CN206039189U - Control system takes photo by plane based on AVR singlechip - Google Patents
Control system takes photo by plane based on AVR singlechip Download PDFInfo
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- CN206039189U CN206039189U CN201620761266.2U CN201620761266U CN206039189U CN 206039189 U CN206039189 U CN 206039189U CN 201620761266 U CN201620761266 U CN 201620761266U CN 206039189 U CN206039189 U CN 206039189U
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Abstract
The utility model relates to a control system, more specifically say, relate to control system takes photo by plane based on AVR singlechip. Control system includes camera, compass detection circuitry, reducing motor, drive circuit, button module, singlechip, power supply circuit, reset circuit, clock circuit and LCD display module, and the input of singlechip is being connected to the output of camera, the input of singlechip is being connected to compass detection circuitry's output, drive circuit's input is being connected to the output of singlechip, reducing motor's input is being connected to drive circuit's output, the input of singlechip is being connected to the output of button module, the input of singlechip is being connected to power supply circuit's output, the input of LCD display module is being connected to the output of singlechip. The utility model discloses control system takes photo by plane based on AVR singlechip, it is accurate that it is controlled, can detect the angle of aircraft, and operation according to the different control motors of angle realizes the aircraft smooth flight, can also realize regularly shooing.
Description
Technical field
The utility model relates generally to navigation system, more particularly, it relates to the control system that takes photo by plane based on AVR single chip
System.
Background technology
With developing rapidly for society, requirement more and more higher of the people to picture, figure of taking photo by plane is with than virtual three-dimensional effect
Figure is truer, more specifically effect.But the technology of taking photo by plane is just gradually to enter into our life in recent years, development is not especially complete
It is kind.And the technical difficulty of aerial photography aircraft design is big, there are problems that aircraft revolves inclined, image pixel problem etc., not easy to operate, later stage
Process complicated.In order to preferably realize the control taken photo by plane, the research of control system is particularly important.How to allow and work out one efficiently
Control system be very with significance research direction.
The content of the invention
Utility model is mainly solving the technical problems that provide the control system of taking photo by plane based on AVR single chip, its control is accurate
Really, the angle of aircraft can be detected, according to the operatings of the different control motor of angle, aircraft smooth flight is realized, can be with
Realize BR.
For solving above-mentioned technical problem, the utility model includes camera, compass based on the control system of taking photo by plane of AVR single chip
Detection circuit, decelerator, drive circuit, key-press module, single-chip microcomputer, power circuit, reset circuit, clock circuit and LCD
Display module, its precise control can detect the angle of aircraft, according to the operating of the different control motor of angle, realize flying
Machine smooth flight, can also realize BR.
Wherein, the output end of the camera is connected to the input of single-chip microcomputer；The output end of the compass detection circuit connects
Then the input of single-chip microcomputer；The output end of the single-chip microcomputer is connected to the input of drive circuit；The drive circuit it is defeated
Go out the input that end is connected to decelerator；The output end of the key-press module is connected to the input of single-chip microcomputer；The electricity
The output end of source circuit is connected to the input of single-chip microcomputer；The output end of the reset circuit is connected to the input of single-chip microcomputer；
The output end of the clock circuit is connected to the input of single-chip microcomputer；The output end of the single-chip microcomputer is connected to LCD display module
Input.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
Single-chip microcomputer adopts AT mega16 single-chip microcomputers.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
Compass detection circuit adopts WY211S-JQR flat digital compass.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
Key-press module adopts matrix keyboard.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
LCD display module adopts LCD3501 displays.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
Drive circuit adopts L298 driving chips.
Further optimize as of the present utility model, the utility model taking photo by plane described in control system based on AVR single chip
Reset circuit adopts electrification reset circuit.
Control effect：Take photo by plane control system of the utility model based on AVR single chip, its precise control can be detected winged
The angle of machine, according to the operating of the different control motor of angle, realizes aircraft smooth flight, can also realize BR.
