CN105947201A - Modularized unmanned aerial vehicle and use method thereof - Google Patents
Modularized unmanned aerial vehicle and use method thereof Download PDFInfo
- Publication number
- CN105947201A CN105947201A CN201610269708.6A CN201610269708A CN105947201A CN 105947201 A CN105947201 A CN 105947201A CN 201610269708 A CN201610269708 A CN 201610269708A CN 105947201 A CN105947201 A CN 105947201A
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- functional module
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- unmanned plane
- intelligent terminal
- modularized
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- 238000000034 method Methods 0.000 title claims abstract description 25
- 238000001179 sorption measurement Methods 0.000 claims abstract description 18
- 230000006870 function Effects 0.000 claims description 22
- 208000007623 Lordosis Diseases 0.000 claims description 9
- 241000256844 Apis mellifera Species 0.000 claims description 3
- 238000012790 confirmation Methods 0.000 claims description 3
- 230000007613 environmental effect Effects 0.000 claims description 3
- 230000000875 corresponding effect Effects 0.000 description 13
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000002596 correlated effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 241000222065 Lycoperdon Species 0.000 description 1
- 241000768494 Polymorphum Species 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004899 motility Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/048—Monitoring; Safety
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
Abstract
The invention relates to the technical field of unmanned aerial vehicles, and provides a modularized unmanned aerial vehicle (UAV) and a use method thereof, wherein the modularized UAV includes a UAV body and one or more functional modules. The UAV body includes an MCU, a wireless signal transmitting-receiving module, and one or more functional components of a gyroscope, an indication light and a buzzer; the UAV body is provided with one or more adsorption magnets used for adsorbing corresponding adsorption magnets on different functional modules so as to complete fixation of the functional modules; the functional modules comprise one or more functional modules of cameras with various specifications, spiral wings with various specifications, battery packs with various specifications and auxiliary modules with various specifications. The modularized UAV provided by the embodiment of the invention can be freely assembled and completes personal customization based on adsorption magnets for fixing the structure and a standard uniform interface assembly mode.
Description
[technical field]
The present invention relates to unmanned air vehicle technique field, particularly relate to a kind of Modularized unmanned machine and using method thereof.
[background technology]
UAV is called for short " unmanned plane ", is that one is filled by radio robot or self programme-control
Put the unmanned vehicle of operation, come across the forties in 20th century the earliest.Both at home and abroad unmanned plane is correlated with skill
Art develops rapidly, and UAS is of a great variety, the wide distinct characteristics of purposes, cause its size, quality,
Voyage, boat time, flying height, flight speed, task dispatching many-side has larger difference.Due to unmanned plane
Multiformity, have different sorting techniques for different considering:
Classifying by flying platform configuration, unmanned plane can be divided into fixed-wing unmanned plane, rotor wing unmanned aerial vehicle, nobody flies
Ship, umbrella wing unmanned plane, flapping wing unmanned plane etc..And the simplification that wherein rotor wing unmanned aerial vehicle manipulates due to it and
Hovering top grade is specific, is widely used in and takes photo by plane, transports the field such as express delivery, rescue and relief work.Along with rotor
The raising of the civilian universal rate of unmanned plane, the flying power of unmanned plane and its abundant functional characteristic are more come
More multi-user is paid attention to, and the unmanned plane of subsidiary different plug-in parts also arises at the historic moment.But, in prior art
A kind of a whole set of solution proposed for different application environment.
In consideration of it, overcoming the defect existing for the prior art is the art problem demanding prompt solution.
[summary of the invention]
The technical problem to be solved in the present invention is a kind of for the proposition of different application environment in prior art
A whole set of solution, be generally both for designed by general field, lack motility.
The present invention adopts the following technical scheme that
First aspect, embodiments provides a kind of Modularized unmanned machine, including unmanned plane body, and one
Individual or multiple functional modules are concrete:
Described unmanned plane body includes MCU and wireless signal transceiver module, and gyroscope, display lamp and honeybee
One or more functional unit in ring device；
It is provided with one or more adsorption magnet on described unmanned plane body, is used for and difference in functionality module
Corresponding adsorption magnet adsorb, thus complete the fixing of functional module；Wherein, described Functional Module
Include the auxiliary of the photographic head of plurality of specifications, the screw wing of plurality of specifications, the set of cells of plurality of specifications and plurality of specifications
Help one or more functional modules in module.
Preferably, one or more functional module and corresponding attachment structure on unmanned plane body, specifically
For a kind of notch pushed from top to bottom, from the bottom to top, from left to right and/or from right to left, function mould
Its connection interface of block specially can embed described notch, and based on self and the absorption of unmanned plane body
Magnet completes the structure fixed.
Preferably, one or more functional module and corresponding attachment structure on unmanned plane body, specially without
Interface groove is set on man-machine body；The interface position of one or more functional module arranges lordosis,
Described lordosis is used for inserting described groove；Wherein, on described lordosis and groove, contact position is provided with absorption magnetic
Ferrum.
Preferably, one or more functional module and corresponding attachment structure on unmanned plane body, between number
Thimble structure or elastic piece structure is used according to interface.
On the other hand, the embodiment of the present invention additionally provides a kind of Modularized unmanned machine using method, described use
Method includes:
The relevant information currently without man-machine application scenario of intelligent terminal for reception operator input；
Intelligent terminal calculates the functional module configuration strategy meeting current application occasion；
Intelligent terminal feeds back one or more optional function module configuration strategy to operator, in order to operation
Personnel selection suitably configures the assembling that strategy completes the functional module of unmanned plane.
Preferably, in the relevant information currently without man-machine application scenario of intelligent terminal for reception operator input
Before, also include:
The unmanned plane body information of intelligent terminal for reception operator input and one or more merit having been provided with
Energy module information, described one or more functional module information having been provided with is imported data base by intelligent terminal；
Then intelligent terminal feeds back one or more optional function module configuration strategy to operator, specifically also
Including:
Described intelligent terminal proofreads the functional module needed for each energy module configures strategy and described operator join
One or more standby functional module, and in the way of highlighted, present attainable functional module configuration strategy.
Preferably, the relevant information of described application scenario, specifically include:
One or more in wind speed, cruising time, shooting time, shooting environmental type and style of shooting.
Preferably, described intelligent terminal calculates the functional module configuration strategy meeting current application occasion, tool
Body includes:
Essential functional module type is confirmed according to style of shooting；
Cruising time needed for confirmation, and according to optional battery module capacity, and believed by unmanned plane body
Breath, the weight of each alternative functional module and/or power, be calculated and meet the one of current application occasion
Plant or several functions module configuration strategy；Wherein said each alternative functional module belongs to be confirmed
Essential functional module type.
Preferably, described intelligent terminal feeds back one or more optional function module configuration strategy to operator
Member, also includes:
In described intelligent terminal's feedback server, storage corresponds to one or more optional function mould
The use case of block configuration strategy is to operator；Wherein, described use case includes being made by designer
And the case uploaded onto the server or the case being made by historical operation personnel and uploading onto the server.
Preferably, described intelligent terminal feeds back one or more optional function module configuration strategy to operator
Member, also includes:
Corresponding to various configuration strategies, the use parameter that corresponding display draws during calculating；Wherein, institute
State and use parameter to include the cruising time of various configuration strategy, applicable scene information, be used rate, dominance
In one or more.
Compared with prior art, the beneficial effects of the present invention is: embodiments provide a kind of support
Assembly model in the unified interface of adsorption magnet fixed structure and standard achieves and can freely assemble, and completes
The Modularized unmanned machine of people's customization.For carrying out abundant module trade market future and for application-specific field
The module configuration strategy customization of scape provides feasibility.
[accompanying drawing explanation]
Fig. 1 is a kind of Modularized unmanned machine structural representation that the embodiment of the present invention provides；
Fig. 2 is a kind of Modularized unmanned machine housing construction schematic diagram that the embodiment of the present invention provides；
Fig. 3 is a kind of Modularized unmanned machine battery group modular structure schematic diagram that the embodiment of the present invention provides；
Fig. 4 is a kind of Modularized unmanned machine using method schematic flow sheet that the embodiment of the present invention provides；
Fig. 5 is a kind of Modularized unmanned machine using method schematic flow sheet that the embodiment of the present invention provides.
[detailed description of the invention]
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with accompanying drawing and reality
Execute example, the present invention is further elaborated.Only should be appreciated that specific embodiment described herein
Only in order to explain the present invention, it is not intended to limit the present invention.
As long as additionally, technical characteristic involved in each embodiment of invention described below is each other
Between do not constitute conflict just can be mutually combined.
Embodiment 1:
Embodiments provide a kind of Modularized unmanned machine, as Figure 1-3, described Modularized unmanned
Machine includes unmanned plane body 2, one or more functional module 3, concrete:
Described unmanned plane body includes MCU and wireless signal transceiver module, and gyroscope, display lamp and honeybee
One or more functional unit in ring device；
It is provided with one or more adsorption magnet 31 on described unmanned plane body, is used for and difference in functionality module
On corresponding adsorption magnet adsorb, thus complete the fixing of functional module；Wherein, described functional module
Photographic head, the screw wing of plurality of specifications, the set of cells of plurality of specifications and plurality of specifications including plurality of specifications
One or more functional modules in supplementary module.
Wherein, in conjunction with in the scheme that the embodiment of the present invention is realized, described screw wing can be to use the present invention
Described adsorption magnet structure completes to install, and it is positioned at the mounting seat on unmanned plane body as shown in Figure 2；Also
Can be in the way of being to use screw wing and unmanned plane body to be constituted fixed connection structure, owing to described screw wing is
Optional structure in functional module, therefore, above two implementation is all at the protection model of the embodiment of the present invention
In enclosing.
As described in Figure 3, the structural representation installing set of cells functional module on unmanned plane body is given.
Embodiments provide a kind of group relying on adsorption magnet fixed structure and the unified interface of standard
Die-filling formula achieves and can freely assemble, and completes the Modularized unmanned machine of personal customization.Abundant for carrying out future
Module trade market and the module for application-specific scene configure strategy customization and provide feasibility.
In conjunction with the embodiment of the present invention, for the fixed form of its module, in addition to relying on adsorption magnet, also
Need to coordinate one or more functional module and corresponding attachment structure on unmanned plane body, specially one
The notch kind pushed from top to bottom, from the bottom to top, from left to right and/or from right to left, functional module its
Connect interface and specially can embed described notch, and based on self and the adsorption magnet of unmanned plane body
Complete the structure fixed.Preferably, described notch generally can set up one on the groove edge of functional module
Individual or multiple projections, and corresponding draw-in groove passage relevant position on unmanned plane body arrange one or
Multiple recesses, thus further utilize this projection and recess to strengthen the firm of interface.
In conjunction with the embodiment of the present invention, for the fixed form of its module, in addition to relying on adsorption magnet, also
Need to coordinate one or more functional module and corresponding attachment structure on unmanned plane body, such as Fig. 1 institute
Show, specially on unmanned plane body, interface groove 32 is set；The interface of one or more functional module
Position arranges lordosis (not shown), and described lordosis is used for inserting described groove 32；Wherein, described lordosis
Contact position on groove 32 is provided with adsorption magnet.
For the connection interface of the most unified each module, and simplify band line interface on fuselage, in conjunction with the present invention
Embodiment, it is provided that a kind of preferably implementation, wherein, one or more functional module and unmanned plane machine
Corresponding attachment structure on body, between data-interface use thimble structure or elastic piece structure.
Embodiment 2:
The embodiment of the present invention additionally provides a kind of Modularized unmanned machine using method, and described using method can be with base
The Modularized unmanned machine provided in embodiment 1 realizes, and as shown in Figure 4, described using method includes following
Step:
In step 201, being correlated with currently without man-machine application scenario of intelligent terminal for reception operator input
Information.
Wherein, the relevant information of described application scenario includes: wind speed, cruising time, shooting time, shooting
One or more in environmental form and style of shooting.
In step 202., intelligent terminal calculates the functional module configuration strategy meeting current application occasion.
In step 203, intelligent terminal feeds back one or more optional function module configuration strategy to operation
Personnel, in order to operator select suitably to configure the assembling of the functional module that strategy completes unmanned plane.
Embodiments provide a kind of Modularized unmanned machine using method, and can be defeated according to operator
The relevant information of the unmanned plane application scenario entered, the configuration strategy of systematic function module.Thus be operator
Use its own unmanned plane functional module to provide one and use strategy the most efficiently, further, far
Journey server can also collect the result that the configuration strategy using difference in functionality module of operator is completed,
And browse for operator after being attached to different configuration strategies, thus provide more intuitive for operator
References object.
In conjunction with the embodiment of the present invention, there is a kind of preferably implementation, enter in this preferably implementation
The configuration strategy considering to be obtained by intelligent terminal's analysis of one step, the merit having relative to current operation personnel
Cannot be able to realize for module.In order to solve above-mentioned situation about being likely encountered, grasp in intelligent terminal for reception
Before making the relevant information currently without man-machine application scenario of personnel's input, also include:
The unmanned plane body information of intelligent terminal for reception operator input and one or more merit having been provided with
Energy module information, described one or more functional module information having been provided with is imported data base by intelligent terminal；
Then intelligent terminal feeds back one or more optional function module configuration strategy to operator, specifically also
Including:
Described intelligent terminal proofreads the functional module needed for each energy module configures strategy and described operator join
One or more standby functional module, and in the way of highlighted, present attainable functional module configuration strategy.
Wherein, the described highlighted a kind of display side being specially difference and other the most attainable functional modules configuration strategy
Formula.Including, but not limited to, the brightness of display is higher than the most attainable functional module configuration strategy；With completely
The unmanned plane model approach of normal display present, and for the most attainable functional module configuration strategy, then
The functional module being wherein not equipped with is presented in the way of Lycoperdon polymorphum Vitt and/or low-light level
In conjunction with the embodiment of the present invention, in order to realize described step 202, there is a kind of preferably specific implementation,
As it is shown in figure 5, specifically include:
In step 2021, confirm essential functional module type according to style of shooting.
In step 2022, the cruising time needed for confirmation, and according to optional battery module capacity, and
By unmanned plane body information, the weight of each alternative functional module and/or power, it is calculated to meet and works as
One or more functional modules configuration strategy of front application scenario；Wherein said each alternative function mould
Block belongs to the essential functional module type confirmed.
In conjunction with the embodiment of the present invention, there is a kind of preferably implementation, described intelligent terminal feed back one or
Person's multiple optional function module configuration strategy gives operator, also includes:
In described intelligent terminal's feedback server, storage corresponds to one or more optional function mould
The use case of block configuration strategy is to operator；Wherein, described use case includes being made by designer
And the case uploaded onto the server or the case being made by historical operation personnel and uploading onto the server.
In conjunction with the embodiment of the present invention, there is a kind of preferably implementation, described intelligent terminal feed back one or
Person's multiple optional function module configuration strategy gives operator, also includes:
Corresponding to various configuration strategies, the use parameter that corresponding display draws during calculating；Wherein, institute
State and use parameter to include the cruising time of various configuration strategy, applicable scene information, be used rate, dominance
In one or more.
It is emphasized that the method that the embodiment of the present invention is proposed is applicable not only to user and selects functional module
Configuration strategy completes the assembling of own module unmanned plane, can equally be well applied to user when buying for the first time, root
According to the configuration strategy using Requirement Acquisition cost performance optimum of self, and complete buying.
What deserves to be explained is, the information between module in said apparatus, unit is mutual, in execution process etc.
Holding, owing to the processing method embodiment with the present invention is based on same design, particular content can be found in side of the present invention
Narration in method embodiment, here is omitted.
One of ordinary skill in the art will appreciate that all or part of step in the various methods of embodiment is can
Completing instructing relevant hardware by program, this program can be stored in a computer-readable storage medium
In matter, storage medium may include that read only memory (ROM, Read Only Memory), random access memory
Memorizer (RAM, Random Access Memory), disk or CD etc..
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all at this
Any amendment, equivalent and the improvement etc. made within bright spirit and principle, should be included in the present invention
Protection domain within.
Claims (10)
1. a Modularized unmanned machine, it is characterised in that include unmanned plane body, one or more function
Module is concrete:
Described unmanned plane body includes MCU and wireless signal transceiver module, and gyroscope, display lamp and honeybee
One or more functional unit in ring device；
It is provided with one or more adsorption magnet on described unmanned plane body, is used for and difference in functionality module
Corresponding adsorption magnet adsorb, thus complete the fixing of functional module；Wherein, described Functional Module
Include the auxiliary of the photographic head of plurality of specifications, the screw wing of plurality of specifications, the set of cells of plurality of specifications and plurality of specifications
Help one or more functional modules in module.
