CN110406672A - Multi-axis aircraft returns depressed place charging system and method automatically - Google Patents
Multi-axis aircraft returns depressed place charging system and method automatically Download PDFInfo
- Publication number
- CN110406672A CN110406672A CN201910623430.1A CN201910623430A CN110406672A CN 110406672 A CN110406672 A CN 110406672A CN 201910623430 A CN201910623430 A CN 201910623430A CN 110406672 A CN110406672 A CN 110406672A
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- charging
- axis aircraft
- hoistable platform
- proximity
- signal lamp
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/12—Inductive energy transfer
-
- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of Multi-axis aircrafts to return depressed place charging system and method automatically, setting signal lamp on cabinet, and telescoping cover is by the drive control bidirectional-movement that stretches；Hoistable platform is the square of center aperture, is moved up and down by lifting drive control；The lower section of hoistable platform surface and center opening is arranged in vision target；The charging proximity is the equally distributed four poroid mechanisms being arranged in by the center opening of hoistable platform, it is corresponding with the landing rack position of Multi-axis aircraft, charging receiving coil is provided on landing gear, after Multi-axis aircraft drops to hoistable platform, landing gear insertion charging proximity, is charged by charging proximity；Circuit portion controls the flashing of signal lamp, the charging for the proximity that charges, drives output drive signal to flexible driving and lifting.The present invention is dropped on platform by visual identity stopping platform target, realizes automated wireless charging by Wireless charging coil array.
Description
Technical field
The invention belongs to electronic technology field, in particular to a kind of Multi-axis aircraft returns depressed place charging system and method automatically.
Background technique
With the development of science and technology, Multi-axis aircraft, especially quadrotor Multi-axis aircraft technology now increasingly at
It is ripe, it is also more and more stable to the control of Multi-axis aircraft, it is relevant military affairs, the disaster relief, it is civilian on application all grow a lot.
For example, Amazon and suitable rich express company all send the technology of express delivery in research and development Multi-axis aircraft recently.However, the one of this technology
A great bottleneck is that the cruising ability of Multi-axis aircraft is low, and Multi-axis aircraft is substantially powers by battery, can take
Carried charge is limited, it is difficult to work long hours.In addition, needing Multi-axis aircraft fixed in hidden danger peak period or when encountering emergency event
When or continuous work, need someone supervise guarantee its recycle charging during the work time, not only influence working efficiency in this way, and
Charging is also inconvenient when working outside, influences performing effectively for task.
Major part Multi-axis aircraft is mostly to enhance cruising ability, high-frequency disassembly using the method for replacement battery at present
It is easily damaged rack and its electronic component, and replacement battery is larger to the dependence of people, Multi-axis aircraft automatic charging technology
It will be new development trend.By retrieval, relevant technical solution exists in the prior art and discloses, it is a kind of only to charging system
Abstractdesription, there are still more problems in the specific implementation process；Another Multi-axis aircraft charging pile and its charging side
Method, including electric pushrod, protrusion and communication module, are fixed with protrusion on the charging panel of rotor Multi-axis aircraft, four protrusions are
One group, a square is constituted, protrusion is covered with charging panel, constitutes multiple squares；Telescopic electric pushrod is mounted on charging
The sawtooth projection of the surrounding of plate, bumper bracket bottom is embedded in the gap that charging panel convexes to form, and rotor Multi-axis aircraft cannot
It moves horizontally；After rotor Multi-axis aircraft smooth flight drops on charging panel, no gyroplane sends signal to communication module,
It after charging module receives signal, sends and instructs to electric pushrod, electric pushrod stretches out, the buffering of fixed rotor Multi-axis aircraft
Frame bottom.Multi-axis aircraft in this programme is difficult to be accurately positioned in landing, and independence is poor, and charge efficiency is low, needs
It is further improved.
Summary of the invention
In view of this, return depressed place charging system automatically the present invention provides a kind of Multi-axis aircraft, including cabinet, signal lamp,
Telescoping cover, flexible driving, hoistable platform, vision target, charging proximity, lifting driving and circuit portion, wherein
Setting signal lamp on the cabinet, the telescoping cover, flexible driving, hoistable platform, vision target, charging are close
Portion, lifting driving and circuit portion are arranged in cabinet；
The telescoping cover is by the drive control bidirectional-movement that stretches；The hoistable platform is the square of center aperture, by rising
Drive control is dropped to move up and down；The lower section of hoistable platform surface and center opening is arranged in the vision target；The charging
Near-end is the equally distributed four poroid mechanisms being arranged in by the center opening of hoistable platform, the landing gear with Multi-axis aircraft
Position is corresponding, and charging receiving coil is provided on landing gear, after Multi-axis aircraft drops to hoistable platform, landing gear insertion
Charge proximity, is charged by charging proximity；The flashing of circuit portion control signal lamp, the charging for the proximity that charges,
To flexible driving and lifting driving output drive signal.
