CN106532818A - Automatic endurance charging pile for rotor wing unmanned aerial vehicle and automatic endurance method therefor - Google Patents
Automatic endurance charging pile for rotor wing unmanned aerial vehicle and automatic endurance method therefor Download PDFInfo
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- CN106532818A CN106532818A CN201611011593.7A CN201611011593A CN106532818A CN 106532818 A CN106532818 A CN 106532818A CN 201611011593 A CN201611011593 A CN 201611011593A CN 106532818 A CN106532818 A CN 106532818A
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- aerial vehicle
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- rotor wing
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- charging pile
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- 238000000034 method Methods 0.000 title claims abstract description 24
- 230000008569 process Effects 0.000 claims abstract description 10
- 238000012544 monitoring process Methods 0.000 claims description 19
- 230000004044 response Effects 0.000 claims description 17
- 230000005611 electricity Effects 0.000 claims description 10
- 230000007613 environmental effect Effects 0.000 claims description 4
- 239000002245 particle Substances 0.000 claims description 3
- 230000007812 deficiency Effects 0.000 claims description 2
- 230000002035 prolonged effect Effects 0.000 abstract 1
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
Classifications
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- H02J7/0027—
-
- 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
- B64C39/028—Micro-sized aircraft
-
- 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
- B64U50/34—In-flight charging
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
- H02J7/0045—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction concerning the insertion or the connection of the batteries
Abstract
The invention discloses an automatic endurance charging pile for a rotor wing unmanned aerial vehicle and an automatic endurance method therefor. The charging pile comprises a square base, wherein a wireless charging apparatus is arranged in the center of the square base; a two-dimensional code scanning gun and a signal transmitter are arranged on each of four corners separately; triangular cover plates are arranged on the four edges; and a power supply and a controller for controlling the equipment are arranged in the base. According to the automatic endurance method, when the unmanned aerial vehicle detects that the electric quantity is insufficient, a nearest charging pile is searched; the charging pile performs two-dimensional code recognition on the unmanned aerial vehicle, and the cover plates are opened after successful recognition; then the unmanned aerial vehicle lands above the square base, and is charged by the charging pile, and meanwhile, the cover plates are closed to protect the unmanned aerial vehicle; and when the unmanned aerial vehicle is fully charged or when the charging quantity of the unmanned aerial vehicle satisfies the residual flight task requirement, the charging process is stopped, the cover plates are opened, the unmanned aerial vehicle can continuously perform the residual task, and then the cover plates are closed. By adoption of the automatic endurance charging pile and the automatic endurance method, the unmanned aerial vehicle can automatically finds the charging pile to be charged in low electric quantity, so that the endurance of the unmanned aerial vehicle is greatly prolonged.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, in particular to a kind of rotor wing unmanned aerial vehicle independently continue a journey charging pile and
Its method.
Background technology
Rotor wing unmanned aerial vehicle develops extremely rapid in recent years as a kind of new unmanned plane.Hang specific to rotor wing unmanned aerial vehicle
Stop and VTOL ability has in mapping, electric inspection process, environmental monitoring, agricultural insurance, Post disaster relief, the cruise of border high frequency etc.
Prominent technical advantage.But, existing rotor wing unmanned aerial vehicle does not rapidly develop because of reasons such as endurance differences.
Endurance is it is crucial that depending on the capacity of battery.But at present, weight is the lithium battery of 300g in theory
Can only allow the unmanned plane during flying 17 minutes of 500g.And hydrogen fuel cell, solar cell etc. are subject to existing technical merit
With the factor of manufacturing cost, temporarily cannot also popularize.
In order to improve voyage, people constantly propose that various improved rotor wing unmanned aerial vehicle battery and power consumption efficiency are higher
Motor.For example, unmanned plane voyage can be improved using the method for increasing charge capacity, but the shortcoming of this method is to increase charge capacity
While, the load of unmanned plane also substantially increases, and voyage improves unobvious.As can be seen here, how to effectively improve rotor nobody
The course continuation mileage of machine has been those skilled in the art's problem demanding prompt solution.
The content of the invention
The problem not enough in order to make up existing unmanned plane endurance, the present invention is intended to provide a kind of rotor wing unmanned aerial vehicle is autonomous
Continuation of the journey charging pile and its method, realize that unmanned plane autonomous charging station of finding in the case of not enough power supply is charged, make nobody
The cruising time of machine lengthens significantly.
