CN206096948U - Unmanned aerial vehicle control system - Google Patents
Unmanned aerial vehicle control system Download PDFInfo
- Publication number
- CN206096948U CN206096948U CN201621122843.XU CN201621122843U CN206096948U CN 206096948 U CN206096948 U CN 206096948U CN 201621122843 U CN201621122843 U CN 201621122843U CN 206096948 U CN206096948 U CN 206096948U
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- China
- Prior art keywords
- control system
- aerial vehicle
- vehicle control
- unmanned aerial
- flight controller
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Abstract
The utility model discloses an unmanned aerial vehicle control system, including flight controller, current -voltage meter, lithium cell, OSD image superimposer, data transmission ware, flight controller is junction current voltameter, OSD image superimposer, data transmission ware respectively, and current -voltage counts and still connects the lithium cell, flight controller is last still to be connected with a plurality of electronic governor. The utility model discloses unmanned aerial vehicle control system adopts the integration design, and intelligent degree is high, and the module use amount is few, has reduced cost of manufacture and preparation complexity.
Description
Technical field
This utility model is related to unmanned air vehicle technique, specifically a kind of unmanned aerial vehicle control system.
Background technology
Expect 2025, domestic unmanned plane market scale is about 30,000,000,000, and agricultural plant protection is about 20,000,000,000, security protection city
Field about 15,000,000,000, electric inspection process is about 5,000,000,000, and total scale will be up to 75,000,000,000.This under the background of scale development, it is bound to
There are substantial amounts of Hang Wai companies to enter this field.In the case of according to prior art, because the enterprise of other industries enters this
Industry, in the case of the unmanned air vehicle technique being ignorant of, cannot quickly produce finished product.But this design of my company is just
Such problem is solved, the layman enterprise for making also can quickly assemble unmanned plane finished product.Prior art, enterprises production efficiency
Low, fraction defective is high, and assembling is complicated, safeguards and sell all very inconvenient.
Utility model content
The purpose of this utility model is to provide a kind of degree of intelligence height, the few unmanned aerial vehicle control system of module usage amount,
Propose in solve the problems, such as above-mentioned background technology.
For achieving the above object, this utility model provides following technical scheme：
A kind of unmanned aerial vehicle control system, including flight controller, current/voltage meter, lithium battery, OSD image overlay devices, number
According to transmitter, the flight controller connects respectively current/voltage meter, OSD image overlay devices, data link, current/voltage meter
Lithium battery is also connected with, multiple electron speed regulators are also associated with the flight controller.
As preferred version of the present utility model：The rated voltage of the lithium battery is 11.1V.
As preferred version of the present utility model：Motor is respectively connected with each electron speed regulator.
Compared with prior art, the beneficial effects of the utility model are：This utility model unmanned aerial vehicle control system adopts one
Body Integrated design, degree of intelligence is high, and module usage amount is few, reduces cost of manufacture and makes complexity.
Description of the drawings
Fig. 1 is a kind of unmanned aerial vehicle control system overall construction drawing of the present utility model.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of this utility model protection.
Refer to Fig. 1, a kind of unmanned aerial vehicle control system, including flight controller, current/voltage meter, lithium battery, OSD images
Averager, data link, the flight controller connects respectively current/voltage meter, OSD image overlay devices, data link,
Current/voltage meter is also connected with lithium battery, and multiple electron speed regulators are also associated with the flight controller.
The rated voltage of lithium battery is 11.1V.Motor is respectively connected with each electron speed regulator.
Operation principle of the present utility model is：1. integrated design is adopted, as long as a small amount of welding just can be assembled
One finished product, produces efficiency in enormous quantities and improves nearly 70%, 2. adopts integrated design, tailored appearance, operation to deduct 60%, no
Yield is substantially reduced.
Preferred embodiment of the present utility model is the foregoing is only, it is all in this practicality not to limit this utility model
Within new spirit and principle, any modification, equivalent substitution and improvements made etc. should be included in guarantor of the present utility model
Within the scope of shield.
Claims (3)
1. a kind of unmanned aerial vehicle control system, including flight controller, current/voltage meter, lithium battery, OSD image overlay devices, data
Transmitter, it is characterised in that the flight controller connects respectively current/voltage meter, OSD image overlay devices, data link,
Current/voltage meter is also connected with lithium battery, and multiple electron speed regulators are also associated with the flight controller.
2. a kind of unmanned aerial vehicle control system according to claim 1, it is characterised in that the rated voltage of the lithium battery is
11.1V。
3. a kind of unmanned aerial vehicle control system according to claim 2, it is characterised in that be all connected with each electron speed regulator
There is motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621122843.XU CN206096948U (en) | 2016-10-14 | 2016-10-14 | Unmanned aerial vehicle control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621122843.XU CN206096948U (en) | 2016-10-14 | 2016-10-14 | Unmanned aerial vehicle control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206096948U true CN206096948U (en) | 2017-04-12 |
Family
ID=58483267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621122843.XU Expired - Fee Related CN206096948U (en) | 2016-10-14 | 2016-10-14 | Unmanned aerial vehicle control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206096948U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106990739A (en) * | 2017-05-19 | 2017-07-28 | 安徽师范大学 | A kind of unmanned aerial vehicle control system |
-
2016
- 2016-10-14 CN CN201621122843.XU patent/CN206096948U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106990739A (en) * | 2017-05-19 | 2017-07-28 | 安徽师范大学 | A kind of unmanned aerial vehicle control system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 Termination date: 20171014 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |