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CN109774521A - UAV docking system - Google Patents

UAV docking system
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Publication number
CN109774521A
CN109774521ACN201910048432.2ACN201910048432ACN109774521ACN 109774521 ACN109774521 ACN 109774521ACN 201910048432 ACN201910048432 ACN 201910048432ACN 109774521 ACN109774521 ACN 109774521A
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unit
capture
drone
charging interface
unmanned plane
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CN109774521B (en
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张岩
秦帆
刘立志
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Hebei University of Science and Technology
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Hebei University of Science and Technology
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Abstract

Translated fromChinese

本发明适用于无人飞行器技术领域,提供一种无人机对接系统,包括捕获单元、无人机单元以及控制单元,捕获单元和无人机单元分别能够与控制单元通信;捕获单元包括基座、设置于基座上的捕获模块以及用于与无人机单元对接的第一充电接口,第一充电接口设置在捕获模块上;无人机单元包括无人机、设置在无人机顶部的被捕获模块以及用于与捕获单元对接的第二充电接口,第二充电接口设置在被捕获模块上;捕获单元通过捕获模块和被捕获模块对无人机单元进行捕获定位,捕获单元和无人机单元通过第一充电接口和第二充电接口进行对接。本发明提供的无人机对接系统,实现无人机在空中对接充电,避免了降落充电的繁琐步骤,大大提高无人机的使用效率。

The invention is applicable to the technical field of unmanned aerial vehicles, and provides an unmanned aerial vehicle docking system, comprising a capture unit, an unmanned aerial vehicle unit and a control unit, the capture unit and the unmanned aerial vehicle unit can respectively communicate with the control unit; the capture unit includes a base , a capture module arranged on the base, and a first charging interface for docking with the drone unit, the first charging interface is set on the capture module; the drone unit includes a drone, and the drone unit is arranged on the top of the drone The captured module and the second charging interface for docking with the captured unit, the second charging interface is set on the captured module; the capture unit captures and locates the drone unit through the capture module and the captured module, and the capture unit and the unmanned aerial vehicle The machine unit is connected through the first charging interface and the second charging interface. The UAV docking system provided by the invention realizes docking and charging of the UAV in the air, avoids the tedious steps of landing charging, and greatly improves the use efficiency of the UAV.

Description

Unmanned plane docking system
Technical field
The invention belongs to unmanned vehicle technical fields, are to be related to a kind of unmanned plane docking system more specifically.
Background technique
With the development automatically controlled with the technologies such as micro electronmechanical, unmanned plane (especially multi-rotor aerocraft) is with the letter of its structureThe features such as single, easy to use, VTOL and be used widely, be widely used in electric inspection process, express delivery delivery, ecology prisonThe fields such as survey, aerial mapping, emergency mitigation, fire-fighting investigation, consumer entertainment.But unmanned plane (especially multi-rotor aerocraft) existsCruising ability is weak, the big disadvantage of power consumption, therefore unmanned plane can only generally run to be forced within 1-2 hours land and charge, sternlyGhost image rings the lasting use of unmanned plane, limits it in the further development of industrial circle, if it is possible to provide one kind in the skyTo the aerial docking charging unit that unmanned plane charges, the service efficiency of unmanned plane will be greatly improved.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned plane docking systems, it is intended to solve because existing unmanned plane during flying device mustMust land the technical problem for charging and causing unmanned plane during flying device service efficiency low.
To achieve the above object, the technical solution adopted by the present invention is that: a kind of unmanned plane docking system, including capture are singleMember can be docked and isolated unmanned plane unit and matched control unit with the capturing unit, and the capture is singlyThe first and described unmanned plane unit is able to communicate with described control unit;The capturing unit include pedestal, be set to it is describedTrapping module on pedestal and the first charging interface for docking with the unmanned plane unit, first charging interface are setIt sets on the trapping module;The captured module that the unmanned plane unit includes unmanned plane, is arranged at the top of the unmanned planeAnd the second charging interface for docking with the capturing unit, second charging interface are arranged in the captured moduleOn;The capturing unit carries out capture positioning to the unmanned plane unit by the trapping module and the captured module,The capturing unit and the unmanned plane unit are docked by first charging interface and second charging interface.