Description of the drawings
The utility model is described in more detail with specific implementation method below in conjunction with the accompanying drawings.
Fig. 1 is take photo by plane control system hardware structure diagram of the utility model based on AVR single chip.
Fig. 2 is take photo by plane control system driver circuit schematic diagram of the utility model based on AVR single chip.
Fig. 3 is take photo by plane control system LCD display module schematic diagram of the utility model based on AVR single chip.
Fig. 4 is take photo by plane control system key-press module schematic diagram of the utility model based on AVR single chip.
Fig. 5 is take photo by plane control system clock circuit schematic diagram of the utility model based on AVR single chip.
Fig. 6 is take photo by plane control system reset circuit schematic diagram of the utility model based on AVR single chip.
Specific embodiment
Specific embodiment one：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the control of taking photo by plane described in present embodiment based on AVR single chip
System includes camera, compass detection circuit, decelerator, drive circuit, key-press module, single-chip microcomputer, power circuit, reset electricity
Road, clock circuit and LCD display module, its precise control can detect the angle of aircraft, be controlled according to the difference of angle electronic
The operating of machine, realizes aircraft smooth flight, can also realize BR.
Wherein, the output end of the camera is connected to the input of single-chip microcomputer, and camera is used for shooting image, realizes taking photo by plane.
The output end of the compass detection circuit is connected to the input of single-chip microcomputer, and it is inclined that compass detection circuit is used for aircraft rotation
The detection of angle.
The output end of the single-chip microcomputer is connected to the input of drive circuit, and single-chip microcomputer is used for controlling motor rotation and phase
Machine shoots.
The output end of the drive circuit is connected to the input of decelerator, and drive circuit is used for driving deceleration electric
Machine works.
The output end of the key-press module is connected to the input of single-chip microcomputer, and key-press module is used for adjusting rotation and hand manually
Dynamic regulating time.
The output end of the power circuit is connected to the input of single-chip microcomputer, and power circuit is for powering to single-chip microcomputer.
The output end of the reset circuit is connected to the input of single-chip microcomputer, and reset circuit is used for making single-chip microcomputer return to just
Beginning state.
The output end of the clock circuit is connected to the input of single-chip microcomputer, and clock circuit provides system for giving single-chip microcomputer
Time.
The output end of the single-chip microcomputer is connected to the input of LCD display module, and LCD display module is used for showing camera
Rotation inclination angle and BR time.
Specific embodiment two：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the single-chip microcomputer adopts AT mega16 single-chip microcomputers, AT
Mega16 is the 8 CMOS microcontrollers of low-power consumption based on enhanced AVR risc architectures.Due to its advanced instruction set and
Single clock cycle time for each instruction, the data throughput of AT mega16 are up to 1MIPS/MHz.
Specific embodiment three：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the compass detection circuit adopts WY211S-JQR number of planes
Word compass, its operation principle are the magnetic components for sensing magnetic field of the earth by magnetoresistive transducer, so as to draw orientation angles.Sieve
Disk sends data in RS232 level mode to host computer.The Product Precision is high, stable.
Specific embodiment four：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the key-press module adopts matrix keyboard, matrix keyboard
With multiple buttons, it is possible to achieve various control function.
Specific embodiment five：
With reference to Fig. 1,2,3,4,5,6 illustrate present embodiment, the LCD display module adopt LCD3501 displays, make be
System is with " man-machine " dialogue function, it is easy to accomplish online programming is controlled, with highly versatile, the features such as cost performance is high.
Specific embodiment six：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the drive circuit adopts L298 driving chips, and L298 is one
The single chip integrated high voltage of money, high current, two-way full-bridge type Motor drive, are designed for connection standard TTL logic levels, drive
Inductive load (such as relay, coil, DC and stepper motor).L298 provides two enable inputs, can not rely on
In the case of input signal, enabled or disabled L298 devices.