Modularized unmanned machine the most according to claim 1, it is characterised in that one or more
Functional module and corresponding attachment structure, specially one on unmanned plane body from top to bottom, from the bottom to top, by
Left-to-right and/or the notch pushed from right to left, its connection interface of functional module specially can embed institute
State notch, and complete the structure fixed based on self adsorption magnet with unmanned plane body.
Modularized unmanned machine the most according to claim 1, it is characterised in that one or more function
Module arranges interface groove in corresponding attachment structure on unmanned plane body, specially unmanned plane body；Described
The interface position of one or more functional module arranges lordosis, and described lordosis is used for inserting described groove；Its
In, on described lordosis and groove, contact position is provided with adsorption magnet.
4. according to the arbitrary described Modularized unmanned machine of claim 1-3, it is characterised in that one or many
Individual functional module and corresponding attachment structure on unmanned plane body, between data-interface use thimble structure
Or elastic piece structure.
5. a Modularized unmanned machine using method, it is characterised in that described using method includes:
The relevant information currently without man-machine application scenario of intelligent terminal for reception operator input；
Intelligent terminal calculates the functional module configuration strategy meeting current application occasion；
Intelligent terminal feeds back one or more optional function module configuration strategy to operator, in order to operation
Personnel selection suitably configures the assembling that strategy completes the functional module of unmanned plane.
Modularized unmanned machine using method the most according to claim 5, it is characterised in that in intelligence eventually
Before end receives the relevant information currently without man-machine application scenario of operator's input, also include:
The unmanned plane body information of intelligent terminal for reception operator input and one or more merit having been provided with
Energy module information, described one or more functional module information having been provided with is imported data base by intelligent terminal；
Then intelligent terminal feeds back one or more optional function module configuration strategy to operator, specifically also
Including:
Described intelligent terminal proofreads the functional module needed for each energy module configures strategy and described operator join
One or more standby functional module, and in the way of highlighted, present attainable functional module configuration strategy.
7. according to the Modularized unmanned machine using method described in claim 5 or 6, it is characterised in that described
The relevant information of application scenario, specifically includes:
One or more in wind speed, cruising time, shooting time, shooting environmental type and style of shooting.
Modularized unmanned machine using method the most according to claim 7, it is characterised in that described intelligence
Terminal calculates the functional module configuration strategy meeting current application occasion, specifically includes:
Essential functional module type is confirmed according to style of shooting；
Cruising time needed for confirmation, and according to optional battery module capacity, and believed by unmanned plane body
Breath, the weight of each alternative functional module and/or power, be calculated and meet the one of current application occasion
Plant or several functions module configuration strategy；Wherein said each alternative functional module belongs to be confirmed
Essential functional module type.
9. according to the Modularized unmanned machine using method described in claim 5 or 6, it is characterised in that described
It is tactful to operator that intelligent terminal feeds back the configuration of one or more optional function module, also includes:
In described intelligent terminal's feedback server, storage corresponds to one or more optional function mould
The use case of block configuration strategy is to operator；Wherein, described use case includes being made by designer
And the case uploaded onto the server or the case being made by historical operation personnel and uploading onto the server.
