CN201002722Y - Aircraft two freedom degree image stabilizing platform - Google Patents

Aircraft two freedom degree image stabilizing platform Download PDF

Info

Publication number
CN201002722Y
CN201002722Y CNU2007201033402U CN200720103340U CN201002722Y CN 201002722 Y CN201002722 Y CN 201002722Y CN U2007201033402 U CNU2007201033402 U CN U2007201033402U CN 200720103340 U CN200720103340 U CN 200720103340U CN 201002722 Y CN201002722 Y CN 201002722Y
Authority
CN
China
Prior art keywords
aircraft
roll
pitch
gyroscope
degrees
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
CNU2007201033402U
Other languages
Chinese (zh)
Inventor
仝昊天
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CNU2007201033402U priority Critical patent/CN201002722Y/en
Application granted granted Critical
Publication of CN201002722Y publication Critical patent/CN201002722Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Stereoscopic And Panoramic Photography (AREA)
  • Accessories Of Cameras (AREA)

Abstract

A two-degree-of-freedom image stabilization pan comprises a detection device, an action device and an image collection device. The detection device is electrically connected with the action device, the action device is connected with the image collection device, the detection device is used to detect a swing angle of an aircraft and the action device correspondingly adjusts detection results of the detection device. If mounted on the aircraft, the utility model can ensure the camera lens is kept steady while the aircraft is shaking so as to stabilize, trace and lock an image while finely tune the shaking of a vehicle.

Description

Aircraft two degrees of freedom surely looks like The Cloud Terrace
Technical field
The present invention relates to the electronic equipment field, particularly relate to a kind of aircraft two degrees of freedom and surely look like The Cloud Terrace.
Background technology
Utilize the aircraft images acquired very general, but at present during images acquired, the staff just simply is fixed on image collecting device on the aircraft, aircraft image acquisition in flight course is put and can be carried out ground, the continuous acquisition work of image all around, but the flight of aircraft is not pulsation-free always, and roll takes place sometimes, pitching takes place sometimes, so along with the action of aircraft, along with rocking, it is not very high taking the picture quality of coming out to camera lens yet.
The utility model content
The utility model is at the defective of above-mentioned prior art, provide a kind of aircraft two degrees of freedom surely to look like The Cloud Terrace, it is loaded on the aircraft, can accomplish that aircraft rocks, and pick-up lens does not rock thereupon, thereby has stablely, follows the tracks of, the effect of lock image also can be made fine setting to the shake of the vehicle.
Aircraft two degrees of freedom surely looks like The Cloud Terrace, comprise a detecting device, a movement device and an image collecting device, described detecting device is electrically connected with described movement device, described movement device is captiveed joint with image collecting device, described detecting device is used for the pendulum angle of sense aircraft, and described movement device is used for the testing result of detecting device is done the corresponding action of adjusting.
Described detecting device comprises a roll gyroscope and a pitch gyroscope, the angle of described roll gyroscope sense aircraft roll, the angle of described pitch gyroscope sense aircraft pitching.
Described movement device comprises a roll steering wheel and a pitch-control motor, and described roll steering wheel is electrically connected with the roll gyroscope, and the angle of roll is made corresponding adjustment; Described pitch-control motor is electrically connected with pitch gyroscope, and the angle of pitching is made corresponding adjustment, and described detecting device also comprises a support, and described roll steering wheel and a pitch-control motor are separately fixed on the described support and setting in vertical direction.
Described image collector is changed to pick up camera.
Described pitch-control motor is captiveed joint with pick up camera, and described pitch-control motor is installed in pitching place of support, and described roll steering wheel is fixed on roll place of support.
Described support is an aluminium alloy post.
Aircraft two degrees of freedom is a system that realizes the images acquired function on aircraft as The Cloud Terrace surely, the image stabilization of the utility model for realizing collecting, a detecting device and a movement device have been adopted, detecting device is used for the motion conditions of sense aircraft, it is fed back to movement device, make the corresponding action adjustment, move and the motionless purpose of image thereby reach aircraft by movement device, make and take the image stabilization that obtains, clear.
A roll gyroscope and a pitch gyroscope have been comprised in the detecting device, the roll gyroscope detects the roll angle of flight, pitch gyroscope detects the luffing angle of flight, comprise a roll steering wheel and a pitch-control motor in the movement device, the roll steering wheel is made compensation to the roll angle, pitch-control motor is made compensation to luffing angle, thereby realizes the function of the steady picture of two degrees of freedom.
The utility model has adopted a support, and pitch-control motor is captiveed joint with pick up camera, and is rack-mount, and the pitch-control motor action drives the pick up camera action, thereby makes pick up camera obtain the compensation of luffing angle; The roll steering wheel is fixedly mounted on roll place of support, and the action of roll steering wheel drives the support action, makes pick up camera also obtain the compensation of roll angle, has realized that therefore aircraft is moving, and the motionless purpose of camera.The preferred aluminum alloy materials of support, the one, because it punches easily other parts are fixed, the while light weight, it is too big to be unlikely the load increase that makes aircraft.
Utilize the aircraft of RC Goblin model plane as experiment usefulness, the utility model aircraft two degrees of freedom surely is fixed on the helicopter as The Cloud Terrace, by remote controller control helicopter flight, the distant bar of remote controller by the control steering wheel manually obtains to enter the steady picture of locking state again behind the image then, the image of camera picked-up is transferred to video signal receiver, insert computer through video-signal converting apparatus again, just can clearly see the image of pick up camera in the helicopter photographs, make helicopter make exercises by the aircraft remote controller, can see that from computer unsharp phenomenon does not take place image.Because The Cloud Terrace has two degrees of freedom, the scope that artificially obtains image is very big, and is also very flexible.Can also after choosing image by hand, enter the steady picture of locking state again.
Description of drawings
Fig. 1 the utility model aircraft two degrees of freedom surely looks like The Cloud Terrace and is connected the work scheme drawing with external piece
Each label lists as follows among the figure:
1-aircraft two degrees of freedom surely looks like The Cloud Terrace, 2-helicopter power supply, 3-video signal receiver, the 4-video-signal converting apparatus, the 5-computer, 11-detecting device, 12-movement device, the 13-image collecting device, 14-aluminium alloy post 111-roll gyroscope, 112-pitch gyroscope, 121-roll steering wheel, the 122-pitch-control motor, the 131-pick up camera.
The specific embodiment
Embodiment
Fig. 1 is connected the work scheme drawing for the utility model aircraft two degrees of freedom surely looks like The Cloud Terrace with external piece.Aircraft two degrees of freedom surely looks like The Cloud Terrace 1 by detecting device 11, and movement device 12 and image collecting device 13 are formed, and movement device 12 and image collecting device 13 are installed on the aluminium alloy post 14.Movement device 12 is electrically connected with detecting device 11, and detecting device 11 is used to detect the pendulum angle of helicopter, and movement device 12 is used for the testing result of detecting device 11 is done the corresponding action of adjusting.Detecting device comprises a roll gyroscope 111 and a pitch gyroscope 112, the roll gyroscope is installed in roll place of helicopter, be used to detect the angle of helicopter roll, pitch gyroscope 112 is installed in pitching place of helicopter, is used for the angle of sense aircraft pitching.
Movement device 12 comprises a roll steering wheel 121 and a pitch-control motor 122, and roll steering wheel 121 is electrically connected with roll gyroscope 111, and the angle of roll is made corresponding adjustment; Pitch-control motor 122 is electrically connected with pitch gyroscope 112, and the angle of pitching is made corresponding adjustment.Image collector is changed to pick up camera 131, and pitch-control motor 122 is captiveed joint with pick up camera 131 and is fixedly mounted on pitching place of aluminium alloy post 14, and roll steering wheel 121 is fixed on roll place of aluminium alloy post 14.
Aircraft two degrees of freedom surely is installed on the helicopter as The Cloud Terrace 1, with roll gyroscope 111 and pitch gyroscope 112, roll steering wheel 121 is connected with helicopter power supply 2 with pitch-control motor 122, the action of control helicopter remote controller RC Goblin, and then manually obtain to enter again behind the image the steady picture of locking state by the distant bar of remote controller of control steering wheel, the picture signal of image collecting device 13 picked-ups passes to video signal receiver 3, be connected to computer 5 through video-signal converting apparatus 4 again, just can have seen the image of collection.Because reverse respectively control roll steering wheel 121 in back and pitch-control motor 122 are measured in rocking of roll gyroscope 111 and 112 pairs of helicopters of pitch gyroscope, make it to the corresponding angle of pick up camera 131 compensation, it is constant that thereby the influence that pick up camera can not be rocked by helicopter, camera can keep setting attitude.Can see that from computer after the rocking of helicopter, image is obviously swing and unsharp phenomenon not.Because two degrees of freedom is arranged, the scope that artificially obtains image is also very big, and angle that can very flexible adjustment shooting can also enter lock onto target again behind the image and surely looks like state by manual choosing.

