CN206515648U - Detachable unmanned aerial vehicle (UAV) control device - Google Patents
Detachable unmanned aerial vehicle (UAV) control device Download PDFInfo
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- CN206515648U CN206515648U CN201621360909.9U CN201621360909U CN206515648U CN 206515648 U CN206515648 U CN 206515648U CN 201621360909 U CN201621360909 U CN 201621360909U CN 206515648 U CN206515648 U CN 206515648U
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Abstract
The utility model belongs to unmanned aerial vehicle control system technical field, the detachable unmanned aerial vehicle (UAV) control device proposed, the control panel on mainboard is detachably arranged at including mainboard and by PIN interfaces, mainboard controller is provided with mainboard, flight controller is provided with control panel, flight controller is connected by PIN interfaces with drive device plug-in unit, flight controller is all connected with flight control crystal oscillator and receiver, mainboard controller and gyro sensor, accelerometer chip, baroceptor, six axle gyroscopes and mainboard control crystal oscillator are all connected with, also include being connected with PIN interfaces and being detachably arranged at the satellite positioning module on mainboard, communication module, Pulse width modulation module, mainboard controller is respectively connected with CAN communication converter with flight controller.The utility model is skillfully constructed, and solves integral replacing control mainboard in the prior art, and maintenance cost is higher, and easily causes the technical problem that electronic component wastes and causes unnecessary environmental pollution.
Description
Technical field
The utility model belongs to unmanned aerial vehicle control system technical field, is related to a kind of detachable unmanned aerial vehicle (UAV) control device.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..At present taking photo by plane, agricultural, plant protection, oneself
Bat, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, video display
The application in the fields such as romance is shot, manufactured, the purposes of unmanned plane in itself has greatly been expanded, developed country is also in positive extension row
Industry is applied and development unmanned air vehicle technique.But the controller rapid wear in current unmanned aerial vehicle (UAV) control mainboard, is difficult maintenance after damage, must
Must be by control mainboard integral replacing, maintenance cost is higher, and easily causes other unspoiled electronic components wastes and cause not
Necessary environmental pollution.
Utility model content
The utility model proposes a kind of detachable unmanned aerial vehicle (UAV) control device, integral replacing control master in the prior art is solved
Plate, maintenance cost is higher, and easily causes the technical problem that electronic component wastes and causes unnecessary environmental pollution.
What the technical solution of the utility model was realized in：
Detachable unmanned aerial vehicle (UAV) control device, including mainboard and the control on the mainboard is detachably arranged at by PIN interfaces
It is provided with mainboard controller, the mainboard controller and power module connection, the control panel and is provided with plate, the mainboard
Flight controller, the flight controller is connected by the PIN interfaces with drive device plug-in unit,
The flight controller is all connected with flight control crystal oscillator and receiver,
The mainboard controller and gyro sensor, accelerometer chip, baroceptor, six axle gyroscopes and mainboard
Control crystal oscillator is all connected with,
Also include satellite positioning module, the communication for being connected and being detachably arranged on the mainboard with the PIN interfaces
Module, Pulse width modulation module,
The mainboard controller is respectively connected with CAN communication converter with the flight controller.
As further technical scheme, in addition to equal it be connected with the PIN interfaces and be detachably arranged at the mainboard
On USB interface and I2C communication modules.
As further technical scheme, in addition to LED light, the LED light includes controlling with the mainboard
The redgreenblue lamp of device connection, and two monochromes being connected respectively with the mainboard controller and the flight controller
Lamp.
As further technical scheme, the redgreenblue lamp is connected by I2C communications with the mainboard controller.
As further technical scheme, in addition to answering that the mainboard controller and the flight controller are all connected with
Position module and emulator.
As further technical scheme, the mainboard controller is also connected with programmable read only memory and SD card.
It is used as further technical scheme, the gyro sensor, the accelerometer chip, the baroceptor
It is connected with the six axles gyroscope by SPI communication with the mainboard controller.
As further technical scheme, the PIN interfaces are NGFF interfaces.
It is used as further technical scheme, the mainboard controller model STM32F427IIH6, the flight controller
Model STM32F103CBU6, the gyro sensor model L3GD20, the accelerometer chip model
LSM303D, the baroceptor model MS5611, the six axles gyroscope model MPU6000.