10. according to the Modularized unmanned machine using method described in claim 5 or 6, it is characterised in that institute
State intelligent terminal feed back one or more optional function module configuration strategy give operator, also include:
Corresponding to various configuration strategies, the use parameter that corresponding display draws during calculating；Wherein, institute
State and use parameter to include the cruising time of various configuration strategy, applicable scene information, be used rate, dominance
In one or more.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610269708.6A CN105947201A (en) | 2016-04-27 | 2016-04-27 | Modularized unmanned aerial vehicle and use method thereof |
| PCT/CN2016/100338 WO2017185629A1 (en) | 2016-04-27 | 2016-09-27 | Modularized unmanned aerial vehicle and use method thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610269708.6A CN105947201A (en) | 2016-04-27 | 2016-04-27 | Modularized unmanned aerial vehicle and use method thereof |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107024224A (en) * | 2017-04-28 | 2017-08-08 | 南京信息工程大学 | The angle measurement unit and measuring method of tiltrotor aircraft |
| WO2017185629A1 (en) * | 2016-04-27 | 2017-11-02 | 乐视控股（北京）有限公司 | Modularized unmanned aerial vehicle and use method thereof |
| WO2019047429A1 (en) * | 2017-09-05 | 2019-03-14 | 北京工业大学 | Multi-rotor unmanned aerial vehicle-based duct propulsion system |
| CN112650263A (en) * | 2020-12-08 | 2021-04-13 | 电子科技大学 | Control method of combined unmanned aerial vehicle |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109782794B (en) * | 2018-12-24 | 2022-10-11 | 丰翼科技(深圳)有限公司 | Independently-arranged pre-flight detection device for unmanned aerial vehicle and unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979107A (en) * | 2014-05-21 | 2014-08-13 | 北京理工大学 | Folding rotor-type unmanned aerial vehicle |
| CN104730589A (en) * | 2015-03-30 | 2015-06-24 | 上海海事大学 | Aeromagnetic measuring data collection system and device |
| CN104773289A (en) * | 2015-04-16 | 2015-07-15 | 四川理工学院 | Internet-of-things-based micro four-rotor aircraft |
| US20150375586A1 (en) * | 2008-06-16 | 2015-12-31 | Aurora Flight Sciences Corporation | Combined submersible vessel and unmanned aerial vehicle |
| CN204998752U (en) * | 2015-01-04 | 2016-01-27 | 北京零零无限科技有限公司 | Folding unmanned aerial vehicle |
| CN205098485U (en) * | 2015-11-06 | 2016-03-23 | 刘东昌 | Collapsible modularization unmanned aerial vehicle protection architecture |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104280575A (en) * | 2013-07-05 | 2015-01-14 | 天津浩洋环宇科技有限公司 | Portable circuit board testing device |
| CN104460474A (en) * | 2014-10-26 | 2015-03-25 | 吉林医药学院 | Universal ground monitoring system for unmanned aerial vehicle |
| WO2016112124A2 (en) * | 2015-01-08 | 2016-07-14 | Vantage Robotics, Llc | Unmanned aerial vehicle with propeller protection and high impact survivability |
| CN204822083U (en) * | 2015-05-27 | 2015-12-02 | 江苏雪龙信息科技有限公司 | For military use alert unmanned aerial vehicle system that uses of multipurpose |
| CN204776026U (en) * | 2015-06-10 | 2015-11-18 | 深圳九星智能航空科技有限公司 | Lid quick assembly disassembly device behind unmanned aerial vehicle |
| CN104950906A (en) * | 2015-06-15 | 2015-09-30 | 中国人民解放军国防科学技术大学 | Unmanned aerial vehicle remote measuring and control system and method based on mobile communication network |
| CN105129093A (en) * | 2015-07-16 | 2015-12-09 | 张萍 | Multi-rotor-wing unmanned plane |
| CN205176518U (en) * | 2015-11-04 | 2016-04-20 | 陕西蔚蓝航天测控技术开发有限公司 | A portable ground control station for unmanned aerial vehicle ground control |
| CN105947201A (en) * | 2016-04-27 | 2016-09-21 | 乐视控股（北京）有限公司 | Modularized unmanned aerial vehicle and use method thereof |
-
2016
- 2016-04-27 CN CN201610269708.6A patent/CN105947201A/en active Pending
- 2016-09-27 WO PCT/CN2016/100338 patent/WO2017185629A1/en active Application Filing
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150375586A1 (en) * | 2008-06-16 | 2015-12-31 | Aurora Flight Sciences Corporation | Combined submersible vessel and unmanned aerial vehicle |
| CN103979107A (en) * | 2014-05-21 | 2014-08-13 | 北京理工大学 | Folding rotor-type unmanned aerial vehicle |
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| CN205098485U (en) * | 2015-11-06 | 2016-03-23 | 刘东昌 | Collapsible modularization unmanned aerial vehicle protection architecture |
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| WO2017185629A1 (en) * | 2016-04-27 | 2017-11-02 | 乐视控股（北京）有限公司 | Modularized unmanned aerial vehicle and use method thereof |
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