Preferably, the circuit portion includes wireless charging circuit, governor circuit and telecommunication circuit, wherein
The wireless charging circuit is to charging control section output signal, to charge to Multi-axis aircraft；The master control
Circuit exports control signal to signal lamp, wireless charging circuit and telecommunication circuit；The telecommunication circuit and remote control terminal and more
Axis aircraft is communicated.
Preferably, the charging proximity includes charging transmitting coil and close switch；Close to switch by Multi-axis aircraft
Landing gear triggering, charging transmitting coil charge to the charging receiving coil on the landing gear of Multi-axis aircraft.
It preferably, is rack shape below the telescoping cover.
Preferably, described stretch is driven to gear-like.
Based on above-mentioned purpose, the present invention also provides a kind of Multi-axis aircrafts to return depressed place charging method, including following step automatically
It is rapid:
S10, remote control terminal send control signal, so that Multi-axis aircraft returns depressed place charging system automatically is in shape of awaiting orders
State: signal lamp is opened, telescoping cover is opened, hoistable platform is raised to and flushes with cabinet upper surface；
S20, Multi-axis aircraft start back depressed place task, search for signal lamp in the sky according to GPS position information；
S30, after Multi-axis aircraft finds signal lamp, tracking signal lamp slowly lands；
S40, recognizes the vision target of hoistable platform upper surface, adjusts itself according to the relative position information of vision target
Posture continues to land, and the circuit portion foundation for returning with Multi-axis aircraft depressed place charging system automatically communicates；
S50 recognizes the vision target below the center opening of hoistable platform, according to the relative position of the vision target
Information adjusts itself posture, until landing gear is fallen completely in four poroid mechanisms of charging proximity, triggers close to switch；
S60, circuit portion, which sends to stop to Multi-axis aircraft, completes information, and hoistable platform decline, telescoping cover is closed, signal lamp
It closes, charging proximity starts to charge；
S70, after charging complete, Multi-axis aircraft sends charge completion information to circuit portion, and the proximity that charges stops charging；
S80 then sends a signal to circuit portion if Multi-axis aircraft stop terminates, and telescoping cover is opened, and hoistable platform rises,
Multi-axis aircraft starting is flown away from, and new task is executed.
Compared with prior art, Multi-axis aircraft disclosed by the invention returns depressed place charging system and method automatically, at least has
Below the utility model has the advantages that
(1) hoistable platform provides landing carrier for Multi-axis aircraft, while vision target being arranged on hoistable platform, realizes
It makes a return voyage, position, full automation operation of landing, improving the accuracy and efficiency of positioning landing；
(2) charging proximity is poroid, and poroid inner wall is provided with charging transmitting coil, on the landing gear of Multi-axis aircraft
Charging receiving coil matching, efficiently charged；Poroid bottom is positioned proximate to switch, and starts to charge when sensing landing,
Reduce energy consumption；
(3) when charging after Multi-axis aircraft landing, hoistable platform falls, and telescoping cover is closed, and Multi-axis aircraft is loaded into
In " depressed place ", independence and security performance of the invention have been fully demonstrated；
(4) it is tentatively guided by signal lamp, the vision target on hoistable platform surface determines landing place relatively, in conjunction with lifting
Vision target in Platform center aperture adjusts position, so that landing gear falls completely within charging proximity, landing automates, is accurate
Change.
Detailed description of the invention
In order to keep the purpose of the present invention, technical scheme and beneficial effects clearer, the present invention provides following attached drawing and carries out
Illustrate:
Fig. 1 is the structural perspective that Multi-axis aircraft of the embodiment of the present invention returns depressed place charging system automatically；
Fig. 2 is the structural plan figure that Multi-axis aircraft of the embodiment of the present invention returns depressed place charging system automatically；
Fig. 3 is the top view that Multi-axis aircraft of the embodiment of the present invention returns depressed place charging system automatically；
Fig. 4 is the charging proximity structural schematic diagram that Multi-axis aircraft of the embodiment of the present invention returns depressed place charging system automatically；
Fig. 5 is the step flow chart that Multi-axis aircraft of the embodiment of the present invention returns depressed place charging method automatically.
Specific embodiment
Below in conjunction with attached drawing, a preferred embodiment of the present invention will be described in detail.