To realize above-mentioned technical purpose, above-mentioned technique effect is reached, the present invention is achieved through the following technical solutions：
A kind of rotor wing unmanned aerial vehicle is independently continued a journey charging pile, including a plinth for rotor wing unmanned aerial vehicle landing, described square
Four sides of base be respectively arranged with one piece can folding angle fillet, one can be formed after four pieces of angle fillets closures
Cover in the pyramid of the rotor wing unmanned aerial vehicle for protecting；It is respectively arranged with one to stretch on four angles of the plinth
Bar, per expansion link described in root on be provided with one for recognizing the two-dimensional code scanning rifle of the rotor wing unmanned aerial vehicle fuselage Quick Response Code
And a signal projector for chargeable signal is fed back to the rotor wing unmanned aerial vehicle；Use is provided with the plinth
In the wireless charging device charged for the rotor wing unmanned aerial vehicle, it is provided with the wireless charging device for monitoring the rotor
The electric quantity monitoring equipment of unmanned plane battery electric quantity；The plinth is internally provided with a controller, the controller point
It is not connected with the wireless charging device, the angle fillet, the two-dimensional code scanning rifle and power supply.
Further, realize connecting by hinge between the angle fillet and the plinth.
Further, the upper surface of the plinth is provided with the projection for avoiding the rotor wing unmanned aerial vehicle from skidding
Grain.
Further, the energy source mode of the power supply be solar charging electrically or grid charging mode.
Further, when the power supply energy source mode be solar charging electrically when, the triangle lid
The outer surface of plate arranges the solar panels that the promising power supply charges.
Further, described grid charging mode includes wireless charging mode or wired charging modes.
Further, the discernible Quick Response Code of the two-dimensional code scanning rifle includes PDF417 codes, QR codes and GM codes.
Further, lightning rod is installed on the charging pile.
A kind of rotor wing unmanned aerial vehicle is independently continued a journey method, comprises the following steps：
Step 1）When rotor wing unmanned aerial vehicle not enough power supply in flight way, rotor wing unmanned aerial vehicle reaches nearest by GPS navigation immediately
Charging pile near, then hover over above charging pile；
Step 2）Controller control expansion link drive two-dimensional code scanning rifle be raised above, two-dimensional code scanning rifle to be sprayed on rotor without
Quick Response Code immediately below man-machine fuselage is caught, and the Quick Response Code after seizure is sent to controller is identified；
Step 3）When controller identifies captured Quick Response Code, and after confirming the identity information of rotor wing unmanned aerial vehicle, controller
Chargeable signal is fed back to rotor wing unmanned aerial vehicle by signal projector；
Step 4）Four pieces of angle fillets of controller control charging pile launch, and rotor wing unmanned aerial vehicle is adjusted by itself flight control system
Flight attitude, on the plinth of charging pile, the wireless charging device on plinth enters safe falling to rotor wing unmanned aerial vehicle
Row charges；
Step 5）While starting to charge up, controller controls four pieces of angle fillet closures, and rotor wing unmanned aerial vehicle is completely encapsulated in
In charging pile, prevent rotor wing unmanned aerial vehicle that such environmental effects or stolen are subject in charging process；
Step 6）In charging process, electric quantity monitoring equipment real-time monitoring charge capacity, and by the electric quantity signal for real-time monitoring
Controller is sent to, controller joint GPS system determines rotor wing unmanned aerial vehicle residue flight path and calculates required for this section of route
Electricity；
Step 7）When controller once to monitor rotor wing unmanned aerial vehicle fully charged or calculate current charged amount and remain remaining enough
During navigational duty, controller launches the charge signal that finish to rotor wing unmanned aerial vehicle by signal projector immediately；
Step 8）After charging is finished, controller controls four pieces of angle fillets immediately to launch again, rotor wing unmanned aerial vehicle automatic
Continue cruise mode, steadily take off from plinth, remaining task is completed by original set airline operation；
Step 9）After rotor wing unmanned aerial vehicle flies away from charging pile, controller controls four pieces of angle fillets and closes again, waits next
Secondary charging tasks.
The invention has the beneficial effects as follows：
The present invention intends building appropriate charging pile on unmanned plane patrol course line（Similar filling station）, unmanned plane can be in electricity
In the case of deficiency, autonomous charging station of finding is charged, and compensate for the not enough problem of current unmanned plane endurance.
