CN104516355A - Self-photographing aircraft and self-photographing method thereof - Google Patents
Self-photographing aircraft and self-photographing method thereof Download PDFInfo
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- CN104516355A CN104516355A CN201410855994.5A CN201410855994A CN104516355A CN 104516355 A CN104516355 A CN 104516355A CN 201410855994 A CN201410855994 A CN 201410855994A CN 104516355 A CN104516355 A CN 104516355A
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- auto heterodyne
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Abstract
The invention discloses a self-photographing aircraft and a self-photographing method thereof. The self-photographing aircraft comprises an aircraft body and a ground controller in wireless communication connection with the aircraft body, wherein the aircraft body comprises a flight control circuit, a flight positioning module, a flight wireless communication module and a camera; the flight positioning module, the flight wireless communication module and the camera are connected with the flight control circuit; the ground controller is a self-photographing controller which comprises a control casing, a ground control circuit, a ground wireless communication circuit and a ground positioning module; the ground control circuit, the ground wireless communication circuit and the ground positioning module are arranged in the control casing; the ground wireless communication circuit and the ground positioning module are electrically connected with the ground control circuit; the self-photographing controller further comprises a self-photographing button arranged on the control casing; the self-photographing button is electrically connected with the ground control circuit; the ground wireless communication circuit is in wireless communication connection with the flight wireless communication circuit. According to the self-photographing aircraft, the aircraft body can take pictures or videos along a flight path according to received positioning information from the ground positioning module after a self-photographer presses the self-photographing button, thereby achieving the self-photographing purpose.
Description
Technical field
The present invention relates to a kind of small aircraft, particularly relate to a kind of auto heterodyne type aircraft and self-timer method thereof.
Background technology
In prior art, have the small aircraft (unmanned vehicle) that much can carry out taking photo by plane, but these small aircrafts are in shooting process, for the shooting to other people or article as many, and are not suitable for the shooting to oneself.Because the ground controller of small aircraft of the prior art does not have the function button that can directly autodyne, cause utilizing small aircraft to carry out auto heterodyne and become very complicated, and inconvenient operation.
Therefore, be necessary to develop the small aircraft that can carry out easily autodyning.
Summary of the invention
In order to overcome above-mentioned the deficiencies in the prior art part, the object of the present invention is to provide a kind of auto heterodyne type aircraft and self-timer method thereof.
A kind of auto heterodyne type aircraft, comprises aircraft body, and the ground controller be connected with the wireless telecommunications of aircraft body; Described aircraft body comprises flight control circuit, and with flight control circuit be connected flight locating module, fly wireless communication module and video camera; Described ground controller is auto heterodyne controller, comprises control housing, and is provided with the ground control circuit, terrestrial wireless communicating circuit and the ground locating module that control in housing; Described terrestrial wireless communicating circuit, ground locating module and ground control circuit are electrically connected; Described auto heterodyne controller also comprises the self-timer button be located at and controlled on housing; Described self-timer button and ground control circuit are electrically connected; Described terrestrial wireless communicating circuit is connected with the wireless telecommunications of flight wireless communication line.
Its further technical scheme is: described auto heterodyne controller also comprises the distance setting button be located on control housing, highly sets button and flight path setting button.
Its further technical scheme is: described self-timer button, distance setting button, highly setting button and flight path setting button are mechanical button or electronic touching type I button; Described flight locating module and ground locating module are GPS locating module or the Big Dipper locating module.
Its further technical scheme is: described aircraft body is also provided with the imageing sensor for flight navigation upwards extended.
Its further technical scheme is: described aircraft body is provided with the steady The Cloud Terrace of increasing to downward-extension, and the below of the steady The Cloud Terrace of described increasing is provided with described video camera.The steady The Cloud Terrace of increasing wherein can adopt the supporting structure of XYZ tri-axle rotary type, and is provided with the drive motor of XYZ tri-axle.
Its further technical scheme is: described auto heterodyne controller is provided with the shooting display screen for showing auto heterodyne image.
Its further technical scheme is: described auto heterodyne controller is list structure, is provided with hand grip portion.