The utility model use principle and have the beneficial effect that：
1st, the utility model changes current unmanned aerial vehicle (UAV) control device and the natural mode of mainboard integrated setting, innovative
The critical piece control panel of rapid wear in unmanned aerial vehicle (UAV) control device is separated from mainboard, both are carried out into plug-in type detachably sets
Put so that after control panel is damaged, only this part is removed and changed, without changing whole mainboard, use is effectively saved
The maintenance cost at family, it is to avoid other wastes for not damaging electronic component, effectively reduces unnecessary environmental pollution, and behaviour
Make easy, user is just operable without too high circuit design knowledge, carried out without professional person, effectively increase unmanned plane control
The maintenance speed of system processed, is set scientific and reasonable.
Wherein, receiver and flight controller are arranged on control panel so that remote control sends signal and can received
Machine is quickly reached in flight controller after receiving, it is ensured that flight controller controls unmanned plane action according to remote signal in time, this
One sets the agility that effectively ensure that no-manned machine distant control control, meets its use demand.Meanwhile, the utility model is passed all
Induction device (gyro sensor, accelerometer chip, baroceptor, six axle gyroscopes etc.) is arranged on mainboard, by it
It is connected with mainboard controller, the workload of flight controller has effectively been shared in this setting, reduces control panel and occur what is damaged
Probability, also ensures stability during unmanned plane operation.In addition, the utility model is also provided with satellite positioning module so that nothing
It is man-machine operationally to monitor the positional information of itself in real time and be accurate to the temporal information of nanosecond, it effectively ensure that unmanned plane
Security, automation and the intellectuality of operation.
2nd, redgreenblue lamp is connected by the utility model by I2C communications with mainboard controller, it is ensured that indicator lamp is accounted for
Resource is less, only uses 2 lines, meets the tighter use requirement of unmanned aerial vehicle control system I/O port resource.
The setting of programmable read only memory is easy to user that program is wiped or write as needed, and number after power down
According to that will not lose, meet the use demand of user.The setting of SD card is then easy to user to being stored or being copied using data.
Various sensing devices are connected by SPI communication with mainboard controller, each transducing signal and mainboard has been effectively ensured
High speed between controller is propagated, and meets equipment service requirement.
Brief description of the drawings
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Fig. 1 is the utility model structural representation；
Fig. 2 is the utility model control structure wire schematic diagram；
Fig. 3 is the circuit theory diagrams of flight controller in the utility model；
Fig. 4 is the circuit theory diagrams of mainboard controller in the utility model；
Fig. 5 is the circuit theory diagrams of power module in the utility model；
Fig. 6 is the circuit theory diagrams of flight control crystal oscillator in the utility model；
Fig. 7 is the circuit theory diagrams of receiver in the utility model；
Fig. 8 is the circuit theory diagrams of gyro sensor in the utility model；
Fig. 9 is the circuit theory diagrams of accelerometer chip in the utility model；
Figure 10 is the circuit theory diagrams of baroceptor in the utility model；
Figure 11 is the circuit theory diagrams of six axle gyroscopes in the utility model；
Figure 12 is the circuit theory diagrams of mainboard control crystal oscillator in the utility model；
Figure 13 is the circuit theory diagrams of PIN interfaces in the utility model；
Figure 14 is the circuit theory diagrams of SD card in the utility model；
Figure 15 is the circuit theory diagrams of USB interface in the utility model；
Figure 16 is the circuit theory diagrams of redgreenblue lamp in the utility model；
Figure 17 is the circuit theory diagrams of monochromatic burner in the utility model；
Figure 18 is the circuit theory diagrams of reseting module in the utility model；
Figure 19 is the circuit theory diagrams of programmable read only memory in the utility model；
In figure：1- mainboards, 2- control panels, 3- mainboard controllers, 4- flight controllers, 5- flight control crystal oscillators, 6- is received
Machine, 7- gyro sensors, 8- accelerometer chips, 9- baroceptors, the axle gyroscopes of 10- six, 11- mainboards control crystal oscillator,
12-PIN interfaces, 13- satellite positioning modules, 14- communication modules, 15-CAN communication converters, 16-USB interfaces, 17- pulses are wide
