 | 2019-04-16 | A kind of unmanned aerial vehicle (UAV) control core buckle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110069030A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113093781A (en) * | 2021-04-12 | 2021-07-09 | 广东汇天航空航天科技有限公司 | Manned aircraft, data interface module and transmission method of flight control data |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103870429A (en) * | 2014-04-03 | 2014-06-18 | 清华大学 | High-speed-signal processing board based on embedded GPU |
| CN107064960A (en) * | 2017-03-28 | 2017-08-18 | 上海双微导航技术有限公司 | A kind of GNSS satellite receiver baseband hardware platform circuit structure based on SOC frameworks |
| CN107797816A (en) * | 2017-09-15 | 2018-03-13 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | FPGA program online updating circuits |
| CN207503227U (en) * | 2017-11-17 | 2018-06-15 | 深圳市中达瑞和科技有限公司 | A kind of core board based on embedded system |
| CN207869146U (en) * | 2018-03-05 | 2018-09-14 | 西安彼睿电子科技有限公司 | A kind of FPGA reconfigurable networks processing board |
| CN208401881U (en) * | 2018-07-02 | 2019-01-18 | 成都吉纬科技有限公司 | A kind of base band control system |
| CN109491949A (en) * | 2018-11-27 | 2019-03-19 | 哈尔滨工业大学 | Dynamic reconfigurable frame and method based on Zynq |
-
2019
- 2019-04-16 CN CN201910304904.6A patent/CN110069030A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103870429A (en) * | 2014-04-03 | 2014-06-18 | 清华大学 | High-speed-signal processing board based on embedded GPU |
| CN107064960A (en) * | 2017-03-28 | 2017-08-18 | 上海双微导航技术有限公司 | A kind of GNSS satellite receiver baseband hardware platform circuit structure based on SOC frameworks |
| CN107797816A (en) * | 2017-09-15 | 2018-03-13 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | FPGA program online updating circuits |
| CN207503227U (en) * | 2017-11-17 | 2018-06-15 | 深圳市中达瑞和科技有限公司 | A kind of core board based on embedded system |
| CN207869146U (en) * | 2018-03-05 | 2018-09-14 | 西安彼睿电子科技有限公司 | A kind of FPGA reconfigurable networks processing board |
| CN208401881U (en) * | 2018-07-02 | 2019-01-18 | 成都吉纬科技有限公司 | A kind of base band control system |
| CN109491949A (en) * | 2018-11-27 | 2019-03-19 | 哈尔滨工业大学 | Dynamic reconfigurable frame and method based on Zynq |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113093781A (en) * | 2021-04-12 | 2021-07-09 | 广东汇天航空航天科技有限公司 | Manned aircraft, data interface module and transmission method of flight control data |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE112013007744B3 (en) | DEVICE, SYSTEM AND METHOD FOR PROVIDING WIRELESS COMMUNICATION BETWEEN DEVICES | |
| EP2587385B1 (en) | Usb key device and method for realizing intelligent card communication using usb interface | |
| US20190146806A1 (en) | Method and apparatus for plug and play, networkable iso 18000-7 connectivity | |
| US20070288671A1 (en) | Low power and low pin count bi-directional dual data rate device interconnect interface | |
| CN106878613B (en) | Data communication device and method and unmanned aerial vehicle | |
| CN110069030A (en) | A kind of unmanned aerial vehicle (UAV) control core buckle | |
| CN208963014U (en) | The fusing device of multichannel sensing data | |
| CN109240960B (en) | Exchange board circuit based on VPX architecture and implementation method thereof | |
| CN111198704A (en) | FPGA remote upgrading system based on TCP protocol | |
| CN109358995A (en) | A kind of multifunctional testing backboard and test method | |
| WO2016197883A1 (en) | Method and system for updating program of microcontroller online | |
| CN106059599A (en) | S-band receiving-transmitting integrated processor system | |
| CN102314405A (en) | CCID (USB (universal serial bus) chip/smart card interface devices) protocol processing circuit | |
| CN106649179B (en) | A kind of device exporting Serial Port Information and switching part and a kind of electronic equipment | |
| CN212515401U (en) | Rocket-borne full-redundancy comprehensive electronic system | |
| CN214311726U (en) | A adapter plate for prototype is verified | |
| US20150039797A1 (en) | Removable expansion interface device | |
| CN210572737U (en) | Secondary radar signal processing device | |
| CN105740192A (en) | PS2 interface keyboard/mouse hot plug system and realization method thereof | |
| CN107247677B (en) | Conversion device and electronic equipment | |
| CN217721604U (en) | Expandable function verification development daughter board | |
| CN205793087U (en) | Video and network function development board | |
| CN220188924U (en) | Server based on Feiteng platform | |
| CN213211018U (en) | Signal processing board card | |
| CN219552900U (en) | BMC card and computer 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 | ||
| CB03 | Change of inventor or designer information |
Inventor after: Pan Bin Inventor before: Pan Bin Inventor before: Zhou Jing |
|
| CB03 | Change of inventor or designer information | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190730 |
|
| RJ01 | Rejection of invention patent application after publication |