Further, the captured module includes the capture bar being arranged at the top of the unmanned plane, the trapping moduleFirst pivoted arm and described the are respectively driven including the first pivoted arm hinged with the pedestal respectively, the second pivoted arm and twoThe steering engine that two pivoted arms rotate respectively;The first holding section, the free end of second pivoted arm is arranged in the free end of first pivoted armSecond holding section is set, and first holding section and second holding section are oppositely arranged;The steering engine respectively drives the first cardConjunction portion and second holding section, which abut, clamps the capture bar.
Further, the free end of first pivoted arm is additionally provided with for inducing the capture bar to engage with described firstFirst guide part of portion's engaging, first guide part are located at the lower part of first holding section;The freedom of second pivoted armEnd is additionally provided with the second guide part for inducing the capture bar to engage with second holding section, second guiding positionIn the lower part of second holding section;First guide part is identical with second pilot construction.
Further, first guide part include two in angle setting guide rods, two guide rods respectively withFirst pivoted arm is connected.
Further, the setting height of first guide part is greater than the setting height of second guide part.
Further, first pivoted arm and second pivoted arm are rectangular parallelepiped structure, and the captured module is also wrappedIt includes and is arranged at the top of the capture bar and for abutting the capture cuboid clamped with first pivoted arm and second pivoted arm.
Further, first charging interface is separately positioned on first pivoted arm and second pivoted arm including twoRelative inner power contacting plate, second charging interface include be separately positioned on it is described capture cuboid two sides chargingContact chip.
Further, the trapping module further includes the video camera that the base bottom is arranged in, the captured moduleIt further include two fixation and recognition lamps being arranged at the top of the capture cuboid.
Further, the captured module further includes the laser ranging sensing being arranged at the top of the capture cuboidDevice.
Unmanned plane docking system provided by the invention can position, capture the capturing unit of unmanned plane by being arranged, andCaptured module accordingly is set on unmanned plane, realizes capturing unit to unmanned plane list by trapping module and captured moduleMember carries out capture positioning, while docks the first charging interface and the second charging interface, realizes that unmanned plane docks in the skyCharging avoids the tedious steps of landing charging, greatly improves the service efficiency of unmanned plane.
Detailed description of the invention
Fig. 1 is one of the schematic diagram in docking of unmanned plane docking system provided in an embodiment of the present invention;
Fig. 2 is the two of the schematic diagram in docking of unmanned plane docking system provided in an embodiment of the present invention;
Fig. 3 is the left view of Fig. 2;
Fig. 4 is the schematic diagram after the completion of the docking of unmanned plane docking system provided in an embodiment of the present invention;
Fig. 5 is the left view of Fig. 4.
In figure: 1- capturing unit;11- pedestal;The first pivoted arm of 12-;The first holding section 121-;122- guide rod;13- secondPivoted arm;14- steering engine;The first charging interface of 15-;16- video camera;2- unmanned plane unit;21- unmanned plane;22- captures bar;23- is caughtCatch cuboid;24- fixation and recognition lamp;The second charging interface of 25-;26- laser range sensor.
Specific embodiment
In order to which technical problems, technical solutions and advantages to be solved are more clearly understood, tie belowAccompanying drawings and embodiments are closed, the present invention will be described in further detail.It should be appreciated that specific embodiment described herein is onlyTo explain the present invention, it is not intended to limit the present invention.
It should be noted that unless otherwise clearly defined and limited, " installation ", " connected ", " fixation ", " are set " connection "Set " etc. terms shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integral;It can beMechanical connection, is also possible to be electrically connected;It can be directly connected, two can also be can be indirectly connected through an intermediaryThe interaction relationship of connection or two elements inside element.It for the ordinary skill in the art, can basisConcrete condition understands the concrete meaning of above-mentioned term in the present invention.
In addition, " multiple ", " several " are meant that two or more, unless otherwise specifically defined.
