CN202609092U - Single-propeller three-axis flight shooting system - Google Patents
Single-propeller three-axis flight shooting system Download PDFInfo
- Publication number
- CN202609092U CN202609092U CN 201220185910 CN201220185910U CN202609092U CN 202609092 U CN202609092 U CN 202609092U CN 201220185910 CN201220185910 CN 201220185910 CN 201220185910 U CN201220185910 U CN 201220185910U CN 202609092 U CN202609092 U CN 202609092U
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- CN
- China
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- camera
- shooting
- control desk
- propeller
- triangle body
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- Expired - Fee Related
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- Studio Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model relates to a video transmission system and particularly to a single-propeller three-axis flight shooting system. The technical scheme includes that the system comprises a foldable triangular machine body, an aeromodelling lithium battery, a driving electronic controller, a control panel, a three-axis gyroscope, a camera, and protection covers, wherein the driving electronic controller is installed on the lower portion of the foldable triangular machine body, the control panel is connected with the lower portion of the driving electronic controller, the camera and the three-axis gyroscope are installed on the control panel, a protection cover is arranged on the periphery of each of propellers, and the aeromodelling lithium battery is fixed in the foldable triangular machine body. The single-propeller three-axis flight shooting system has the advantages that under the conditions of high-altitude shooting, water surface shooting and the like, remote real-time monitoring and shooting can be achieved, the system is provided with a power supply, the endurance time reaches 50 minutes, and the environment and a site can not be affected.
Description
Technical field
The utility model relates to a kind of Video transmission system, three flight of particularly a kind of fly able single-blade camera system.
Background technology
At present; In carrying out the video capture process; In some cases because the problem of photographer's angle did not photograph some crucial camera lenses, and there is the bottleneck restriction of landing site in traditional unmanned plane, be difficult to realize going straight up to rise and fall, aloft hover, airmanship such as automatic cruising; Conventional aircraft also exists volume big in addition, the problem of transportation trouble.Existing general rotor craft is the professional and utilizes remote controller control, and is strongly professional, and difficulty is high.
Summary of the invention
The purpose of the utility model is exactly the above-mentioned defective that exists to prior art; Three flight of a kind of single-blade camera system is provided; Have that cost is low, multiple functions such as highly versatile, volume are little, built-in power, transmission over radio, super low-power consumption, satisfy the demand of high-altitude monitoring and video recording production.
Its technical scheme is: mainly by collapsible triangle body, model plane lithium electricity, drive electric accent, control desk, three-axis gyroscope, camera, protective cover and form; The bottom installing drive electricity of described collapsible triangle body is transferred; Drive electricity and transfer connection control desk down; Camera and three-axis gyroscope are installed on the control desk, around each screw propeller, are provided with protective cover, fixing model plane lithium in the collapsible triangle body.
Three directions of above-mentioned collapsible triangle body are installed numeral and analog sensor, and signal wire (SW) is connected to control desk.
The beneficial effect of the utility model is: the needs high-altitude take and situation such as water surface shooting under, can remote real-time monitoring and shooting, native system is self-powered, reaches 50 minutes cruise duration, can not constitute any influence to environment and scene.
Description of drawings
Accompanying drawing 1 is the structural representation of the utility model;
Accompanying drawing 2 is system architecture scheme drawings of the utility model;
Among the last figure: collapsible triangle body 1, model plane lithium electricity 2, drive that electricity transfers 3, control desk 4, three-axis gyroscope 5, camera 6, protective cover 7, single-blade motor 8, terminal 9, monitoring range a.
The specific embodiment
In conjunction with accompanying drawing 1-2, the utility model is done further to describe:
The utility model mainly by collapsible triangle body 1, model plane lithium electricity 2, drive that electricity transfers 3, control desk 4, three-axis gyroscope 5, camera 6, protective cover 7 form; The bottom installing drive electricity of described collapsible triangle body 1 transfers 3; Drive electricity regulation and control system single-blade motor 8; Drive electricity and transfer connection control desk 43 times, camera 6 and three-axis gyroscope 5 are installed on the control desk 4, form the monitoring range a of a plurality of directions; Be provided with protective cover 7 around each screw propeller, fixing model plane lithium electric 2 in the collapsible triangle body 1; Three directions of folding triangle body 1 are installed numeral and analog sensor, and signal wire (SW) is connected to control desk 4.