System embodiment is referring to Fig. 1-4, including cabinet 1, signal lamp 2, telescoping cover 3, flexible driving 4, hoistable platform 5, view
Feel target 6, charging proximity 7, lifting driving 8 and circuit portion 9, wherein
Setting signal lamp 2 on cabinet 1, telescoping cover 3, flexible driving 4, hoistable platform 5, vision target 6, charging proximity 7,
Lifting driving 8 and circuit portion 9 are arranged in cabinet 1；
Telescoping cover 3 is by flexible 4 control bidirectional-movement of driving；Hoistable platform 5 is the square of center aperture, is driven by lifting
8 controls move up and down；The lower section on hoistable platform 5 surface and center opening is arranged in vision target 6；The proximity 7 that charges is setting
Equally distributed four poroid mechanisms by the center opening of hoistable platform 5, the landing rack position phase with Multi-axis aircraft 10
It is corresponding, charging receiving coil 72 is provided on landing gear, after Multi-axis aircraft 10 drops to hoistable platform 5, landing gear insertion
Charge proximity 7, is charged by charging proximity 7；Circuit portion 9 control signal lamp 2 flashing, charge proximity 7 charging,
To flexible driving 4 and lifting 8 output drive signals of driving.
In specific embodiment, circuit portion 9 includes wireless charging circuit, governor circuit and telecommunication circuit, wherein wireless charging
Circuit is to charging control section output signal, to charge to Multi-axis aircraft 10；Governor circuit is to signal lamp 2, wireless charging
Circuit and telecommunication circuit output control signal；Telecommunication circuit is communicated with remote control terminal and Multi-axis aircraft 10.
Referring to fig. 4, charging proximity 7 includes charging transmitting coil 71 and close switch 73；Flown close to switch 73 by multiaxis
The landing gear of row device 10 triggers, and charging transmitting coil 71 carries out the charging receiving coil 72 on the landing gear of Multi-axis aircraft 10
Charging.
By above-mentioned setting, hoistable platform 5 realizes rise and fall by lifting driving 8；There are three 5 upper surface of hoistable platform dresses
Vision target 6, in equilateral triangle, the intermediate aperture of hoistable platform 5 are also equipped with vision target 6 below hole.The surrounding of aperture is equal
Four poroid mechanisms of cloth, the poroid mechanism are the proximity 7 that charges, and charging transmitting coil 71 are wound on the inner wall in hole, for sending out
Radio energy, the tail portion of 10 landing gear of Multi-axis aircraft is wound with charging receiving coil 72, with the charging transmitting coil on the inner wall in hole
71 intercouple, for receiving electric energy.The bottom in hole is positioned proximate to switch 73, for perceiving 10 cabinet of Multi-axis aircraft, 1 top,
It is the position that Multi-axis aircraft 10 guides this system by transmitting optical signal.Telescoping cover 3 is lower to have rack gear, and driving 4 of stretching is tooth
Colyliform, therefore telescoping cover 3 is moved back and forth by flexible 4 drive rack-and-pinion realization of driving.Circuit portion 9 includes wireless charging circuit, master
Circuit and telecommunication circuit are controlled, governor circuit is used to control signal lamp 2, the switch of wireless charging system and flexible driving 4 and rises
The movement of drop driving 8, telecommunication circuit with remote control terminal and 10 end of Multi-axis aircraft for being communicated.In addition, not having in field
Under conditions of having power supply, also mountable large-sized battery pack is system power supply.
Embodiment of the method is referring to Fig. 5, comprising the following steps:
S10, remote control terminal send control signal, so that Multi-axis aircraft returns depressed place charging system automatically is in shape of awaiting orders
State: signal lamp is opened, telescoping cover is opened, hoistable platform is raised to and flushes with cabinet upper surface；
S20, Multi-axis aircraft start back depressed place task, search for signal lamp in the sky according to GPS position information；
S30, after Multi-axis aircraft finds signal lamp, tracking signal lamp slowly lands；
S40, recognizes the vision target of hoistable platform upper surface, adjusts itself according to the relative position information of vision target
Posture continues to land, and the circuit portion foundation for returning with Multi-axis aircraft depressed place charging system automatically communicates；
S50 recognizes the vision target below the center opening of hoistable platform, according to the relative position of the vision target
Information adjusts itself posture, until landing gear is fallen completely in four poroid mechanisms of charging proximity, triggers close to switch；
S60, circuit portion, which sends to stop to Multi-axis aircraft, completes information, and hoistable platform decline, telescoping cover is closed, signal lamp
It closes, charging proximity starts to charge；
S70, after charging complete, Multi-axis aircraft sends charge completion information to circuit portion, and the proximity that charges stops charging；
S80 then sends a signal to circuit portion if Multi-axis aircraft stop terminates, and telescoping cover is opened, and hoistable platform rises,
Multi-axis aircraft starting is flown away from, and new task is executed.
Embodiment of the method is repeated no more referring to system embodiment.
The above is merely preferred embodiments of the present invention, be not intended to limit the invention, it is all in spirit of the invention and
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within principle.