Referring to Figure 1 to Fig. 5, now the embodiment of unmanned plane docking system provided by the invention is illustrated.Unmanned planeDocking system including capturing unit 1, can be docked and isolated unmanned plane unit 2 and matched control with capturing unit 1Unit processed.Control unit is the control axis of whole system, can be the controllers such as computer, PLC, single-chip microcontroller or controllerDocking and the separating action of capturing unit 1 and unmanned plane unit 2 are coordinated in combination.Capturing unit 1 and unmanned plane unit 2 distinguish energyIt is enough to be communicated with control unit, to realize that control unit controls and monitors capturing unit 1 and unmanned plane unit 2.Optionally, control unit can be independently arranged or be arranged in capturing unit 1, control unit, capturing unit 1 and unmanned plane listMember 2 is respectively provided with wireless communication module, in order to which control unit, capturing unit 1 and unmanned plane unit 2 are communicated.
Unmanned plane unit 2 is main unmanned plane during flying device, carries out capture crawl with capturing unit 1 and docks, thusIt completes to be operated from capturing unit 1 to the charging of unmanned plane unit 2, stop or data exchange etc., capturing unit 1 is generally located onIt on building or hovers in the sky, in order to make unmanned plane unit 2 dock charging with the completion of capturing unit 1 in the sky.
Capturing unit 1 includes pedestal 11, the trapping module being set on pedestal 11 and is used to dock with unmanned plane unit 2The first charging interface 15, the first charging interface 15 be arranged on trapping module.Unmanned plane unit 2 includes unmanned plane 21, settingCaptured module at the top of unmanned plane 21 and the second charging interface for being docked with capturing unit, the second charging interface 25Setting is in captured module, and the second charging interface 25 with the rechargeable battery of unmanned plane 21 for being electrically connected, the first chargingMouth 15 is connect with the high capacity cell (or alternating current) for being set in pedestal 11 or being arranged in outside, passes through the first charging interface 15Docking for unmanned plane unit 2 and capturing unit 1 is realized with the docking (electrical connection) of the second charging interface 25, realization unmanned plane 21Charging operations.
In docking operation, unmanned plane unit 2 first flies to the attached of capturing unit 1 by manual control or by control unit controlClose predeterminated position, capturing unit 1 again precisely catch unmanned plane unit 2 by the movement of trapping module and captured moduleAfter obtaining positioning, the first charging interface 15 and the second charging interface 25 also just complete docking electrical connection, capturing unit 1 and unmanned planeUnit 2 carries out docking electrical connection by the first charging interface 15 and the second charging interface 25, to realize filling to unmanned plane 21Electricity.
Unmanned plane docking system provided in an embodiment of the present invention can position, capture the capture list of unmanned plane by being arrangedMember, and captured module accordingly is set on unmanned plane, so that capturing unit is passed through trapping module and the realization pair of captured moduleUnmanned plane unit carries out capture positioning, while docks the first charging interface and the second charging interface, realizes that unmanned plane existsAerial docking charging, avoids the tedious steps of landing charging, greatly improves the service efficiency of unmanned plane.
It is caught referring to Figure 1 to Fig. 5 as a kind of specific embodiment of unmanned plane docking system provided by the inventionObtaining module includes the capture bar 22 that 21 top of unmanned plane is arranged in, and trapping module includes the first pivoted arm hinged with pedestal 11 respectively12, the second pivoted arm 13 and two respectively drive the steering engine 14 that the first pivoted arm 12 and the second pivoted arm 13 rotate respectively.
The first holding section 121 is arranged in the free end of first pivoted arm 12, and the second holding section is arranged in the free end of the second pivoted arm 13,First holding section 121 and the second holding section are oppositely arranged.In docking operation, steering engine 14 respectively drives the first pivoted arm 12 and second turnArm 13 rotates, and abuts the first holding section 121 being oppositely arranged and the second holding section from two sides with capture bar 22 respectively, thisSample has just clamped capture bar 22 using the first holding section 121 and the second holding section, keeps capturing unit 1 and unmanned plane unit 2 completeAt capture and docking.At the end of docking, steering engine 14 respectively drives the first pivoted arm 12 and the second pivoted arm 13 rotates backward, and makes unmanned plane2 free flight of unit.
Referring to Figure 1, a kind of specific embodiment as unmanned plane docking system provided by the invention, the first holding section121 be notch compatible with capture 22 shape of bar.