Claims (6)

1. aircraft two degrees of freedom surely looks like The Cloud Terrace, comprise a detecting device, a movement device and an image collecting device, it is characterized in that: described detecting device is electrically connected with described movement device, described movement device is captiveed joint with image collecting device, described detecting device is used for the pendulum angle of sense aircraft, and described movement device is used for the testing result of detecting device is done the corresponding action of adjusting.
2. aircraft two degrees of freedom according to claim 1 surely looks like The Cloud Terrace, it is characterized in that: described detecting device comprises a roll gyroscope and a pitch gyroscope, the angle of described roll gyroscope sense aircraft roll, the angle of described pitch gyroscope sense aircraft pitching.
3. aircraft two degrees of freedom according to claim 2 surely looks like The Cloud Terrace, it is characterized in that: described movement device comprises a roll steering wheel and a pitch-control motor, and described roll steering wheel is electrically connected with the roll gyroscope, and the angle of roll is made corresponding adjustment; Described pitch-control motor is electrically connected with pitch gyroscope, and the angle of pitching is made corresponding adjustment, and described detecting device also comprises a support, and described roll steering wheel and a pitch-control motor are separately fixed on the described support and setting in vertical direction.
4. aircraft two degrees of freedom according to claim 1 surely looks like The Cloud Terrace, it is characterized in that: described image collector is changed to pick up camera.
5. aircraft two degrees of freedom according to claim 4 surely looks like The Cloud Terrace, it is characterized in that: described pitch-control motor is captiveed joint with pick up camera, and described pitch-control motor is installed in pitching place of support, and described roll steering wheel is fixed on roll place of support.
6. aircraft two degrees of freedom according to claim 5 surely looks like The Cloud Terrace, it is characterized in that: described support is an aluminium alloy post.
CNU2007201033402U 2007-01-25 2007-01-25 Aircraft two freedom degree image stabilizing platform Expired - Fee Related CN201002722Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007201033402U CN201002722Y (en) 2007-01-25 2007-01-25 Aircraft two freedom degree image stabilizing platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007201033402U CN201002722Y (en) 2007-01-25 2007-01-25 Aircraft two freedom degree image stabilizing platform

Publications (1)

Publication Number Publication Date
CN201002722Y true CN201002722Y (en) 2008-01-09

Family

ID=39038262

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007201033402U Expired - Fee Related CN201002722Y (en) 2007-01-25 2007-01-25 Aircraft two freedom degree image stabilizing platform

Country Status (1)

Country Link
CN (1) CN201002722Y (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102996984A (en) * 2011-09-09 2013-03-27 深圳市大疆创新科技有限公司 Gyro-type dynamic self-balancing pan-tilt
CN103092437A (en) * 2012-12-13 2013-05-08 同济大学 Portable touch interactive system based on image processing technology
WO2013158050A1 (en) 2012-04-16 2013-10-24 Airnamics, Napredni Mehatronski Sistemi D.O.O. Stabilization control system for flying or stationary platforms
CN104811588A (en) * 2015-04-10 2015-07-29 浙江工业大学 Shipborne image stabilization control method based on gyroscope
CN104914883A (en) * 2015-06-16 2015-09-16 百色学院 Camera steering gear pan-tilt control system
US9485427B2 (en) 2013-10-08 2016-11-01 SZ DJI Technology Co., Ltd Apparatus and methods for stabilization and vibration reduction
US9493232B2 (en) 2013-07-31 2016-11-15 SZ DJI Technology Co., Ltd. Remote control method and terminal
US9648240B2 (en) 2011-09-09 2017-05-09 SZ DJI Technology Co., Ltd Stabilizing platform
CN109538900A (en) * 2018-09-10 2019-03-29 天津市亚安科技有限公司 Based on gyroscope PID surely as cloud platform control system and method, manned vehicle
CN111854677A (en) * 2020-07-30 2020-10-30 大连理工大学 Device for measuring swinging angle of soft rope for hanging heavy object on aircraft