2nd, charging pile cover plate of the invention can be closed when charging, and form the cover of a pyramid, can be effective
Charging pile is protected not affected and the antitheft problem of unmanned plane charging process by wind and frost sleet natural environment, human factor.
3rd, before unmanned plane charging, charging pile carries out Quick Response Code identification to unmanned plane using two-dimensional code scanning rifle, not only can
Effectively confirm the identity information of unmanned plane, and effectively prevent the problem that the unmanned chance error of different vendor is rushed.
4th, the raised particle on charging pile base of the invention can prevent unmanned plane from occurring to skid in charging process, protect
The safety of unmanned plane is hindered.
5th, charging pile of the invention accurately can be grasped charge capacity when unmanned plane charges and accurately count with reference to GPS system
The electricity needed for unmanned plane range-to-go is calculated, once finding that charge capacity meets range-to-go demand enough, stops at once filling
Electricity, can so greatly prolong the service life of charging pile, reduce later maintenance cost.
6th, charging pile of the invention is by with reference to GPS system precise positioning so that unmanned plane recharging becomes simply may be used
Lean on, allow unmanned plane operating efficiency to greatly increase, have broad application prospects.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of specification, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after.
The specific embodiment of the present invention is shown in detail in by following examples and its accompanying drawing.
Description of the drawings
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, this
Bright schematic description and description does not constitute inappropriate limitation of the present invention for explaining the present invention.In the accompanying drawings：
Fig. 1 is the three-dimensional structure diagram of charging pile of the present invention；
Fig. 2 is top view when charging pile cover plate of the present invention is opened；
Fig. 3 is the electric diagram of charging pile of the present invention.
Label declaration in figure：1st, plinth；2nd, angle fillet；3rd, expansion link；4th, two-dimensional code scanning rifle；5th, signal is sent out
Emitter；6th, wireless charging device；7th, electric quantity monitoring equipment；8th, controller；9th, power supply；10th, rotor wing unmanned aerial vehicle.
Specific embodiment
Below with reference to the accompanying drawings and in conjunction with the embodiments, describe the present invention in detail.
Referring to shown in Fig. 1-3, a kind of rotor wing unmanned aerial vehicle is independently continued a journey charging pile, including one lands for rotor wing unmanned aerial vehicle 10
Plinth 1, four sides of the plinth 1 be respectively arranged with one piece can folding angle fillet 2, four pieces of triangles
Shape cover plate 2 can be formed after closing and be covered in a pyramid for protecting the rotor wing unmanned aerial vehicle 10；The plinth 1
An expansion link 3 is respectively arranged with four angles, per expansion link described in root 3 on be provided with one for recognize the rotor without
The two-dimensional code scanning rifle 4 of man-machine 10 fuselage Quick Response Code and one are for feeding back chargeable signal to the rotor wing unmanned aerial vehicle 10
Signal projector 5；The wireless charging device 6 for charging for the rotor wing unmanned aerial vehicle 10, institute are provided with the plinth 1
State and be provided with wireless charging device 6 for monitoring the electric quantity monitoring equipment 7 of 10 battery electric quantity of the rotor wing unmanned aerial vehicle；The side
Shape base 1 is internally provided with a controller 8, the controller 8 respectively with the wireless charging device 6, the triangle
Cover plate 2, the two-dimensional code scanning rifle 4 and power supply 9 connect.
Further, realize connecting by hinge between the angle fillet 2 and the plinth 1.
Further, the upper surface of the plinth 1 is provided with convex for avoid the rotor wing unmanned aerial vehicle 10 from skidding
Play particle.
Further, the energy source mode of the power supply 9 be solar charging electrically or grid charging mode.
Further, when the power supply 9 energy source mode be solar charging electrically when, the triangle lid
The outer surface of plate 2 arranges the big-power solar plate that the promising power supply 9 charges, and lower of noon sun can be fast by sunshine
Speed is full of, and solar panels also can expand on demand.
Further, described grid charging mode includes wireless charging mode or wired charging modes, wherein the nothing
The highest charge efficiency of line charging modes can reach more than 80%, and the charging interval can according to actual needs by designing coil size
Change, wired charging modes are may be provided at the urban operating mechanisms such as bus platform, street lamp.