A kind of self-timer method of aircraft, the method is provided with self-timer button on ground controller, when aircraft body is in state of flight, press self-timer button, the flight control circuit be provided with in aircraft body is centered by the ground locating information that the ground controller received sends, again according to the flight locating information of aircraft body, control aircraft and carry out around formula flight with center, and control video camera and take pictures continuously and/or make a video recording; Wherein, the auto heterodyne distance of acquiescence, autodyne height and auto heterodyne track is provided with in flight control circuit, when user inputs the parameter of auto heterodyne distance, auto heterodyne height and auto heterodyne track by ground controller, preserve in the storer that the control circuit that extremely flown by these parameter transmission is provided with.
Its further technical scheme is: at least comprise two auto heterodyne steps, and after autodyning for the first time, aircraft is in floating state; Ground controller is received primary auto heterodyne image and is shown by display screen, operating personnel by the distance that is provided with setting button, highly set button and flight path and set after button carries out the amendment of parameter, again press self-timer button, start second time and autodyne.
Its further technical scheme is: auto heterodyne process at least comprises two circumference, and the shape that helically rises; The flight path of aircraft body is oval or circular in the shape of surface level; Ground controller is provided with the lead angle button for adjusting spiral gradient.
The present invention's beneficial effect is compared with prior art: the present invention autodyne aircraft adopt ground controller be auto heterodyne controller, be provided with special self-timer button, after auto heterodyne person presses self-timer button, the intrinsic flight control circuit of aircraft, can according to the locating information of the ground locating module received, can carry out taking pictures or making a video recording round auto heterodyne controller with certain flight path (such as square, triangle, circle or ellipse), reach the object of auto heterodyne.Owing to being provided with self-timer button, operating in a key, very simply.Flight path can also be set in advance, and the parameter such as height and distance.The self-timer method of a kind of aircraft of the present invention can adopt the auto heterodyne step of more than secondary, and centre can change parameter, carries out shooting again, to improve the effect of auto heterodyne, without the need to allow aircraft land after again to take off shooting, save time.The self-timer method of a kind of aircraft of the present invention can also adopt spiralling flight path, makes to take the photo that comes or video has more visual angle.
Below in conjunction with the drawings and specific embodiments, the invention will be further described.
Accompanying drawing explanation
Fig. 1 is the using state schematic diagram of a kind of type aircraft specific embodiment of autodyning of the present invention;
Fig. 2 is the circuit structure block scheme of a kind of type aircraft specific embodiment of autodyning of the present invention;
Fig. 3 is the floor map of the auto heterodyne controller of a kind of type aircraft specific embodiment of autodyning of the present invention.
Reference numeral
10 aircraft bodies 11 fly control circuit
12 flight locating module 13 video cameras
14 flight wireless communication lines 20 are autodyned controller
201 hand grip portions 21 control housing
22 ground control circuit 23 terrestrial wireless communicating circuits
24 ground locating module 25 self-timer buttons
26 distance setting buttons 27 highly set button
28 flight paths setting buttons 29 are made a video recording display screen
202 directionkeys
Embodiment
In order to more fully understand technology contents of the present invention, below in conjunction with specific embodiment technical scheme of the present invention being introduced further and illustrating, but being not limited to this.
As shown in Figure 1 to Figure 3, a kind of auto heterodyne type of the present invention aircraft, comprises aircraft body 10, and the ground controller be connected with aircraft body 10 wireless telecommunications; Aircraft body 10 comprise flight control circuit 11, and with flight control circuit 11 be connected flight locating module 12, fly wireless communication module 12 and video camera 13; Ground controller is auto heterodyne controller 20, comprises and controls housing 21, and is provided with the ground control circuit 22, terrestrial wireless communicating circuit 23 and the ground locating module 24 that control in housing 21; Terrestrial wireless communicating circuit 23, ground locating module 24 are electrically connected with ground control circuit 22; Auto heterodyne controller 20 also comprises the self-timer button 25 be located at and controlled on housing 21; Self-timer button 25 and ground control circuit 22 are electrically connected; Terrestrial wireless communicating circuit 23 is connected with the wireless telecommunications of flight wireless communication line 14.When aircraft body is in airflight state, aircraft control people handles auto heterodyne controller, press self-timer button, executor (controller of namely autodyning) sends positional information to aircraft (i.e. aircraft body), flying vehicles control circuit controls aircraft body around its position one week according to its positional information, and is taken pictures continuously or make a video recording in this position of camera alignment, the object of souvenir thus realization manipulation people (i.e. auto heterodyne person) is taken pictures.Store the auto heterodyne parameter (i.e. distance, height and track) of acquiescence in flight control circuit, after each flight is autodyned, the auto heterodyne parameter set can be kept in flight control circuit.Aircraft body 10 is provided with the steady The Cloud Terrace 15 of increasing to downward-extension, and the below increasing steady The Cloud Terrace 15 is provided with described video camera.The steady The Cloud Terrace of increasing wherein can adopt the supporting structure of XYZ tri-axle rotary type, and is provided with the drive motor of XYZ tri-axle, to realize the adjustment of the camera angle to video camera.
Auto heterodyne controller 20 also comprises is located at distance setting button 26 (can be set as air line distance therebetween, also can be set as the distance of horizontal direction therebetween) controlled on housing 21, highly setting button 27 (namely between aircraft body and auto heterodyne controller in the distance of vertical direction) and flight path sets button 28 (such as can be set as circle, ellipse, triangle or tetragonal flight path).Also be provided with the directionkeys 202 for controlling heading, lifting key 203, decline key 204 and initiate key 205.
Wherein, self-timer button, distance setting button, highly setting button and flight path setting button can be mechanical button or electronic touching type I button.Flight locating module and ground locating module also can be GPS locating module or the Big Dipper locating module.
As shown in Figure 3, auto heterodyne controller 20 is also provided with the shooting display screen 29 for showing auto heterodyne image, auto heterodyne controller 20 is list structure, be provided with the hand grip portion 201 (self-timer button 25 is wherein also close to lower end) being positioned at lower end, person grips to be easy to auto heterodyne, and operates with one hand.
In other embodiment, aircraft body is also provided with the imageing sensor for flight navigation upwards extended, and navigator display is provided with on auto heterodyne controller, the image in aircraft front is shown during for flying, because the heading of aircraft can change, therefore, imageing sensor is the top being fixed on aircraft body by rotating mechanism.This rotating mechanism is electrically connected with flight control circuit, is controlled by flight control circuit.In other embodiment, auto heterodyne controller also can be allowed only to be provided with a display screen, by arranging a display switching push button, the displaying contents of display screen be switched, switches between navigation picture and photographed images.
In other embodiment, auto heterodyne controller also can adopt other structure, does not such as arrange display screen; Again such as, distance setting button, highly setting button and flight path setting button are replaced realizing by numerical key.
In other embodiment, ground controller (controller of namely autodyning) also can be provided with the lead angle button for adjusting spiral gradient.
The self-timer method of a kind of aircraft of the present invention, the method is provided with self-timer button on ground controller, when aircraft body is in state of flight, press self-timer button, the flight control circuit be provided with in aircraft body is centered by the ground locating information that the ground controller received sends, again according to the flight locating information of aircraft body, control aircraft and carry out around formula flight with center, and control video camera and take pictures continuously and/or make a video recording; Wherein, the auto heterodyne distance of acquiescence, autodyne height and auto heterodyne track is provided with in flight control circuit, when user inputs the parameter of auto heterodyne distance, auto heterodyne height and auto heterodyne track by ground controller, preserve in the storer that the control circuit that extremely flown by these parameter transmission is provided with.
As concrete auto heterodyne process, method one can be adopted:
At least comprise two auto heterodyne steps, after autodyning for the first time, aircraft is in floating state; Ground controller is received primary auto heterodyne image and is shown by display screen, operating personnel by the distance that is provided with setting button, highly set button and flight path and set after button carries out the amendment of parameter, again press self-timer button, start second time and autodyne.
Also method two can be adopted:
Auto heterodyne process at least comprises two circumference, and the shape that helically rises; The flight path of aircraft body is oval or circular in the shape of surface level; Ground controller is provided with the lead angle button for adjusting spiral gradient.
Also method one and method two can be combined and apply, more than secondary of namely can autodyning, process of at every turn autodyning, comprises the circumference of more than secondary around flight; After each bat is complete, after having seen image by operating personnel, carry out the adjustment of parameter again.
In sum, the present invention autodyne aircraft adopt ground controller be auto heterodyne controller, be provided with special self-timer button, after auto heterodyne person presses self-timer button, the intrinsic flight control circuit of aircraft, according to the locating information of the ground locating module received, can carry out taking pictures or making a video recording round auto heterodyne controller with certain flight path (such as square, triangle, circle or ellipse), reach the object of auto heterodyne.Owing to being provided with self-timer button, operating in a key, very simply.Flight path can also be set in advance, and the parameter such as height and distance.The self-timer method of a kind of aircraft of the present invention can adopt the auto heterodyne step of more than secondary, and centre can change parameter, carries out shooting again, to improve the effect of auto heterodyne, without the need to allow aircraft land after again to take off shooting, save time.The self-timer method of a kind of aircraft of the present invention can also adopt spiralling flight path, makes to take the photo that comes or video has more visual angle.
Above-mentionedly only further illustrate technology contents of the present invention with embodiment, so that reader is easier to understand, but does not represent embodiments of the present invention and be only limitted to this, any technology done according to the present invention extends or recreation, all by protection of the present invention.Protection scope of the present invention is as the criterion with claims.
Claims (10)
1. an auto heterodyne type aircraft, comprises aircraft body, and the ground controller be connected with the wireless telecommunications of aircraft body; It is characterized in that described aircraft body comprises flight control circuit, and with flight control circuit be connected flight locating module, fly wireless communication module and video camera; Described ground controller is auto heterodyne controller, comprises control housing, and is provided with the ground control circuit, terrestrial wireless communicating circuit and the ground locating module that control in housing; Described terrestrial wireless communicating circuit, ground locating module and ground control circuit are electrically connected; Described auto heterodyne controller also comprises the self-timer button be located at and controlled on housing; Described self-timer button and ground control circuit are electrically connected; Described terrestrial wireless communicating circuit is connected with the wireless telecommunications of flight wireless communication line.
2. a kind of auto heterodyne type aircraft according to claim 1, is characterized in that described auto heterodyne controller also comprises the distance setting button be located on control housing, highly sets button and flight path setting button.
3. a kind of auto heterodyne type aircraft according to claim 2, is characterized in that described self-timer button, distance setting button, highly setting button and flight path setting button are mechanical button or electronic touching type I button; Described flight locating module and ground locating module are GPS locating module or the Big Dipper locating module.
4. a kind of auto heterodyne type aircraft according to claim 1, is characterized in that described aircraft body is also provided with the imageing sensor for flight navigation upwards extended.
5. a kind of auto heterodyne type aircraft according to claim 1, it is characterized in that a kind of auto heterodyne type aircraft according to claim 1, it is characterized in that described aircraft body is provided with the steady The Cloud Terrace of increasing to downward-extension, the below of the steady The Cloud Terrace of described increasing is provided with described video camera.
6. a kind of auto heterodyne type aircraft according to claim 1, is characterized in that described auto heterodyne controller is provided with the shooting display screen for showing auto heterodyne image.
7. a kind of auto heterodyne type aircraft according to claim 1, is characterized in that described auto heterodyne controller is list structure, is provided with hand grip portion.
8. the self-timer method of an aircraft, the method is provided with self-timer button on ground controller, when aircraft body is in state of flight, press self-timer button, the flight control circuit be provided with in aircraft body is centered by the ground locating information that the ground controller received sends, again according to the flight locating information of aircraft body, control aircraft and carry out around formula flight with center, and control video camera and take pictures continuously and/or make a video recording; Wherein, the auto heterodyne distance of acquiescence, autodyne height and auto heterodyne track is provided with in flight control circuit, when user inputs the parameter of auto heterodyne distance, auto heterodyne height and auto heterodyne track by ground controller, preserve in the storer that the control circuit that extremely flown by these parameter transmission is provided with.