Referring to Figure 1 to Fig. 5, as a kind of specific embodiment of unmanned plane docking system provided by the invention, firstThe free end of pivoted arm 12 is additionally provided with the first guide part for inducing capture bar 22 to engage with the first holding section 121, and first leadsIt is located at the lower part of the first holding section 121 to portion;The free end of second pivoted arm 13 is additionally provided with for inducing capture bar 22 and secondSecond guide part of holding section engaging, the second guide part are located at the lower part of the second holding section.First guide part and the second guide partStructure is identical.By the first guide part of setting and the second pilot construction, capture bar 22 can be quickly directed to firstAt holding section 121 and the second holding section, is conducive to capture the unit that is captured of bar 22 and quickly positions capture.
Referring to Figure 1 to Fig. 5, as a kind of specific embodiment of unmanned plane docking system provided by the invention, firstGuide part includes two guide rods 122 in angle setting, and two guide rods 122 are connected with the first pivoted arm 12 respectively, in this way, two leadTo the distance between bar 122 minimum with the first pivoted arm 12 connecting place, maximum far from 12 connecting place of the first pivoted arm, to make two122 pairs of capture bars 22 of guide rod have guiding role.When docking, capture bar 22 hovering to predetermined position is simultaneously located at two guide rodsBetween 122, when steering engine 14 drives the rotation of the first pivoted arm 12, remain that capture bar 22 between two guide rods 122, finally drivesDynamic first pivoted arm 12, which turns to, makes to capture the position that bar 22 engages with the first holding section 121.Second guide part and the first guide partStructure is identical with application method, and two guide rods 122 of the second guide part are connected with the second pivoted arm 13 respectively, and first turnThe rotation of arm 12 is synchronous carry out with the rotation of the second pivoted arm 13.
As a kind of specific embodiment of unmanned plane docking system provided by the invention, two guide rods of the first guide part122 in 90 degree of angle settings, and two guide rods 122 of the second guide part are in 90 degree of angle settings, in this way before docking, the first guidingJust it is enclosed the region of a probably similar square between portion and the second guide part, in docking operation, capture bar 22 entersTo the region of similar square, in this way, unmanned plane 21 (capture bar 22) do not need early period it is too smart in the region of similar squareClose positioning, it will be able to the guidance of bar 22 will be captured to the first holding section using the guiding role of the first guide part and the second guide part121 and second carry out capture positioning in holding section.
Referring to Figure 1 to Fig. 5, as a kind of specific embodiment of unmanned plane docking system provided by the invention, in order toTwo guide rods 122 of two guide rods 122 and the second guide part that prevent the first guide part are interfered, the setting of the first guide partHeight is greater than the setting height of the second guide part.
Referring to Figure 1, Fig. 4 and Fig. 5, as a kind of specific embodiment of unmanned plane docking system provided by the invention,First pivoted arm 12 and the second pivoted arm 13 are rectangular parallelepiped structure, and captured module further includes setting at 22 top of capture bar and is used forWith the capture cuboid 23 of 13 collective effect of the first pivoted arm 12 and the second pivoted arm (abutting clamping).In docking operation and dockCheng Shi, capture bar 22 is with the first holding section 121 and the second holding section while engage respectively, capture cuboid 23 also with first turnArm 12 and the second pivoted arm 13, which abut, to be clamped, and the shaking of unmanned plane 21 is prevented, and thus being avoided that influences because unmanned plane 21 shakes bringThe problem of charging effect.
Referring to Figure 1, a kind of specific embodiment as unmanned plane docking system provided by the invention, the first chargingMouth 15 includes two power contacting plates for being separately positioned on the relative inner of the first pivoted arm 12 and the second pivoted arm 13, the second chargingMouth 25 includes the charging contacts for being separately positioned on capture 23 two sides of cuboid.After the completion of docking, capture bar 22 is respectively with theOne holding section 121 and the engaging of the second holding section, capture cuboid 23 also abut clamping with the first pivoted arm 12 and the second pivoted arm 13, togetherWhen each power contacting plate be also electrically connected respectively with corresponding charging contact pad, be set to pedestal 11 to easily realize very muchHigh capacity cell (or alternating current) interior or that outside is arranged in is electrically connected with the rechargeable battery of unmanned plane 21.