Further, 4 discernible Quick Response Code of the two-dimensional code scanning rifle includes PDF417 codes, QR codes and GM codes.
Further, lightning rod is installed on the charging pile, prevents thunder and lightning from causing to charging pile and rotor wing unmanned aerial vehicle
Infringement.
A kind of rotor wing unmanned aerial vehicle is independently continued a journey method, comprises the following steps：
Step 1）When the not enough power supply in flight way of rotor wing unmanned aerial vehicle 10, rotor wing unmanned aerial vehicle 10 is reached by GPS navigation immediately
Near nearest charging pile, then hover over above charging pile；
Step 2）The control expansion link 3 of controller 8 drives two-dimensional code scanning rifle 4 to be raised above, and 4 pairs, two-dimensional code scanning rifle is sprayed on rotation
Quick Response Code immediately below 10 fuselage of wing unmanned plane is caught, and the Quick Response Code after seizure is sent to controller 8 is identified；
Wherein, using two-dimensional code scanning one can be quick identification rotor wing unmanned aerial vehicle information, two can be prevented from the nothing of other
It is man-machine to carry out rubbing electricity；As the GPS system of rotor wing unmanned aerial vehicle there may be certain error, it is impossible to accurately hover over certain and fix
Two-dimensional code scanning rifle on, therefore charging pile employs four two-dimensional code scanning rifles, increases scanning area, and passes through expansion link
Preferably the Quick Response Code of fuselage can be scanned, greatly increase the success rate of scanning；
Step 3）When controller 8 identifies captured Quick Response Code, and after confirming the identity information of rotor wing unmanned aerial vehicle 10, control
Device 8 feeds back chargeable signal to rotor wing unmanned aerial vehicle 10 by signal projector 5；
Step 4）Four pieces of angle fillets 2 of the control charging pile of controller 8 launch, and rotor wing unmanned aerial vehicle 10 passes through itself flight control system
Adjustment flight attitude, safe falling on the plinth 1 of charging pile, the wireless charging device 6 on plinth 1 to rotor without
Man-machine 10 are charged；
Step 5）While starting to charge up, controller 8 controls four pieces of angle fillets 2 and closes, and rotor wing unmanned aerial vehicle 10 is wrapped completely
It is rolled in charging pile, prevents rotor wing unmanned aerial vehicle 10 that environmental factor is subject in charging process（Heavy rain, severe snow, cold current）Affect or
It is stolen；
Step 6）In charging process, 7 real-time monitoring charge capacity of electric quantity monitoring equipment, and by the electric quantity signal for real-time monitoring
Controller 8 is sent to, the joint GPS system of controller 8 determines 10 remaining flight path of rotor wing unmanned aerial vehicle and calculates this section of route institute
The electricity of needs；
Step 7）When controller 8 once monitoring rotor wing unmanned aerial vehicle 10 is fully charged or calculate current charged amount and maintain enough to remain
During remaining navigational duty, controller 8 launches the charge signal that finish to rotor wing unmanned aerial vehicle 10 by signal projector 5 immediately；
For example, when only need to be charged to remaining required by task electricity and add 20% standby electricity, you can stop charging, can so prolong
The service life of long charging pile, reduces later maintenance cost；
Step 8）After charging is finished, controller 8 controls four pieces of angle fillets 2 immediately to launch again, and rotor wing unmanned aerial vehicle 10 is automatic
Start and continue cruise mode, steadily take off from plinth 1, remaining task is completed by original set airline operation；
Step 9）After rotor wing unmanned aerial vehicle 10 flies away from charging pile, controller 8 controls four pieces of angle fillets 2 and closes again, waits
Charging tasks next time.
The preferred embodiments of the present invention are the foregoing is only, the present invention is not limited to, for those skilled in the art
For member, the present invention can have various modifications and variations.All any modifications within the spirit and principles in the present invention, made,
Equivalent, improvement etc., should be included within the scope of the present invention.
