CN206766368U - A kind of camera system based on four rotor wing unmanned aerial vehicles - Google Patents

A kind of camera system based on four rotor wing unmanned aerial vehicles Download PDF

Info

Publication number
CN206766368U
CN206766368U CN201720668878.1U CN201720668878U CN206766368U CN 206766368 U CN206766368 U CN 206766368U CN 201720668878 U CN201720668878 U CN 201720668878U CN 206766368 U CN206766368 U CN 206766368U
Authority
CN
China
Prior art keywords
unmanned aerial
camera system
system based
adjusting means
photographing device
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.)
Expired - Fee Related
Application number
CN201720668878.1U
Other languages
Chinese (zh)
Inventor
潘俊涛
王强
吴国强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
North Minzu University
Original Assignee
North Minzu University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by North Minzu University filed Critical North Minzu University
Priority to CN201720668878.1U priority Critical patent/CN206766368U/en
Application granted granted Critical
Publication of CN206766368U publication Critical patent/CN206766368U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

It the utility model is related to a kind of camera system based on four rotor wing unmanned aerial vehicles, including unmanned aerial vehicle body, four rotors, the photographing device that are arranged at the top of the unmanned aerial vehicle body, also include adjusting means, described adjusting means is arranged at the bottom of unmanned aerial vehicle body, described photographing device is arranged in adjusting means, and adjusting means is used to adjust photographing device in real time to targeted attitude.The utility model uses above-mentioned design form, has the characteristics of stable of taking pictures, can greatly improve performance of the unmanned plane when taking pictures, and the utility model also has easy care, changes the advantages of facilitating in addition.

Description

A kind of camera system based on four rotor wing unmanned aerial vehicles
Technical field
It the utility model is related to unmanned air vehicle technique field, in particular to a kind of camera system based on four rotor wing unmanned aerial vehicles.
Background technology
Unmanned plane is unpiloted airborne vehicle on a kind of machine, and it has power set and navigation module, in certain limit It is interior to be preprogramed autonomous control flight by radio robot or computer.At present, the whole world has more than 50 country's equipments More than 300 kinds of unmanned plane, more famous " global hawk ", " predator " that have the U.S., Chinese " ASN " serial large-scale without It is man-machine etc..UAS is the technical support system of a set of synthesis, and it is the extension to unmanned plane concept, and it is by body, machine Upper load and ground installation etc. form, and realize the functions such as its flight, manipulation, data processing and Information Conduction.Filled on unmanned plane Carry multiclass sensor, such as camera, it is possible to achieve image real-time Transmission, high-risk areas detecting function, be widely used in agricultural, The field such as military, traffic and meteorology, to realize cruise shooting and the monitoring to designated area.
At present, civilian unmanned plane realizes vertical lift and high-altitude hovering using more rotary wind type structures mostly, so as to meet to navigate The requirement clapped and monitored.Particularly four rotor wing unmanned aerial vehicles, rotor are evenly distributed in the surrounding of unmanned aerial vehicle body, the stagnant sky of unmanned plane When or be difficult to by rotor the absolute stability for keeping unmanned aerial vehicle body during flight, four rotor moment are tieed up by adjusting rotating speed Hold the stability of complete machine fuselage.Because photographing device is usually rigidly connected with unmanned plane, the swing of unmanned aerial vehicle body will also cause Subsidiary photographing device is swung.Particularly after unmanned plane rises to certain altitude, although the swing of unmanned aerial vehicle body is smaller, Also result in and be installed on the photographing device of fuselage bottom and produce larger swing, unmanned plane will produce larger when high-altitude is taken pictures Deviation, influence unmanned plane and take pictures effect.
The content of the invention
Purpose of design of the present utility model is:By the optimization improvement design to existing unmanned plane camera system structure, Improve the effect of taking pictures when being taken pictures using unmanned plane.
In order to realize above-mentioned purpose of design, the technical solution adopted in the utility model is:
A kind of camera system based on four rotor wing unmanned aerial vehicles, including unmanned aerial vehicle body, symmetrical four rotor and photographing device, also Including adjusting means, the adjusting means is arranged at the bottom of unmanned aerial vehicle body, and the photographing device is arranged in adjusting means, Adjusting means is in targeted attitude for adjusting photographing device.
According to the utility model embodiment, adjusting means includes platform, at least two support columns, motor and angle and passed Sensor, one end of support column are connected to the bottom of unmanned aerial vehicle body, and the other end connects the platform, and platform forms branch with support column Support structure, photographing device are arranged on platform, and at least a support column is telescoping shoring post;Angular transducer is flat for monitoring The angle change of platform, motor are used to drive telescoping shoring post to do stretching motion to realize that the regulation platform is in target Posture.It is further preferred that support column is three, platform and three support columns form three-point support structure.
Preferably, wherein two support columns are telescoping shoring post, motor is two, and a motor is used to drive Move a support column and do stretching motion.It is further preferred that motor is piezoelectric ceramic motor.
Preferably, uav bottom is additionally provided with support frame, and photographing device is located in support frame.It is preferred that support frame as described above is Cuboid framework structure.
By adopting the above-described technical solution, the camera system provided by the utility model based on four rotor wing unmanned aerial vehicles has Following beneficial effect:
1) system includes adjusting means, and the adjusting means is arranged at the bottom of unmanned aerial vehicle body, the photographing device It is arranged in adjusting means, when photographing device produces displacement with the swing of unmanned aerial vehicle body, adjusting means can adjust bat Targeted attitude is at according to equipment, improves stability and quality of taking pictures that unmanned plane is taken pictures.
2) adjusting means includes platform, support column, motor and angular transducer, simple in construction, it is easy to accomplish, and prop up When dagger uses three, platform and three support columns form three-point support structure, can strengthen the steadiness of supporting construction.
3) by setting two telescoping shoring posts, a support column is driven with a motor, can be caused described Platform preferably reaches targeted attitude.
4) because ceramic material has the advantages of being exceedingly fast response speed, regulation dress of the present utility model under inverse piezoelectric effect The motor put uses piezoelectric ceramic motor, can make motor under inverse piezoelectric effect can quick response, improve its use Performance.
5) uav bottom is additionally provided with support frame, and photographing device is located in support frame, can protect photographing device not with Ground contacts, and then avoids photographing device from being damaged.Support frame is cuboid framework structure, and structure is smooth, can ensure unmanned plane Stable landing, will not turn on one's side.
Brief description of the drawings
Fig. 1 is the structural representation of the camera system based on four rotor wing unmanned aerial vehicles.
Fig. 2 is the structural representation of the camera system based on four rotor wing unmanned aerial vehicles after adjustment.
Marked in figure:Unmanned aerial vehicle body 1, four rotors 2, adjusting means 3, photographing device 4, support frame 5.
Embodiment
The utility model is described in further detail with reference to test example and embodiment.
A kind of camera system based on four rotor wing unmanned aerial vehicles as shown in Figure 1, including unmanned aerial vehicle body 1, be arranged at it is described Four rotors 2, photographing device 4 at the top of unmanned aerial vehicle body, in addition to adjusting means 3, the adjusting means 3 are arranged at unmanned plane machine The bottom of body, the photographing device 4 are arranged in adjusting means 3, and adjusting means 3 is in target appearance for adjusting photographing device 4 State, to improve the stability that unmanned plane is taken pictures.
As a kind of citing of embodiment, in the present embodiment, adjusting means 3 include platform, three support columns, two Motor and angular transducer, one end of support column are connected to the bottom of unmanned aerial vehicle body 1, and the other end connects the platform, Platform forms supporting construction with support column, and photographing device 4 is arranged on platform, wherein two support columns are telescoping shoring post, A piece telescoping shoring post is controlled by a motor.Angular transducer can be arranged on platform, for monitoring platform Angle change, when unmanned aerial vehicle body produces swing, support column also can correspondingly be swung, and produce angle change, angular transducer The angle change can be monitored, now motor then drives telescoping shoring post to do stretching motion, on-telescopic support column It is then motionless, so that whole supporting construction is in dbjective state, and then realizes that regulation photographing device 4 is in targeted attitude, such as Fig. 2 institutes Show.The targeted attitude can be the residing posture of photographing device or the appearance set in addition before unmanned aerial vehicle body is swung State.
In the present embodiment, three-point support structure is formed using three support columns and platform, can so strengthen supporting construction Steadiness, more accurately attitude regulation can also be realized by adjusting two telescoping shoring posts, it is readily appreciated that, support column Quantity can also be other set-up modes, as long as ensure be at least two, the quantity of telescoping shoring post can also be only It is limited at least one.
Motor can be preferably piezoelectric ceramic motor, so motor can be made quickly to be rung under inverse piezoelectric effect Should, improve its performance.
In addition, the bottom of unmanned aerial vehicle body 1 is additionally provided with support frame 5, photographing device 4 is located in support frame 5, when unmanned plane falls During ground, using the protection of support frame 5, photographing device can be avoided to be suffered damage with collision on the ground.It is preferred that support frame 5 is rectangular Body frame structure, ensure stabilization during unmanned plane landing, will not turn on one's side.
The foregoing is only a specific embodiment of the invention, but protection scope of the present invention is not limited thereto, any Those familiar with the art the invention discloses technical scope in, change or replacement can be readily occurred in, should all be contained Cover within protection scope of the present invention.Therefore, protection scope of the present invention described should be defined by scope of the claims.