It is captured referring to Figure 1 with Fig. 2 as a kind of specific embodiment of unmanned plane docking system provided by the inventionModule further includes the video camera 16 that 11 bottom of pedestal is arranged in, and captured module further includes that two settings are pushed up in capture cuboid 23The fixation and recognition lamp 24 in portion.The setting of video camera 16 and fixation and recognition lamp 24 can make unmanned plane 21 in butt junction location in justTrue direction, in order to the electrical connection of the first charging interface 15 and the second charging interface 25.
When unmanned plane unit 2 needs capturing unit 1 to charge or stop, the flight of unmanned plane unit 2 to 1 lower section of capturing unit,Unmanned plane unit 2 and capturing unit 1 establish wireless communication connection at this time, and capturing unit 1 identifies fixation and recognition by video camera 16The position of lamp 24, and location information is sent to unmanned plane unit 2 in real time, unmanned plane unit 2 is by the Information revision oneselfPosition is accurately positioned with realizing, can also identify the location information of fixation and recognition lamp 24 according to video camera 16 by operator, manuallyControl is by 2 precise positioning of unmanned plane unit to preset direction, to guarantee that capture bar 22 blocks with the first holding section 121 and second respectivelyAfter the engaging of conjunction portion, each power contacting plate is also electrically connected with corresponding charging contact pad respectively.
As a kind of specific embodiment of unmanned plane docking system provided by the invention, video camera 16 is ccd video camera.
It is caught referring to Figure 1 with Fig. 2 as a kind of specific embodiment of unmanned plane docking system provided by the inventionObtaining module further includes the laser range sensor 26 that 23 top of capture cuboid is arranged in.When unmanned plane unit 2 and capturing unit 1It completes tentatively to after just, into docking trapped state.Unmanned plane unit 2 flies upwards, and real by laser range sensor 26When measurement at a distance from capturing unit 1.Unmanned plane unit 2 passes through laser range sensor 26 and identifies at a distance from capturing unit 1,Unmanned plane unit 2 relies on the position of the Information revision oneself to realize accurate positioning in the vertical direction, can also be by operatingPerson identifies the range information of laser range sensor 26 according to video camera 16, manually controls and arrives 2 precise positioning of unmanned plane unitPredeterminated position on vertical direction.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the inventionMade any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.

Claims (9)

Translated fromChinese
1.无人机对接系统,其特征在于,包括捕获单元、能够与所述捕获单元进行对接和分离的无人机单元以及配套的控制单元,所述捕获单元和所述无人机单元分别能够与所述控制单元通信;所述捕获单元包括基座、设置于所述基座上的捕获模块以及用于与所述无人机单元对接的第一充电接口,所述第一充电接口设置在所述捕获模块上;所述无人机单元包括无人机、设置在所述无人机顶部的被捕获模块以及用于与所述捕获单元对接的第二充电接口,所述第二充电接口设置在所述被捕获模块上;所述捕获单元通过所述捕获模块和所述被捕获模块对所述无人机单元进行捕获定位,所述捕获单元和所述无人机单元通过所述第一充电接口和所述第二充电接口进行对接。1. UAV docking system, is characterized in that, comprises capture unit, the UAV unit that can carry out docking and separation with described capture unit and supporting control unit, described capture unit and described UAV unit can respectively communicate with the control unit; the capture unit includes a base, a capture module disposed on the base, and a first charging interface for docking with the drone unit, the first charging interface is provided at on the capture module; the drone unit includes a drone, a captured module disposed on the top of the drone, and a second charging interface for docking with the capture unit, the second charging interface set on the captured module; the capture unit captures and locates the UAV unit through the capture module and the captured module, and the capture unit and the UAV unit pass the A charging interface is docked with the second charging interface.2.如权利要求1所述的无人机对接系统,其特征在于,所述被捕获模块包括设置在所述无人机顶部的捕获杆,所述捕获模块包括分别与所述基座铰接的第一转臂、第二转臂以及两个分别驱动所述第一转臂和所述第二转臂分别转动的舵机;所述第一转臂的自由端设置第一卡合部,所述第二转臂的自由端设置第二卡合部,所述第一卡合部和所述第二卡合部相对设置;所述舵机分别驱动第一卡合部和所述第二卡合部抵接夹持所述捕获杆。