Spend modulation module, 18-LED indicator lamps, 181- redgreenblue lamps, 182- monochromatic burners, 19- reseting modules, 20- emulators, 21-
Programmable read only memory, 22-SD cards, 23- power modules, 24- drive device plug-in units, 25-I2C communication modules.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
As shown in Fig. 1~19, the utility model proposes detachable unmanned aerial vehicle (UAV) control device, including mainboard 1 and connect by PIN
Mouth 12 is detachably arranged on the control panel 2 on mainboard 1, mainboard 1 and is provided with mainboard controller 3, mainboard controller 3 and power supply mould
Block 23 is connected, and flight controller 4 is provided with control panel 2, and flight controller 4 passes through PIN interfaces 12 and drive device plug-in unit 24
Connection,
Flight controller 4 is all connected with flight control crystal oscillator 5 and receiver 6,
Mainboard controller 3 and gyro sensor 7, accelerometer chip 8, baroceptor 9, six axle gyroscopes 10 and master
Plate control crystal oscillator 11 is all connected with,
Also include being connected with PIN interfaces 12 and being detachably arranged at the satellite positioning module 13 on mainboard 1, communication module
14th, Pulse width modulation module 17,
Mainboard controller 3 is respectively connected with CAN communication converter 15 with flight controller 4.
The utility model changes the natural mode of current unmanned aerial vehicle (UAV) control device and mainboard integrated setting, innovative general
The critical piece control panel 2 of rapid wear is separated from mainboard 1 in unmanned aerial vehicle (UAV) control device, and both are carried out into plug-in type detachably sets
Put so that after control panel 2 is damaged, only this part is removed and changed, without changing whole mainboard 1, is effectively saved
The maintenance cost of user, it is to avoid other wastes for not damaging electronic component, effectively reduces unnecessary environmental pollution, and
Easy to operate, user is just operable without too high circuit design knowledge, is carried out without professional person, effectively increases unmanned plane
The maintenance speed of control system, is set scientific and reasonable.
Wherein, receiver 6 and flight controller 4 are arranged on control panel 2 so that remote control sends signal and can connect
Receipts machine 6 is quickly reached in flight controller 4 after receiving, it is ensured that flight controller 4 controls nobody motor-driven according to remote signal in time
Make, this setting effectively ensure that the agility of no-manned machine distant control control, meet its use demand.Meanwhile, the utility model will
All sensing devices (gyro sensor 7, accelerometer chip 8, baroceptor 9, six axle gyroscopes 10 etc.) are arranged at
On mainboard 1, it is connected with mainboard controller 3, the workload of flight controller 2 has effectively been shared in this setting, reduces control
There is the probability damaged in making sheet 2, also ensures stability during unmanned plane operation.In addition, the utility model is also provided with satellite
Locating module 13 so that unmanned plane can operationally monitor the positional information of itself in real time and be accurate to the time letter of nanosecond
Breath, effectively ensure that security, automation and the intellectuality of unmanned plane operation.
Further, in addition to it is connected with PIN interfaces 12 and is detachably arranged at the usb 16 on mainboard 1 and I2C is logical
Believe module 25.
The setting of usb 16 effectively ensure that the convenience that user uses, and meet the use habit of user.
Further, in addition to LED light 18, LED light 18 includes the redgreenblue being connected with mainboard controller 3
Lamp 181, and two monochromatic burners 182 being connected respectively with mainboard controller 3 and flight controller 4.
Further, redgreenblue lamp 181 is connected by I2C communications with mainboard controller 3.
Redgreenblue lamp 181 is connected by I2C communications with mainboard controller 3, it is ensured that the resource that indicator lamp takes
It is less, 2 lines are only used, meet the tighter use requirement of unmanned aerial vehicle control system I/O port resource.
Further, in addition to mainboard controller 3 and flight controller 4 reseting module 19 and emulator 20 being all connected with.
Further, mainboard controller 3 is also connected with programmable read only memory 21 and SD card 22.
The setting of programmable read only memory 21 is easy to user that program is wiped or write as needed, and after power down
Data will not lose, and meet the use demand of user.The setting of SD card 22 is then easy to user to being stored or being copied using data
Shellfish.