Claims (6)
1. a kind of Multi-axis aircraft returns depressed place charging system automatically, which is characterized in that including cabinet, signal lamp, telescoping cover, flexible drive
Dynamic, hoistable platform, vision target, charging proximity, lifting driving and circuit portion, wherein
Setting signal lamp on the cabinet, the telescoping cover, hoistable platform, vision target, charging proximity, rise at flexible driving
Drop driving and circuit portion are arranged in cabinet；
The telescoping cover is by the drive control bidirectional-movement that stretches；The hoistable platform is the square of center aperture, is driven by lifting
Dynamic control moves up and down；The lower section of hoistable platform surface and center opening is arranged in the vision target；The charging proximity
Landing rack position for equally distributed four poroid mechanisms by the center opening of hoistable platform are arranged in, with Multi-axis aircraft
It is corresponding, charging receiving coil is provided on landing gear, after Multi-axis aircraft drops to hoistable platform, landing gear insertion charging
Proximity is charged by charging proximity；Flashing, the charging for the proximity that charges, Xiang Shen of the circuit portion control signal lamp
Contracting driving and lifting driving output drive signal.
2. system according to claim 1, which is characterized in that the circuit portion includes wireless charging circuit, governor circuit
And telecommunication circuit, wherein
The wireless charging circuit is to charging control section output signal, to charge to Multi-axis aircraft；The governor circuit
Control signal is exported to signal lamp, wireless charging circuit and telecommunication circuit；The telecommunication circuit and remote control terminal and multiaxis fly
Row device is communicated.
3. system according to claim 1, which is characterized in that the charging proximity includes charging transmitting coil and approaches
Switch；It is triggered close to switch by the landing gear of Multi-axis aircraft, the transmitting coil that charges is to filling on the landing gear of Multi-axis aircraft
Electric receiving coil charges.
4. system according to claim 1, which is characterized in that be rack shape below the telescoping cover.
5. system according to claim 4, which is characterized in that described stretch is driven to gear-like.
6. the Multi-axis aircraft of system described in a kind of one of claim 1-5 returns depressed place charging method automatically, which is characterized in that including
Following steps:
S10, remote control terminal sends control signal, so as to return depressed place charging system automatically standby for Multi-axis aircraft: letter
Signal lamp is opened, telescoping cover is opened, hoistable platform is raised to and flushes with cabinet upper surface；
S20, Multi-axis aircraft start back depressed place task, search for signal lamp in the sky according to GPS position information；
S30, after Multi-axis aircraft finds signal lamp, tracking signal lamp slowly lands；
S40 recognizes the vision target of hoistable platform upper surface, is adjusted according to the relative position information of vision target from figure
State continues to land, and the circuit portion foundation for returning with Multi-axis aircraft depressed place charging system automatically communicates；
S50 recognizes the vision target below the center opening of hoistable platform, according to the relative position information of the vision target
Itself posture is adjusted, until landing gear is fallen completely in four poroid mechanisms of charging proximity, is triggered close to switch；
S60, circuit portion, which sends to stop to Multi-axis aircraft, completes information, and hoistable platform decline, telescoping cover is closed, and signal lamp closes
It closes, charging proximity starts to charge；
S70, after charging complete, Multi-axis aircraft sends charge completion information to circuit portion, and the proximity that charges stops charging；
S80 then sends a signal to circuit portion if Multi-axis aircraft stop terminates, and telescoping cover is opened, and hoistable platform rises, multiaxis
Aircraft starting is flown away from, and new task is executed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910623430.1A CN110406672B (en) | 2019-07-11 | 2019-07-11 | Automatic docking charging system and method for multi-axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910623430.1A CN110406672B (en) | 2019-07-11 | 2019-07-11 | Automatic docking charging system and method for multi-axis aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110406672A true CN110406672A (en) | 2019-11-05 |
| CN110406672B CN110406672B (en) | 2021-05-04 |
Family
ID=68361012
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910623430.1A Active CN110406672B (en) | 2019-07-11 | 2019-07-11 | Automatic docking charging system and method for multi-axis aircraft |
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|---|---|---|---|---|
| CN104816834A (en) * | 2015-05-11 | 2015-08-05 | 江苏数字鹰科技发展有限公司 | Aircraft automatic location charging device and method for landing and location through same |
| CN108137154A (en) * | 2015-10-01 | 2018-06-08 | Lg伊诺特有限公司 | For the wireless charging system and its operating method of unmanned vehicle |
| CN105226836A (en) * | 2015-10-20 | 2016-01-06 | 杨珊珊 | A kind of can the unmanned plane of automatic charging, unmanned plane charging system and charging method |
| US20180237161A1 (en) * | 2017-02-21 | 2018-08-23 | Echostar Technologies L.L.C. | Systems and methods for uav docking and recharging |
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| Publication number | Publication date |
|---|---|
| CN110406672B (en) | 2021-05-04 |
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