Claims (9)
1. a kind of rotor wing unmanned aerial vehicle is independently continued a journey charging pile, it is characterised in that：Rotor wing unmanned aerial vehicle is supplied including one（10）Landing
Plinth（1）, the plinth（1）Four sides be respectively arranged with one piece can folding angle fillet（2）, described in four pieces
Angle fillet（2）One can be formed after closure for protecting the rotor wing unmanned aerial vehicle（10）Pyramid on cover；The side
Shape base（1）Four angles on be respectively arranged with an expansion link（3）, per expansion link described in root（3）On be provided with a use
In the identification rotor wing unmanned aerial vehicle（10）The two-dimensional code scanning rifle of fuselage Quick Response Code（4）And one for the rotor nobody
Machine（10）Feed back the signal projector of chargeable signal（5）；The plinth（1）On be provided with for for the rotor nobody
Machine（10）The wireless charging device of charging（6）, the wireless charging device（6）On be provided with for monitoring the rotor wing unmanned aerial vehicle
（10）The electric quantity monitoring equipment of battery electric quantity（7）；The plinth（1）Be internally provided with a controller（8）, the control
Device processed（8）Respectively with the wireless charging device（6）, the angle fillet（2）, the two-dimensional code scanning rifle（4）And supply
Power supply（9）Connection.
2. rotor wing unmanned aerial vehicle according to claim 1 is independently continued a journey charging pile, it is characterised in that：The angle fillet
（2）With the plinth（1）Between by hinge realize connect.
3. rotor wing unmanned aerial vehicle according to claim 1 is independently continued a journey charging pile, it is characterised in that：The plinth（1）
Upper surface be provided with for avoiding the rotor wing unmanned aerial vehicle（10）The raised particle of skidding.
4. rotor wing unmanned aerial vehicle according to claim 1 is independently continued a journey charging pile, it is characterised in that：The power supply（9）
Energy source mode be solar charging electrically or grid charging mode.
5. rotor wing unmanned aerial vehicle according to claim 4 is independently continued a journey charging pile, it is characterised in that：When the power supply
（9）Energy source mode be solar charging electrically when, the angle fillet（2）Outer surface the promising power supply is set
Power supply（9）The solar panels of charging.
6. rotor wing unmanned aerial vehicle according to claim 4 is independently continued a journey charging pile, it is characterised in that：Described grid charging side
Formula includes wireless charging mode or wired charging modes.
7. rotor wing unmanned aerial vehicle according to claim 1 is independently continued a journey charging pile, it is characterised in that：The two-dimensional code scanning rifle
（4）Discernible Quick Response Code includes PDF417 codes, QR codes and GM codes.
8. rotor wing unmanned aerial vehicle according to claim 1 is independently continued a journey charging pile, it is characterised in that：Install on the charging pile
There is lightning rod.
9. a kind of rotor wing unmanned aerial vehicle using charging pile as claimed in claim 1 is independently continued a journey method, it is characterised in that include
Following steps：
Step 1）Work as rotor wing unmanned aerial vehicle（10）In flight way during not enough power supply, rotor wing unmanned aerial vehicle（10）Pass through GPS navigation immediately
Reach near nearest charging pile, then hover over above charging pile；After unmanned plane detects self electric quantity deficiency, unlatching is sought
The pattern of charging pile is looked for, the gps coordinate position of the charging pile closest with current location is found in charging pile database
Step 2）Controller（8）Control expansion link（3）Drive two-dimensional code scanning rifle（4）It is raised above, two-dimensional code scanning rifle（4）It is right
It is sprayed on rotor wing unmanned aerial vehicle（10）Quick Response Code immediately below fuselage is caught, and the Quick Response Code after seizure is sent to controller
（8）It is identified；
Step 3）Work as controller（8）Captured Quick Response Code is identified, and confirms rotor wing unmanned aerial vehicle（10）Identity information after,
Controller（8）By signal projector（5）To rotor wing unmanned aerial vehicle（10）Feed back chargeable signal；
Step 4）Controller（8）Four pieces of angle fillets of control charging pile（2）Launch, rotor wing unmanned aerial vehicle（10）Flown by itself
Control system call interception flight attitude, plinth of the safe falling in charging pile（1）On, plinth（1）On wireless charging Denso