Claims (7)

1. a kind of camera system based on four rotor wing unmanned aerial vehicles, including unmanned aerial vehicle body, it is arranged at the top of the unmanned aerial vehicle body Four rotors, photographing device, it is characterised in that:Also include adjusting means, the adjusting means is arranged at the bottom of unmanned aerial vehicle body Portion, the photographing device are arranged in adjusting means, and adjusting means is in targeted attitude for adjusting photographing device.
A kind of 2. camera system based on four rotor wing unmanned aerial vehicles according to claim 1, it is characterised in that:Adjusting means bag Platform, at least two support columns, motor and angular transducer are included, one end of support column is connected to the bottom of unmanned aerial vehicle body Portion, the other end connect the platform, and platform forms supporting construction with support column, and photographing device is arranged on platform, at least one Support column is telescoping shoring post;Angular transducer is used for the angle change of monitoring platform, and motor is telescopic for driving Support column does stretching motion to realize that the regulation platform is in targeted attitude.
A kind of 3. camera system based on four rotor wing unmanned aerial vehicles according to claim 2, it is characterised in that:Support column is three Root, platform and three support columns form three-point support structure.
A kind of 4. camera system based on four rotor wing unmanned aerial vehicles according to Claims 2 or 3, it is characterised in that:Wherein two Root support column is telescoping shoring post, and motor is two, and a motor is used to drive a support column to do flexible fortune It is dynamic.
A kind of 5. camera system based on four rotor wing unmanned aerial vehicles according to Claims 2 or 3, it is characterised in that:Driving electricity Machine is piezoelectric ceramic motor.
A kind of 6. camera system based on four rotor wing unmanned aerial vehicles according to claim 1, it is characterised in that:Uav bottom Support frame is additionally provided with, photographing device is located in support frame.
A kind of 7. camera system based on four rotor wing unmanned aerial vehicles according to claim 6, it is characterised in that:Support frame as described above For cuboid framework structure.
CN201720668878.1U 2017-06-09 2017-06-09 A kind of camera system based on four rotor wing unmanned aerial vehicles Expired - Fee Related CN206766368U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720668878.1U CN206766368U (en) 2017-06-09 2017-06-09 A kind of camera system based on four rotor wing unmanned aerial vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720668878.1U CN206766368U (en) 2017-06-09 2017-06-09 A kind of camera system based on four rotor wing unmanned aerial vehicles

Publications (1)

Publication Number Publication Date
CN206766368U true CN206766368U (en) 2017-12-19

Family

ID=60636699

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720668878.1U Expired - Fee Related CN206766368U (en) 2017-06-09 2017-06-09 A kind of camera system based on four rotor wing unmanned aerial vehicles

Country Status (1)

Country Link
CN (1) CN206766368U (en)

Similar Documents

Publication Publication Date Title
US10330254B2 (en) Method and system for stabilizing a payload
CN105775118B (en) Jamproof unmanned plane device and control method during one kind hovering
US20220137643A1 (en) Aircraft control method and aircraft
CN105691613A (en) Unmanned aerial vehicle ascending and descending smoothly and control method
WO2020017488A1 (en) Unmanned aerial vehicle
CN104802985A (en) Variable axial multi-rotor aircraft and flight attitude adjustment method thereof
CN109606674A (en) Tail sitting posture vertical take-off and landing drone and its control system and control method
WO2018040006A1 (en) Control method, device and system, aerial vehicle, carrier, and operating device
AU2019100363A4 (en) Unmanned Aerial Vehicle And Its Program Control Device Unmanned Aerial Vehicle And Its Program Control Device
CN106586009A (en) Unmanned aerial vehicle
CN207808952U (en) It is a kind of based on bionics principle three dwell movement quadrotor drone
CN106240807B (en) A kind of integrated unmanned plane of collection photodetection
CN206243457U (en) A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle
CN206012982U (en) A kind of small-sized electric fixed-wing unmanned plane for oblique photograph
CN205060006U (en) Four -rotor unmanned aerial vehicle
CN206021084U (en) Manipulation device
CN111959819A (en) Multi-rotor unmanned aerial vehicle algorithm verification and parameter adjustment system and use method thereof
CN206050074U (en) VTOL Fixed Wing AirVehicle
CN206766368U (en) A kind of camera system based on four rotor wing unmanned aerial vehicles
CN106114817A (en) A kind of aircraft and flight system
CN206096942U (en) Flight control and aircraft
RU130953U1 (en) UNMANNED AIRCRAFT (OPTIONS)
WO2017215594A1 (en) Unmanned aerial vehicle automatic air brushing device
JP6661136B1 (en) Unmanned aerial vehicle
WO2020017486A1 (en) Unmanned aerial vehicle

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: 20171219

Termination date: 20210609

CF01 Termination of patent right due to non-payment of annual fee