Further, gyro sensor 7, accelerometer chip 8, the axle gyroscope 10 of baroceptor 9 and six pass through SPI
Communication is connected with mainboard controller 3.
Various sensing devices are connected by SPI communication with mainboard controller 3, each transducing signal and mainboard has been effectively ensured
High speed between controller 3 is propagated, and meets equipment service requirement.
Further, the PIN interfaces 12 are NGFF interfaces.
NGFF interfaces further reduce with respect to volume for mSATA, more save space.Compared to SATA3 interfaces and mini
PCI-e interfaces, NGFF interfaces transmit data using 4xPCI-e Gen3, and speed is greatly improved, and mainboard 1 and control has been effectively ensured
Data transmission bauds between making sheet 2, meets unmanned plane use demand.
Further, the model STM32F427IIH6 of mainboard controller 3, the model STM32F103CBU6 of flight controller 4,
The model L3GD20 of gyro sensor 7, the model LSM303D of accelerometer chip 8, the model MS5611 of baroceptor 9,
The model MPU6000 of six axle gyroscope 10.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc. should be included in the utility model
Protection domain within.
Claims (9)
1. detachable unmanned aerial vehicle (UAV) control device, it is characterised in that be detachably arranged at including mainboard (1) and by PIN interfaces (12)
Be provided with mainboard controller (3) on control panel (2) on the mainboard (1), the mainboard (1), the mainboard controller (3) and
Power module (23) is connected, and is provided with flight controller (4) on the control panel (2), the flight controller (4) is by described
PIN interfaces (12) are connected with drive device plug-in unit (24),
The flight controller (4) is all connected with flight control crystal oscillator (5) and receiver (6),
The mainboard controller (3) and gyro sensor (7), accelerometer chip (8), baroceptor (9), six axle gyros
Instrument (10) and mainboard control crystal oscillator (11) are all connected with,
Also include the satellite positioning module for being connected and being detachably arranged on the mainboard (1) with the PIN interfaces (12)
(13), communication module (14) and Pulse width modulation module (17),
The mainboard controller (3) is respectively connected with CAN communication converter (15) with the flight controller (4).
2. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that also including the equal and PIN interfaces
(12) USB interface (16) and I2C communication modules (25) for connecting and being detachably arranged on the mainboard (1).
3. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that also including LED light (18), institute
Stating LED light (18) includes the redgreenblue lamp (181) that is connected with the mainboard controller (3), and with the mainboard
Two monochromatic burners (182) that controller (3) and the flight controller (4) are connected respectively.
4. detachable unmanned aerial vehicle (UAV) control device according to claim 3, it is characterised in that the redgreenblue lamp (181)
It is connected by I2C communications with the mainboard controller (3).
5. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that also including with the mainboard controller
And the flight controller (4) reseting module (19) and emulator (20) that are all connected with (3).
6. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that the mainboard controller (3) also with
Programmable read only memory (21) and SD card (22) are all connected with.
7. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that the gyro sensor (7), institute
Accelerometer chip (8), the baroceptor (9) and the six axles gyroscope (10) are stated by SPI communication and the master
Plate controller (3) is connected.
8. detachable unmanned aerial vehicle (UAV) control device according to claim 1, it is characterised in that the PIN interfaces (12) are NGFF
Interface.
9. the detachable unmanned aerial vehicle (UAV) control device according to any one of claim 1~8, it is characterised in that the mainboard control
Device (3) model STM32F427IIH6, flight controller (4) the model STM32F103CBU6, the gyro sensors
Device (7) model L3GD20, accelerometer chip (8) the model LSM303D, baroceptor (9) model
MS5611, six axles gyroscope (10) the model MPU6000.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621360909.9U CN206515648U (en) | 2016-12-13 | 2016-12-13 | Detachable unmanned aerial vehicle (UAV) control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621360909.9U CN206515648U (en) | 2016-12-13 | 2016-12-13 | Detachable unmanned aerial vehicle (UAV) control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206515648U true CN206515648U (en) | 2017-09-22 |
Family
ID=59862511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621360909.9U Active CN206515648U (en) | 2016-12-13 | 2016-12-13 | Detachable unmanned aerial vehicle (UAV) control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206515648U (en) |
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2016
- 2016-12-13 CN CN201621360909.9U patent/CN206515648U/en active Active
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