2. The drone docking system according to claim 1, wherein the captured module comprises a capture rod disposed on the top of the drone, and the capture module comprises hinged joints with the base respectively. A first turning arm, a second turning arm and two steering gears that drive the first turning arm and the second turning arm to rotate respectively; the free end of the first turning arm is provided with a first engaging part, so The free end of the second rotating arm is provided with a second engaging portion, and the first engaging portion and the second engaging portion are arranged oppositely; the steering gear drives the first engaging portion and the second engaging portion respectively. The joint portion abuts and clamps the capture lever.3.如权利要求2所述的无人机对接系统,其特征在于,所述第一转臂的自由端还设置有用于诱导所述捕获杆与所述第一卡合部卡合的第一导向部,所述第一导向部位于所述第一卡合部的下部;所述第二转臂的自由端还设置有用于诱导所述捕获杆与所述第二卡合部卡合的第二导向部,所述第二导向部位于所述第二卡合部的下部;所述第一导向部和所述第二导向部结构相同。3. The unmanned aerial vehicle docking system according to claim 2, wherein the free end of the first rotating arm is further provided with a first hook for inducing the capture rod to engage with the first engaging portion a guide part, the first guide part is located at the lower part of the first engaging part; the free end of the second rotating arm is also provided with a first guide for inducing the capturing rod to engage with the second engaging part Two guide parts, the second guide part is located at the lower part of the second engaging part; the first guide part and the second guide part have the same structure.4.如权利要求3所述的无人机对接系统,其特征在于,所述第一导向部包括两个呈夹角设置的导向杆,两所述导向杆分别与所述第一转臂相连。4 . The docking system for drones according to claim 3 , wherein the first guide portion comprises two guide rods arranged at an included angle, and the two guide rods are respectively connected with the first rotating arm. 5 . .5.如权利要求4所述的无人机对接系统,其特征在于,所述第一导向部的设置高度大于所述第二导向部的设置高度。5 . The drone docking system according to claim 4 , wherein the setting height of the first guide portion is greater than the setting height of the second guide portion. 6 .6.如权利要求2所述的无人机对接系统,其特征在于,所述第一转臂和所述第二转臂均为长方体结构,所述被捕获模块还包括设置在所述捕获杆顶部并用于与所述第一转臂和所述第二转臂抵接夹紧的捕获长方体。6. The drone docking system according to claim 2, wherein the first rotating arm and the second rotating arm are both rectangular parallelepiped structures, and the captured module further comprises a set on the capture rod. The top is a capturing cuboid for abutting and clamping with the first rotating arm and the second rotating arm.7.如权利要求6所述的无人机对接系统,其特征在于,所述第一充电接口包括两个分别设置在所述第一转臂和所述第二转臂的相对内侧的电源接触片,所述第二充电接口包括分别设置在所述捕获长方体两侧的充电接触片。7. The drone docking system according to claim 6, wherein the first charging interface comprises two power contacts respectively disposed on the opposite inner sides of the first rotating arm and the second rotating arm The second charging interface includes charging contact sheets respectively arranged on both sides of the capturing cuboid.8.如权利要求7所述的无人机对接系统,其特征在于,所述捕获模块还包括设置在所述基座底部的摄像机,所述被捕获模块还包括两个设置在所述捕获长方体顶部的定位识别灯。8. The drone docking system according to claim 7, wherein the capturing module further comprises a camera arranged at the bottom of the base, and the captured module further comprises two cameras arranged at the capturing cuboid Location identification light on top.9.如权利要求8所述的无人机对接系统,其特征在于,所述被捕获模块还包括设置在所述捕获长方体顶部的激光测距传感器。9 . The drone docking system according to claim 8 , wherein the captured module further comprises a laser ranging sensor arranged on the top of the capturing cuboid. 10 .
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Cited By (4)

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CN110661310A (en)*2019-08-302020-01-07深圳供电局有限公司 Charging device and drone combination
CN111463860A (en)*2020-04-102020-07-28北京京东乾石科技有限公司Cooperative charging method and device and logistics equipment
CN112278307A (en)*2019-07-222021-01-29上海复亚智能科技有限公司Unmanned aerial vehicle positioning, clamping and charging mechanism, control method and hangar
CN115556930A (en)*2022-09-222023-01-03南京航空航天大学Self-adaptation docking mechanism suitable for visual identification unmanned aerial vehicle

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