During use; The CAMDATA interface that special purpose interface is imported the ARM9 treater is passed through in analog video image transmission through camera 6 is gathered; Deposit buffer memory in through the treater coding; Realize wireless issue through the WIFI transport module of control desk 4 then, coupled router sends to the receiving terminal that pre-sets according to the IP address after receiving signal, and the gravity sensing in the Terminal Server Client terminal 9 capable of using can be complementary with three-axis gyroscope on the aircraft 5; Utilize special-purpose piloting procedure to carry out drive simulating, and can obtain realtime graphic.Flight control system adopts high-precision three-axis gyroscope to realize stabilized flight control and attitude adjustment.Operating range reaches as high as 100 meters, can carry out multi-angle and take.
Improved of the bottleneck restriction of traditional unmanned plane, airmanships such as realization is gone straight up to and risen and fallen, hovers, automatic cruising aloft in landing site.Its triangle body is collapsible, volume is little, be convenient to transportation, and it is big to have solved the conventional aircraft volume, the problem of transportation trouble.Flying quality be can transmit in real time earthward and surface state aerial reconnaissance and shooting carried out through wireless real-time passback image.The utility model adopts the interconnection of WIFI transport module; The communication terminal of any WIFI of having transport module (PC, PDA, mobile phone etc.) all can be controlled aircraft; And ability automatic compensation controlled variable; Make the control difficulty of aircraft reduce thus, controllability is stronger, realizes a key vertical lift.Have certain image recognition and follow technology automatically, make the with better function of aircraft, purposes is wider, and flight is more intelligent.
This programme adopts WIFI technology and embedded technology to combine, and on circuit layout and system architecture, all has own characteristic, and cost performance is high.Adopted accurate electronic gyroscope instrument system, overcome the defective of conventional aircraft, the flight stability degree improves greatly, and picture does not have jelly, do not have and rock when taking photo by plane and during real-time video transmission.
Claims (2)
1. three flight of single-blade camera system; It is characterized in that: mainly transfer (3), control desk (4), three-axis gyroscope (5), camera (6), protective cover (7) to form by collapsible triangle body (1), model plane lithium electricity (2), driving electricity; The bottom installing drive electricity of described collapsible triangle body (1) is transferred (3); Driving electricity transfers (3) to connect control desk (4) down; Control desk (4) go up to be installed camera (6) and three-axis gyroscope (5), around each screw propeller, is provided with protective cover (7), fixing model plane lithium electric (2) in the collapsible triangle body (1).
2. three flight of single-blade according to claim 1 camera system is characterized in that: three directions of described collapsible triangle body (1) are installed numeral and analog sensor, and signal wire (SW) is connected to control desk (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220185910 CN202609092U (en) | 2012-04-27 | 2012-04-27 | Single-propeller three-axis flight shooting system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220185910 CN202609092U (en) | 2012-04-27 | 2012-04-27 | Single-propeller three-axis flight shooting system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202609092U true CN202609092U (en) | 2012-12-19 |
Family
ID=47342812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220185910 Expired - Fee Related CN202609092U (en) | 2012-04-27 | 2012-04-27 | Single-propeller three-axis flight shooting system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202609092U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104133484A (en) * | 2014-07-10 | 2014-11-05 | 浙江飞神车业有限公司 | Multi-rotor aircraft electronic control device, multi-rotor aircraft aerial shooting electronic control device, and aerial shooting following multi-rotor aircraft |
-
2012
- 2012-04-27 CN CN 201220185910 patent/CN202609092U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104133484A (en) * | 2014-07-10 | 2014-11-05 | 浙江飞神车业有限公司 | Multi-rotor aircraft electronic control device, multi-rotor aircraft aerial shooting electronic control device, and aerial shooting following multi-rotor aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121219 Termination date: 20130427 |