Put（6）To rotor wing unmanned aerial vehicle（10）It is charged；
Step 5）While starting to charge up, controller（8）Four pieces of angle fillets of control（2）Closure, by rotor wing unmanned aerial vehicle（10）
It is completely encapsulated in charging pile, prevents rotor wing unmanned aerial vehicle（10）Such environmental effects or stolen are subject in charging process；
Step 6）In charging process, electric quantity monitoring equipment（7）Real-time monitoring charge capacity, and the electricity for real-time monitoring is believed
Number it is sent to controller（8）, controller（8）Joint GPS system determines rotor wing unmanned aerial vehicle（10）Remaining flight path simultaneously calculates this
Electricity required for section route；
Step 7）Work as controller（8）Once monitoring rotor wing unmanned aerial vehicle（10）It is fully charged or calculate current charged amount and tie up enough
When holding remaining navigational duty, controller（8）Pass through signal projector immediately（5）To rotor wing unmanned aerial vehicle（10）Transmitting charges what is finished
Signal；
Step 8）After charging is finished, controller（8）Four pieces of angle fillets are controlled immediately（2）Launch again, rotor wing unmanned aerial vehicle
（10）Automatic continues cruise mode, from plinth（1）On steadily take off, complete residue by original set airline operation
Task；
Step 9）Treat rotor wing unmanned aerial vehicle（10）After flying away from charging pile, controller（8）Four pieces of angle fillets of control（2）Close again
Close, wait charging tasks next time.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611011593.7A CN106532818A (en) | 2016-11-17 | 2016-11-17 | Automatic endurance charging pile for rotor wing unmanned aerial vehicle and automatic endurance method therefor |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611011593.7A CN106532818A (en) | 2016-11-17 | 2016-11-17 | Automatic endurance charging pile for rotor wing unmanned aerial vehicle and automatic endurance method therefor |
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| CN107117056A (en) * | 2017-05-20 | 2017-09-01 | 朱幕松 | New electronic four rotor wing unmanned aerial vehicle of new energy |
| CN107140194A (en) * | 2017-05-16 | 2017-09-08 | 华东交通大学 | A kind of many rotor railway automatic tour inspection systems of tracking for supporting automatic charging |
| CN107146966A (en) * | 2017-04-11 | 2017-09-08 | 歌尔科技有限公司 | Unmanned plane charging assembly, unmanned plane and unmanned plane automatic recharging method |
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| CN113147436A (en) * | 2021-03-04 | 2021-07-23 | 广西电网有限责任公司电力科学研究院 | Multi-unmanned aerial vehicle wireless charging system and charging control method thereof |
| CN113277080A (en) * | 2021-06-20 | 2021-08-20 | 上海倬彼云汉航空科技有限公司 | Flapping wing platform for charging unmanned aerial vehicle and charging method thereof |
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| CN109649193A (en) * | 2018-12-17 | 2019-04-19 | 华人运通控股有限公司 | Charging system and charging method |
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| CN110116818A (en) * | 2019-05-24 | 2019-08-13 | 中国科学院地理科学与资源研究所 | A kind of automatic charging unmanned plane hangar |
| CN110310520A (en) * | 2019-06-14 | 2019-10-08 | 西安理工大学 | The aerial virtual fence method of the wireless ultraviolet light on unmanned plane recharging level ground |
| CN110816857A (en) * | 2019-10-30 | 2020-02-21 | 金陵科技学院 | Unmanned aerial vehicle city raise dust monitoring facilities's battery compartment based on big dipper satellite |
| CN110816857B (en) * | 2019-10-30 | 2023-09-12 | 金陵科技学院 | Unmanned aerial vehicle city raise dust monitoring facilities's battery compartment based on big dipper satellite |
| CN112477637A (en) * | 2020-12-06 | 2021-03-12 | 湖北鹏程新锐科技发展有限公司 | Be used for unmanned aerial vehicle direct connection charging device |
| CN113147436A (en) * | 2021-03-04 | 2021-07-23 | 广西电网有限责任公司电力科学研究院 | Multi-unmanned aerial vehicle wireless charging system and charging control method thereof |
| CN113147436B (en) * | 2021-03-04 | 2023-03-14 | 广西电网有限责任公司电力科学研究院 | Multi-unmanned aerial vehicle wireless charging system and charging control method thereof |
| CN113277080A (en) * | 2021-06-20 | 2021-08-20 | 上海倬彼云汉航空科技有限公司 | Flapping wing platform for charging unmanned aerial vehicle and charging method thereof |
| CN113277080B (en) * | 2021-06-20 | 2023-07-14 | 上海倬彼云汉航空科技有限公司 | Flapping wing platform for unmanned aerial vehicle charging and charging method thereof |
| CN114290977A (en) * | 2022-01-27 | 2022-04-08 | 南京市急救中心 | Emergency command vehicle based on voice and video fusion communication system and construction method |
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