Specific embodiment seven：
Present embodiment is illustrated with reference to Fig. 1,2,3,4,5,6, the reset circuit adopts electrification reset circuit, during energization,
Electric capacity two ends are the equal of short circuit, are then high level on RST pins, and then power supply is charged to electric capacity by resistance, RST ends electricity
Pressure slowly declines, and drops to a certain degree, as low level, and single-chip microcomputer starts normal work.
Operation principle：Compass detection circuit is used for detecting aircraft rotation inclination angle, when the value for detecting is more than preset value, changes
Corresponding interface microcontroller, drives decelerator to rotate forward by drive circuit, when the value for detecting is less than preset value, changes phase
The interface microcontroller answered, drives decelerator reversion by drive circuit.Key-press module can manually adjust motor just,
Reversion, conveniently adjusts and prevents motor stuck.After power circuit is powered to single-chip microcomputer, LCD display module shows Current camera
Rotation inclination angle and the BR time.Reset circuit is used for making single-chip microcomputer return to original state.Clock circuit is used for providing
System time is to single-chip microcomputer.When aircraft occurs to revolve inclined, control system can be automatically adjusted, and allow camera to remain that positive direction is clapped
Take the photograph.
Although the utility model is disclosed as above with preferred embodiment, which is not limited to the utility model, appoints
What person skilled in the art, in without departing from spirit and scope of the present utility model, can do various changes and modification, therefore
Protection domain of the present utility model should be by being defined that claims are defined.
Claims (7)
1. the control system of taking photo by plane based on AVR single chip, it is characterised in that the control system of taking photo by plane based on AVR single chip
Including camera, compass detection circuit, decelerator, drive circuit, key-press module, single-chip microcomputer, power circuit, reset circuit,
Clock circuit and LCD display module, the output end of the camera are connected to the input of single-chip microcomputer；The compass detection circuit
Output end is connected to the input of single-chip microcomputer；The output end of the single-chip microcomputer is connected to the input of drive circuit；The driving
The output end of circuit is connected to the input of decelerator；The output end of the key-press module is connected to the input of single-chip microcomputer
End；The output end of the power circuit is connected to the input of single-chip microcomputer；The output end of the reset circuit is connected to single-chip microcomputer
Input；The output end of the clock circuit is connected to the input of single-chip microcomputer；The output end of the single-chip microcomputer is connected to LCD
The input of display module.
2. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The single-chip microcomputer is adopted
With AT mega16 single-chip microcomputers.
3. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The compass detection
Circuit adopts WY211S-JQR flat digital compass.
4. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The key-press module
Using matrix keyboard.
5. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The LCD shows mould
Block adopts LCD3501 displays.
6. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The drive circuit
Using L298 driving chips.
7. the control system of taking photo by plane based on AVR single chip according to claim 1, it is characterised in that：The reset circuit
Using electrification reset circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620761266.2U CN206039189U (en) | 2016-07-19 | 2016-07-19 | Control system takes photo by plane based on AVR singlechip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620761266.2U CN206039189U (en) | 2016-07-19 | 2016-07-19 | Control system takes photo by plane based on AVR singlechip |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206039189U true CN206039189U (en) | 2017-03-22 |
Family
ID=58311535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620761266.2U Expired - Fee Related CN206039189U (en) | 2016-07-19 | 2016-07-19 | Control system takes photo by plane based on AVR singlechip |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206039189U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109597430A (en) * | 2019-01-18 | 2019-04-09 | 东北农业大学 | The UAV system of dimension analysis is risen based on photo |
-
2016
- 2016-07-19 CN CN201620761266.2U patent/CN206039189U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109597430A (en) * | 2019-01-18 | 2019-04-09 | 东北农业大学 | The UAV system of dimension analysis is risen based on photo |
| CN109597430B (en) * | 2019-01-18 | 2023-04-18 | 东北农业大学 | Unmanned aerial vehicle system based on photo dimension-rising analysis |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170322 Termination date: 20170719 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |