CN108073184B - Unmanned aerial vehicle flight control method and device - Google Patents

Unmanned aerial vehicle flight control method and device Download PDF

Info

Publication number
CN108073184B
CN108073184B CN201711205873.6A CN201711205873A CN108073184B CN 108073184 B CN108073184 B CN 108073184B CN 201711205873 A CN201711205873 A CN 201711205873A CN 108073184 B CN108073184 B CN 108073184B
Authority
CN
China
Prior art keywords
flight direction
unmanned aerial
aerial vehicle
flight
picture
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.)
Active
Application number
CN201711205873.6A
Other languages
Chinese (zh)
Other versions
CN108073184A (en
Inventor
张存
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.)
Beijing Lajin Zhongbo Technology Co ltd
Original Assignee
Beijing Lajin Zhongbo Technology Co ltd
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 Beijing Lajin Zhongbo Technology Co ltd filed Critical Beijing Lajin Zhongbo Technology Co ltd
Priority to CN201711205873.6A priority Critical patent/CN108073184B/en
Publication of CN108073184A publication Critical patent/CN108073184A/en
Application granted granted Critical
Publication of CN108073184B publication Critical patent/CN108073184B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

Abstract

The invention relates to a flight control method and a flight control device for an unmanned aerial vehicle. The method comprises the following steps: acquiring pre-stored pictures from a pre-stored picture group in sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged in sequence; comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result; determining a first flight direction corresponding to the current picture according to the comparison result; and controlling the unmanned aerial vehicle to fly according to the first flight direction. According to the technical scheme, the flight accuracy of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is prevented from failing to fly due to the fact that the flight direction cannot be determined.

Description

Unmanned aerial vehicle flight control method and device
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle flight control method and device.
Background
Unmanned aerial vehicles, abbreviated as "unmanned aerial vehicles", abbreviated as "UAVs", are unmanned aerial vehicles that are operated by means of radio remote control devices and self-contained programmed control devices, or are operated autonomously, either entirely or intermittently, by an onboard computer. Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirement for battle environment, strong battlefield survivability, etc. The unmanned aerial vehicle is generally provided with a GPS positioning system, so that the unmanned aerial vehicle can fly by presetting a flight track, execute shooting tasks and the like.
Disclosure of Invention
The embodiment of the invention provides a method and a device for controlling unmanned aerial vehicle flight. The technical scheme is as follows:
according to a first aspect of an embodiment of the present invention, there is provided a method for controlling flight of an unmanned aerial vehicle, including
Acquiring pre-stored pictures from a pre-stored picture group in sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged in sequence;
comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result;
determining a first flight direction corresponding to the current picture according to the comparison result;
and controlling the unmanned aerial vehicle to fly according to the first flight direction.
In another embodiment, comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result includes:
calculating the matching degree of the current picture and the pre-stored picture;
determining a first flight direction corresponding to the current picture according to the comparison result, wherein the determining comprises the following steps:
and when the matching degree of the current picture and the pre-stored picture is larger than or equal to a preset threshold value, determining the shooting direction corresponding to the current picture as a first flight direction.
In another embodiment, the determining, according to the comparison result, the first flight direction corresponding to the current picture includes:
and when the matching degree of the current picture and the pre-stored picture is smaller than a preset threshold value, determining that the first flight direction is the flight starting point of the returned unmanned aerial vehicle.
In another embodiment, controlling the unmanned aerial vehicle to fly according to the first flight direction includes:
when a GPS signal exists currently, acquiring preset navigation data and current position information;
judging whether the first flight direction is correct or not according to the navigation data and the current position information;
and when the first flight direction is correct, controlling the unmanned aerial vehicle to fly according to the first flight direction.
In another embodiment, controlling the unmanned aerial vehicle to fly according to the first flight direction further comprises:
when the first flight direction is incorrect, correcting the first flight direction according to the navigation data and the current position information to obtain a second flight direction;
and controlling the unmanned aerial vehicle to fly according to the second flight direction.
According to a second aspect of an embodiment of the present invention, there is provided an unmanned aerial vehicle flight control apparatus including:
the acquisition module is used for acquiring pre-stored pictures from a pre-stored picture group in sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged in sequence;
the comparison module is used for comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result;
the determining module is used for determining a first flight direction corresponding to the current picture according to the comparison result;
and the control module is used for controlling the unmanned aerial vehicle to fly according to the first flight direction.
In another embodiment, the comparison module is configured to calculate a matching degree between the current picture and the pre-stored picture;
the determining module is configured to determine, when the matching degree between the current picture and the pre-stored picture is greater than or equal to a preset threshold, that the shooting direction corresponding to the current picture is a first flight direction.
In another embodiment, the determining module is configured to determine that the first flight direction is a return unmanned aerial vehicle flight start point when the matching degree of the current picture and the pre-stored picture is smaller than a preset threshold.
In another embodiment, the control module includes:
the acquisition sub-module is used for acquiring preset navigation data and current position information when the GPS signal exists currently;
the judging sub-module is used for judging whether the first flight direction is correct or not according to the navigation data and the current position information;
and the control sub-module is used for controlling the unmanned aerial vehicle to fly according to the first flight direction when the first flight direction is correct.
In another embodiment, the control module further comprises:
the correction sub-module is used for correcting the first flight direction according to the navigation data and the current position information to obtain a second flight direction when the first flight direction is incorrect;
and the control submodule is used for controlling the unmanned aerial vehicle to fly according to the second flight direction.
In this embodiment, because of the influence of hand geographical environment, unmanned aerial vehicle flight in-process, the condition of GPS no signal probably appears, perhaps GPS subassembly trouble on the unmanned aerial vehicle at this moment, confirms the flight direction through the picture with unmanned aerial vehicle shooting with prestore the picture contrast, improves unmanned aerial vehicle flight's accuracy, avoids unmanned aerial vehicle to fly the failure because unable determination flight direction.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention as claimed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.
FIG. 1 is a flow chart illustrating a method of unmanned aerial vehicle flight control according to an exemplary embodiment;
FIG. 2 is a flow chart illustrating a method of unmanned aerial vehicle flight control according to another exemplary embodiment;
FIG. 3 is a block diagram of a drone flight control device, shown according to an example embodiment;
FIG. 4 is a block diagram of control module 34 shown in accordance with an exemplary embodiment;
fig. 5 is a block diagram of control module 34 shown according to another exemplary embodiment.
Detailed Description
Reference will now be made in detail to exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numbers in different drawings refer to the same or similar elements, unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the invention. Rather, they are merely examples of apparatus and methods consistent with aspects of the invention as detailed in the accompanying claims.
Fig. 1 is a flowchart illustrating a method of controlling a flight of a drone, according to an exemplary embodiment, as shown in fig. 1, including the steps of:
step S11, obtaining pre-stored pictures from a pre-stored picture group according to the sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged according to the sequence.
And S12, comparing the current picture obtained by shooting the surrounding environment with a pre-stored picture to obtain a comparison result.
And S13, determining a first flight direction corresponding to the current picture according to the comparison result.
Step S14, controlling the unmanned aerial vehicle to fly according to the first flight direction.
In another embodiment, step S12 includes: and calculating the matching degree of the current picture and the pre-stored picture. The step S13 includes: when the matching degree of the current picture and the pre-stored picture is larger than or equal to a preset threshold value, determining the shooting direction corresponding to the current picture as a first flight direction.
In another embodiment, determining the first flight direction corresponding to the current picture according to the comparison result includes:
when the matching degree of the current picture and the pre-stored picture is smaller than a preset threshold value, determining the first flight direction as a flight starting point of the returned unmanned aerial vehicle.
In this embodiment, in the unmanned aerial vehicle flight process, control unmanned aerial vehicle is photographed around to, compares the photo of taking with prestored picture to confirm unmanned aerial vehicle flight direction. When the shot picture is matched with the pre-stored picture, the current flight direction of the unmanned aerial vehicle strives for, the unmanned aerial vehicle can continue to fly in the direction, if the current flight direction is not matched with the pre-stored picture, the unmanned aerial vehicle can be controlled to return to the flight starting point.
The embodiment of the invention can be used as an auxiliary positioning mode when the unmanned aerial vehicle does not have GPS signals. Due to the influence of the geographical environment of the hand, the condition that GPS has no signal possibly occurs in the flight process of the unmanned aerial vehicle, or the GPS component on the unmanned aerial vehicle fails, at this time, the flight direction is determined by comparing the picture shot by the unmanned aerial vehicle with the pre-stored picture, the flight accuracy of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is prevented from failing to fly due to the fact that the flight direction cannot be determined.
Fig. 2 is a flowchart illustrating a method of controlling unmanned aerial vehicle flight according to another exemplary embodiment, as shown in fig. 2, in another embodiment, step S14 includes:
step S21, when the GPS signal exists currently, the preset navigation data and the current position information are obtained.
Step S22, judging whether the first flight direction is correct or not according to the navigation data and the current position information, if yes, executing step S23, and if not, executing step S24.
And S23, controlling the unmanned aerial vehicle to fly according to the first flight direction when the first flight direction is correct.
In another embodiment, step S14 further includes:
and S24, correcting the first flight direction according to the navigation data and the current position information to obtain a second flight direction when the first flight direction is incorrect.
And S25, controlling the unmanned aerial vehicle to fly according to the second flight direction.
In this embodiment, the GPS positioning mode and the image comparison mode may be combined to determine the flight direction of the unmanned aerial vehicle, so as to further improve the flight accuracy.
The following are examples of the apparatus of the present invention that may be used to perform the method embodiments of the present invention.
Fig. 3 is a block diagram of a drone flight control apparatus that may be implemented as part or all of an electronic device by software, hardware, or a combination of both, according to an example embodiment. As shown in fig. 3, the unmanned aerial vehicle flight control device includes:
the obtaining module 31 is configured to obtain pre-stored pictures from a pre-stored picture group in sequence, where the pre-stored picture group includes at least two pre-stored pictures arranged in sequence.
The comparison module 32 is configured to compare a current picture obtained by capturing a surrounding environment with a pre-stored picture to obtain a comparison result.
And the determining module 33 is configured to determine a first flight direction corresponding to the current picture according to the comparison result.
The control module 34 is configured to control the unmanned aerial vehicle to fly according to the first flight direction.
In another embodiment, the comparison module 32 is used for calculating the matching degree between the current picture and the pre-stored picture. The determining module 33 is configured to determine, when the matching degree between the current picture and the pre-stored picture is greater than or equal to a preset threshold, that the shooting direction corresponding to the current picture is the first flight direction.
In another embodiment, the determining module 33 is configured to determine the first flight direction as the return unmanned aerial vehicle flight start point when the matching degree between the current picture and the pre-stored picture is less than a preset threshold.
FIG. 4 is a block diagram of the control module 34 shown in accordance with an exemplary embodiment, as shown in FIG. 4, the control module 34 includes:
the obtaining sub-module 41 is configured to obtain preset navigation data and current location information when a GPS signal is currently present.
The judging sub-module 42 is configured to judge whether the first flight direction is correct according to the navigation data and the current position information.
And the control sub-module 43 is used for controlling the unmanned aerial vehicle to fly according to the first flight direction when the first flight direction is correct.
Fig. 5 is a block diagram of the control module 34 shown according to another exemplary embodiment, as shown in fig. 5, the control module 34 further includes: a syndrome module 44.
And the correction sub-module 44 is configured to correct the first flight direction according to the navigation data and the current position information to obtain the second flight direction when the first flight direction is incorrect.
And a control sub-module 43 for controlling the unmanned aerial vehicle to fly according to the second flight direction.
Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the invention and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.
It is to be understood that the invention is not limited to the precise arrangements and instrumentalities shown in the drawings, which have been described above, and that various modifications and changes may be effected without departing from the scope thereof. The scope of the invention is limited only by the appended claims.

Claims (8)

1. A flight control method of an unmanned aerial vehicle is characterized in that,
comprising the following steps:
acquiring pre-stored pictures from a pre-stored picture group in sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged in sequence;
comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result, and further comprising;
calculating the matching degree of the current picture and the pre-stored picture;
determining a first flight direction corresponding to the current picture according to the comparison result, wherein the determining comprises the following steps:
when the matching degree of the current picture and the pre-stored picture is larger than or equal to a preset threshold value, determining the shooting direction corresponding to the current picture as a first flight direction;
and controlling the unmanned aerial vehicle to fly according to the first flight direction.
2. The method of claim 1, wherein the step of determining the position of the substrate comprises,
the determining, according to the comparison result, a first flight direction corresponding to the current picture includes:
and when the matching degree of the current picture and the pre-stored picture is smaller than a preset threshold value, determining that the first flight direction is the flight starting point of the returned unmanned aerial vehicle.
3. The method of claim 1, wherein the step of determining the position of the substrate comprises,
controlling the unmanned aerial vehicle to fly according to the first flight direction, comprising:
when a GPS signal exists currently, acquiring preset navigation data and current position information;
judging whether the first flight direction is correct or not according to the navigation data and the current position information;
and when the first flight direction is correct, controlling the unmanned aerial vehicle to fly according to the first flight direction.
4. The method of claim 3, wherein the step of,
controlling the unmanned aerial vehicle to fly according to the first flight direction, further comprising:
when the first flight direction is incorrect, correcting the first flight direction according to the navigation data and the current position information to obtain a second flight direction;
and controlling the unmanned aerial vehicle to fly according to the second flight direction.
5. An unmanned aerial vehicle flight control device is characterized in that,
comprising the following steps:
the acquisition module is used for acquiring pre-stored pictures from a pre-stored picture group in sequence, wherein the pre-stored picture group comprises at least two pre-stored pictures arranged in sequence;
the comparison module is used for comparing the current picture obtained by shooting the surrounding environment with the pre-stored picture to obtain a comparison result;
the determining module is used for determining a first flight direction corresponding to the current picture according to the comparison result;
the comparison module is used for calculating the matching degree of the current picture and the pre-stored picture;
the determining module is used for determining that the shooting direction corresponding to the current picture is a first flight direction when the matching degree of the current picture and the pre-stored picture is greater than or equal to a preset threshold value;
and the control module is used for controlling the unmanned aerial vehicle to fly according to the first flight direction.
6. The apparatus of claim 5, wherein the device comprises a plurality of sensors,
the determining module is configured to determine that the first flight direction is a return unmanned aerial vehicle flight starting point when the matching degree of the current picture and the pre-stored picture is smaller than a preset threshold.
7. The apparatus of claim 5, wherein the device comprises a plurality of sensors,
the control module includes:
the acquisition sub-module is used for acquiring preset navigation data and current position information when the GPS signal exists currently;
the judging sub-module is used for judging whether the first flight direction is correct or not according to the navigation data and the current position information;
and the control sub-module is used for controlling the unmanned aerial vehicle to fly according to the first flight direction when the first flight direction is correct.
8. The apparatus of claim 7, wherein the device comprises a plurality of sensors,
the control module further includes:
the correction sub-module is used for correcting the first flight direction according to the navigation data and the current position information to obtain a second flight direction when the first flight direction is incorrect;
and the control submodule is used for controlling the unmanned aerial vehicle to fly according to the second flight direction.
CN201711205873.6A 2017-11-27 2017-11-27 Unmanned aerial vehicle flight control method and device Active CN108073184B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711205873.6A CN108073184B (en) 2017-11-27 2017-11-27 Unmanned aerial vehicle flight control method and device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711205873.6A CN108073184B (en) 2017-11-27 2017-11-27 Unmanned aerial vehicle flight control method and device

Publications (2)

Publication Number Publication Date
CN108073184A CN108073184A (en) 2018-05-25
CN108073184B true CN108073184B (en) 2024-02-20

Family

ID=62157255

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711205873.6A Active CN108073184B (en) 2017-11-27 2017-11-27 Unmanned aerial vehicle flight control method and device

Country Status (1)

Country Link
CN (1) CN108073184B (en)

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004333243A (en) * 2003-05-06 2004-11-25 Pasuko:Kk Method for matching image
JP2010140246A (en) * 2008-12-11 2010-06-24 Yaskawa Electric Corp Moving object
JP2011215052A (en) * 2010-03-31 2011-10-27 Aisin Aw Co Ltd Own-vehicle position detection system using scenic image recognition
CN102853835A (en) * 2012-08-15 2013-01-02 西北工业大学 Scale invariant feature transform-based unmanned aerial vehicle scene matching positioning method
CN103245948A (en) * 2012-02-09 2013-08-14 中国科学院电子学研究所 Image match navigation method for double-area image formation synthetic aperture radars
WO2014079632A1 (en) * 2012-11-26 2014-05-30 Robert Bosch Gmbh Autonomous transportation device
CN106054927A (en) * 2016-08-04 2016-10-26 北方民族大学 Intelligent channel tour-inspection device and system based on UAV (Unmanned Aerial Vehicle) and measurement method
CN106292685A (en) * 2015-05-20 2017-01-04 优利科技有限公司 The model of an airplane and flight control method thereof and system
WO2017000875A1 (en) * 2015-06-29 2017-01-05 优利科技有限公司 Aircraft and obstacle avoidance method and system thereof
WO2017080108A1 (en) * 2015-11-13 2017-05-18 深圳市道通智能航空技术有限公司 Flying device, flying control system and method
CN106778587A (en) * 2016-12-09 2017-05-31 国家测绘地理信息局四川测绘产品质量监督检验站 State of flight detection method and device based on unmanned plane image
CN107031523A (en) * 2015-11-30 2017-08-11 法乐第未来公司 The vehicle location based on camera is carried out using known target to determine
CN107356255A (en) * 2017-06-30 2017-11-17 北京臻迪科技股份有限公司 A kind of Navigation of Pilotless Aircraft method and device

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004333243A (en) * 2003-05-06 2004-11-25 Pasuko:Kk Method for matching image
JP2010140246A (en) * 2008-12-11 2010-06-24 Yaskawa Electric Corp Moving object
JP2011215052A (en) * 2010-03-31 2011-10-27 Aisin Aw Co Ltd Own-vehicle position detection system using scenic image recognition
CN103245948A (en) * 2012-02-09 2013-08-14 中国科学院电子学研究所 Image match navigation method for double-area image formation synthetic aperture radars
CN102853835A (en) * 2012-08-15 2013-01-02 西北工业大学 Scale invariant feature transform-based unmanned aerial vehicle scene matching positioning method
WO2014079632A1 (en) * 2012-11-26 2014-05-30 Robert Bosch Gmbh Autonomous transportation device
CN106292685A (en) * 2015-05-20 2017-01-04 优利科技有限公司 The model of an airplane and flight control method thereof and system
WO2017000875A1 (en) * 2015-06-29 2017-01-05 优利科技有限公司 Aircraft and obstacle avoidance method and system thereof
WO2017080108A1 (en) * 2015-11-13 2017-05-18 深圳市道通智能航空技术有限公司 Flying device, flying control system and method
CN107031523A (en) * 2015-11-30 2017-08-11 法乐第未来公司 The vehicle location based on camera is carried out using known target to determine
CN106054927A (en) * 2016-08-04 2016-10-26 北方民族大学 Intelligent channel tour-inspection device and system based on UAV (Unmanned Aerial Vehicle) and measurement method
CN106778587A (en) * 2016-12-09 2017-05-31 国家测绘地理信息局四川测绘产品质量监督检验站 State of flight detection method and device based on unmanned plane image
CN107356255A (en) * 2017-06-30 2017-11-17 北京臻迪科技股份有限公司 A kind of Navigation of Pilotless Aircraft method and device

Also Published As

Publication number Publication date
CN108073184A (en) 2018-05-25

Similar Documents

Publication Publication Date Title
US10273000B2 (en) Control of image triggering for aerial image capturing in nadir alignment for an unmanned aircraft
US9188979B2 (en) Method and system for remotely controlling a vehicle
US20190019051A1 (en) Unmanned mobile apparatus capable of transferring imaging, method of transferring
US20200191556A1 (en) Distance mesurement method by an unmanned aerial vehicle (uav) and uav
US11962375B2 (en) Geolocation-based beamforming for drone communication
CN107783555B (en) Target positioning method, device and system based on unmanned aerial vehicle
US20120221180A1 (en) Unmanned aerial vehicle and control method thereof
KR102187963B1 (en) Method and device of correcting image sensor misalignment using ship identification information
KR102040289B1 (en) Apparatus and method for correcting position of drone
US11605181B2 (en) Control apparatus, control system and control method
US10557718B2 (en) Auxiliary control method and system for unmanned aerial vehicle
WO2018152273A1 (en) Probabilistic landmark navigation (pln) system
CN108073184B (en) Unmanned aerial vehicle flight control method and device
WO2017047118A1 (en) Base station design assistance system using unmanned aerial vehicle, and server used in this system
KR101911353B1 (en) Autonomic flight method when gnss signal loss and unmanned aerial vehicle for the same
KR102258731B1 (en) System and method for controlling flight sequence of unmanned aerial vehicle
JP2016182880A (en) Flight control device of unmanned aircraft, flight control method for unmanned aircraft, and flight control program for unmanned aircraft
KR102238628B1 (en) Vessel backup navigation system using uav in radio interference environment and its method
JP2015193347A (en) Inertia navigation system of missile
US10598495B2 (en) Method for designing a navigation path and method for orienting a sighting member from said navigation path
KR20230032174A (en) Unmanned aerial vehicle formation flight control system and method thereof
Lukashevich et al. The new approach for reliable UAV navigation based on onboard camera image processing
US10338607B2 (en) Unmanned aerial vehicle and method for positioning an unmanned aerial vehicle
KR102609467B1 (en) Automatic flight method using image based navigation in GNSS abnormal situations
KR101747335B1 (en) POV shot by Quad ropteo automatic way and it has a camera mounted POV-oriented member function

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right

Effective date of registration: 20220927

Address after: Room 1602, 16th Floor, Building 18, Yard 6, Wenhuayuan West Road, Beijing Economic and Technological Development Zone, Daxing District, Beijing 100176

Applicant after: Beijing Lajin Zhongbo Technology Co.,Ltd.

Address before: Room 808, Block E, Yonghe Building, No. 28 Andingmen East Street, Dongcheng District, Beijing 100007

Applicant before: TVMINING (BEIJING) MEDIA TECHNOLOGY Co.,Ltd.

TA01 Transfer of patent application right
GR01 Patent grant
GR01 Patent grant