9. self-timer method according to claim 8, is characterized in that at least comprising two auto heterodyne steps, and after autodyning for the first time, aircraft is in floating state; Ground controller is received primary auto heterodyne image and is shown by display screen, operating personnel by the distance that is provided with setting button, highly set button and flight path and set after button carries out the amendment of parameter, again press self-timer button, start second time and autodyne.
10. self-timer method according to claim 8, is characterized in that auto heterodyne process at least comprises two circumference, and the shape that helically rises; The flight path of aircraft body is oval or circular in the shape of surface level; Ground controller is provided with the lead angle button for adjusting spiral gradient.
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| CN201410855994.5A CN104516355A (en) | 2014-12-31 | 2014-12-31 | Self-photographing aircraft and self-photographing method thereof |
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| CN201410855994.5A CN104516355A (en) | 2014-12-31 | 2014-12-31 | Self-photographing aircraft and self-photographing method thereof |
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| CN104516355A true CN104516355A (en) | 2015-04-15 |
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| CN104820432A (en) * | 2015-05-13 | 2015-08-05 | 张�杰 | Unmanned plane wristwatch type controller |
| CN104991562A (en) * | 2015-05-05 | 2015-10-21 | 杨珊珊 | Aircraft operating system, aircraft method control method and aircraft |
| CN105045282A (en) * | 2015-08-19 | 2015-11-11 | 无锡觅睿恪科技有限公司 | Control system of aircraft |
| CN105159321A (en) * | 2015-08-18 | 2015-12-16 | 北京奇虎科技有限公司 | Unmanned aerial vehicle-based photographing method and unmanned aerial vehicle |
| CN105589466A (en) * | 2016-02-24 | 2016-05-18 | 谭圆圆 | Flight control device of unmanned aircraft and flight control method thereof |
| CN105607647A (en) * | 2016-02-25 | 2016-05-25 | 谭圆圆 | Shooting scope adjusting system of aerial equipment and corresponding adjusting method |
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| CN107600412A (en) * | 2017-09-06 | 2018-01-19 | 佛山市道道电子科技有限公司 | A kind of self-timer unmanned plane |
| CN107765709A (en) * | 2016-08-22 | 2018-03-06 | 广州亿航智能技术有限公司 | The method and device of self-timer is realized based on aircraft |
| CN109479090A (en) * | 2017-12-22 | 2019-03-15 | 深圳市大疆创新科技有限公司 | Information processing method, unmanned plane, remote control equipment and non-volatile memory medium |
| CN109835486A (en) * | 2019-03-13 | 2019-06-04 | 李良杰 | Wired unmanned plane self-timer |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101142122A (en) * | 2005-03-18 | 2008-03-12 | 雅马哈发动机株式会社 | Flight control system |
| CN201217501Y (en) * | 2008-06-13 | 2009-04-08 | 金笛 | Suspending type aviation camera shooting self-determination aircraft system |
| CN101592955A (en) * | 2009-04-08 | 2009-12-02 | 孙卓 | A kind of full-automatic unmanned aerial vehicle control system |
| CN102156481A (en) * | 2011-01-24 | 2011-08-17 | 广州嘉崎智能科技有限公司 | Intelligent tracking control method and system for unmanned aircraft |
| CN203064201U (en) * | 2012-12-28 | 2013-07-17 | 贵州斯凯威科技有限公司 | Aerial photo aircraft |
| CN203315750U (en) * | 2013-06-09 | 2013-12-04 | 北京虎渡能源科技有限公司 | Flight entertainment project control platform |
| 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 |
| CN204331468U (en) * | 2014-12-31 | 2015-05-13 | 深圳雷柏科技股份有限公司 | A kind of auto heterodyne type aircraft |
-
2014
- 2014-12-31 CN CN201410855994.5A patent/CN104516355A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101142122A (en) * | 2005-03-18 | 2008-03-12 | 雅马哈发动机株式会社 | Flight control system |
| CN201217501Y (en) * | 2008-06-13 | 2009-04-08 | 金笛 | Suspending type aviation camera shooting self-determination aircraft system |
| CN101592955A (en) * | 2009-04-08 | 2009-12-02 | 孙卓 | A kind of full-automatic unmanned aerial vehicle control system |
| CN102156481A (en) * | 2011-01-24 | 2011-08-17 | 广州嘉崎智能科技有限公司 | Intelligent tracking control method and system for unmanned aircraft |
| CN203064201U (en) * | 2012-12-28 | 2013-07-17 | 贵州斯凯威科技有限公司 | Aerial photo aircraft |
| CN203315750U (en) * | 2013-06-09 | 2013-12-04 | 北京虎渡能源科技有限公司 | Flight entertainment project control platform |
| 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 |
| CN204331468U (en) * | 2014-12-31 | 2015-05-13 | 深圳雷柏科技股份有限公司 | A kind of auto heterodyne type aircraft |
Cited By (20)
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|---|---|---|---|---|
| CN106292720A (en) * | 2015-04-21 | 2017-01-04 | 高域（北京）智能科技研究院有限公司 | A kind of intelligent multi-control flight capture apparatus and flight control method thereof |
| CN104991562A (en) * | 2015-05-05 | 2015-10-21 | 杨珊珊 | Aircraft operating system, aircraft method control method and aircraft |
| CN104820432A (en) * | 2015-05-13 | 2015-08-05 | 张�杰 | Unmanned plane wristwatch type controller |
| WO2016179916A1 (en) * | 2015-05-13 | 2016-11-17 | 张�杰 | Wrist watch type controller of unmanned aerial vehicle |
| CN105159321B (en) * | 2015-08-18 | 2019-02-26 | 北京奇虎科技有限公司 | A kind of photographic method and unmanned vehicle based on unmanned vehicle |
| CN105159321A (en) * | 2015-08-18 | 2015-12-16 | 北京奇虎科技有限公司 | Unmanned aerial vehicle-based photographing method and unmanned aerial vehicle |
| CN105045282A (en) * | 2015-08-19 | 2015-11-11 | 无锡觅睿恪科技有限公司 | Control system of aircraft |
| CN106899798A (en) * | 2015-12-18 | 2017-06-27 | 林其禹 | Self-photographing unmanned aerial vehicle system and execution method thereof |
| CN106899798B (en) * | 2015-12-18 | 2020-02-07 | 林其禹 | Self-photographing unmanned aerial vehicle system and execution method thereof |
| CN105589466A (en) * | 2016-02-24 | 2016-05-18 | 谭圆圆 | Flight control device of unmanned aircraft and flight control method thereof |
| CN105607647A (en) * | 2016-02-25 | 2016-05-25 | 谭圆圆 | Shooting scope adjusting system of aerial equipment and corresponding adjusting method |
| CN107765709A (en) * | 2016-08-22 | 2018-03-06 | 广州亿航智能技术有限公司 | The method and device of self-timer is realized based on aircraft |
| CN107765709B (en) * | 2016-08-22 | 2021-12-31 | 广州亿航智能技术有限公司 | Method and device for realizing self-shooting based on aircraft |
| CN107589691A (en) * | 2017-08-11 | 2018-01-16 | 北京小米移动软件有限公司 | The filming control method and device of unmanned plane |
| CN107600412A (en) * | 2017-09-06 | 2018-01-19 | 佛山市道道电子科技有限公司 | A kind of self-timer unmanned plane |
| CN109479090A (en) * | 2017-12-22 | 2019-03-15 | 深圳市大疆创新科技有限公司 | Information processing method, unmanned plane, remote control equipment and non-volatile memory medium |
| WO2020062163A1 (en) * | 2018-09-29 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Method for controlling pan-tilt, and handheld pan-tilt and handheld device |
| CN109835486A (en) * | 2019-03-13 | 2019-06-04 | 李良杰 | Wired unmanned plane self-timer |
| CN112621766A (en) * | 2021-03-09 | 2021-04-09 | 常州微亿智造科技有限公司 | Flying shooting image error prediction method based on machine learning |
| CN112621766B (en) * | 2021-03-09 | 2021-05-18 | 常州微亿智造科技有限公司 | Flying shooting image error prediction method based on machine learning |
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Application publication date: 20150415 |