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11140322B2 (en) 2011-09-09 2021-10-05 Sz Dji Osmo Technology Co., Ltd. Stabilizing platform
US10321060B2 (en) 2011-09-09 2019-06-11 Sz Dji Osmo Technology Co., Ltd. Stabilizing platform
US9648240B2 (en) 2011-09-09 2017-05-09 SZ DJI Technology Co., Ltd Stabilizing platform
CN102996984A (en) * 2011-09-09 2013-03-27 深圳市大疆创新科技有限公司 Gyro-type dynamic self-balancing pan-tilt
WO2013158050A1 (en) 2012-04-16 2013-10-24 Airnamics, Napredni Mehatronski Sistemi D.O.O. Stabilization control system for flying or stationary platforms
CN103092437A (en) * 2012-12-13 2013-05-08 同济大学 Portable touch interactive system based on image processing technology
CN103092437B (en) * 2012-12-13 2016-07-13 同济大学 A kind of Portable touch interactive system based on image processing techniques
US10747225B2 (en) 2013-07-31 2020-08-18 SZ DJI Technology Co., Ltd. Remote control method and terminal
US11385645B2 (en) 2013-07-31 2022-07-12 SZ DJI Technology Co., Ltd. Remote control method and terminal
US9493232B2 (en) 2013-07-31 2016-11-15 SZ DJI Technology Co., Ltd. Remote control method and terminal
US9927812B2 (en) 2013-07-31 2018-03-27 Sz Dji Technology, Co., Ltd. Remote control method and terminal
US11962905B2 (en) 2013-10-08 2024-04-16 Sz Dji Osmo Technology Co., Ltd. Apparatus and methods for stabilization and vibration reduction
US9485427B2 (en) 2013-10-08 2016-11-01 SZ DJI Technology Co., Ltd Apparatus and methods for stabilization and vibration reduction
US10334171B2 (en) 2013-10-08 2019-06-25 Sz Dji Osmo Technology Co., Ltd. Apparatus and methods for stabilization and vibration reduction
US11134196B2 (en) 2013-10-08 2021-09-28 Sz Dji Osmo Technology Co., Ltd. Apparatus and methods for stabilization and vibration reduction
CN104811588B (en) * 2015-04-10 2018-04-20 浙江工业大学 A kind of boat-carrying based on gyroscope is surely as control method
CN104811588A (en) * 2015-04-10 2015-07-29 浙江工业大学 Shipborne image stabilization control method based on gyroscope
CN104914883A (en) * 2015-06-16 2015-09-16 百色学院 Camera steering gear pan-tilt control system
CN109538900A (en) * 2018-09-10 2019-03-29 天津市亚安科技有限公司 Based on gyroscope PID surely as cloud platform control system and method, manned vehicle
CN111854677A (en) * 2020-07-30 2020-10-30 大连理工大学 Device for measuring swinging angle of soft rope for hanging heavy object on aircraft

Similar Documents

Publication Publication Date Title
CN201002722Y (en) Aircraft two freedom degree image stabilizing platform
US12038129B2 (en) Systems and methods for payload stabilization
CN201287830Y (en) Stabilising bracket for aerial photography camera
US11140322B2 (en) Stabilizing platform
CN107483781B (en) Stabilizing device for self-leveling of unmanned boat pan-tilt camera
CN203705964U (en) Stable closed-loop control device of airborne 3-DOF pan-tilt
CN201626554U (en) Three-freedom-degree inertia stabilization aerial photography cradle head
CN110347171B (en) Aircraft control method and aircraft
CN204372480U (en) Three axles are dynamically from steady The Cloud Terrace
CN104390110A (en) Tri-axial dynamic self-stabilizing cradle head and working method thereof
CN104168460B (en) A kind of light airborne three-axis stabilization device for image
CN103754380B (en) A kind of many lens aerial photography stable platforms
CN102556359A (en) Airborne air-photo image-stabilizing cloud deck of unmanned aerial vehicle
CN205872506U (en) Unmanned aerial vehicle's nacelle
CN103148324A (en) Vehicle-mounted self-balancing camera pan-tilt
US20190049823A1 (en) Ground moving device, stabilizer, mount, and robot head
CN108482694A (en) A kind of rotary oblique photograph holder of two mirrors
CN106965949A (en) A kind of aircraft antidetonation camera
CN207045774U (en) Photo control point aircraft is used in a kind of orthography mapping
CN205186546U (en) Unmanned aerial vehicle with anti -trembling function
CN203780804U (en) Shock-absorption shooting cradle head of aircraft
CN206704562U (en) A kind of single-lens sweeping formula oblique photograph head of unmanned plane
CN207809802U (en) A kind of aircraft inclination flight Self-stabilization holder
CN210852966U (en) Aerial image acquisition device
CN205003745U (en) Processing system is shot to anti -shake's motion target

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: 20080109

Termination date: 20110125