CN114408205A - An unmanned aerial vehicle hangar and its control method - Google Patents
An unmanned aerial vehicle hangar and its control method Download PDFInfo
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- 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
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
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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
- B60L53/30—Constructional details of charging stations
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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
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
- B60L53/38—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles specially adapted for charging by inductive energy transfer
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- 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
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- 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
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- 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
- Y02T90/12—Electric charging stations
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Abstract
Description
技术领域technical field
本发明属于无人机机库技术领域,具体涉及一种无人机机库及其控制方法。The invention belongs to the technical field of unmanned aerial vehicle hangars, and particularly relates to an unmanned aerial vehicle hangar and a control method thereof.
背景技术Background technique
随着对无人机应用价值认知的加深,无人机在消费级、工业级和军用级市场均呈现出迅猛的发展之势。无人机被越来越多运用在航拍、农林植保、安防、测绘、物流、巡检等领域。With the deepening of the understanding of the application value of UAVs, UAVs have shown a rapid development trend in the consumer, industrial and military markets. Drones are increasingly used in aerial photography, agriculture, forestry and plant protection, security, surveying and mapping, logistics, inspection and other fields.
无人机机库一般用于停靠无人机并对无人机进行充电,无人机在降落到无人机机库的停机坪上后,由于无人机的降落点不一定是在停机坪的充电位,对于无人机需要停靠到停机坪的充电位的情况,可以在停机坪上设置位置移动机构将无人机移动到充电位。目前,无人机充完电之后,起飞也是在充电位位置处就地起飞,为了保证无人机起飞时无人机机翼不会碰撞到无人机机库,无人机机库的停机坪的长度设置得比较长,造成无人机机库整体体积较大,增加了无人机机库的重量。The drone hangar is generally used to dock and charge the drone. After the drone landed on the apron of the drone hangar, the landing point of the drone is not necessarily on the apron. If the drone needs to be parked at the charging position of the apron, a position moving mechanism can be set on the apron to move the drone to the charging position. At present, after the drone is fully charged, the take-off is also taken off at the charging position. In order to ensure that the drone's wings will not collide with the drone's hangar when the drone takes off, the drone's hangar will be shut down. The length of the ping is set relatively long, which causes the overall volume of the UAV hangar to be larger and increases the weight of the UAV hangar.
发明内容SUMMARY OF THE INVENTION
针对现有技术中的缺陷,本发明提供了一种无人机机库及其控制方法,以解决现有技术中,无人机充完电之后,起飞也是在充电位位置处就地起飞,为了保证无人机起飞时无人机机翼不会碰撞到无人机机库,无人机机库的停机坪的长度设置得比较长,造成无人机机库整体体积较大,增加了无人机机库的重量的问题。Aiming at the defects in the prior art, the present invention provides an unmanned aerial vehicle hangar and a control method thereof, so as to solve the problem that in the prior art, after the unmanned aerial vehicle is fully charged, the take-off is also taken off at the charging position. In order to ensure that the drone wings will not collide with the drone hangar when the drone takes off, the length of the apron of the drone hangar is set to be relatively long, resulting in a larger overall volume of the drone hangar, increasing the The weight of the drone hangar.
为了解决上述问题,本申请的实施例通过如下方式实现:In order to solve the above problems, the embodiments of the present application are implemented in the following ways:
本申请实施例提供了一种无人机机库,包括:The embodiment of the present application provides a hangar for an unmanned aerial vehicle, including:
箱体、设置在所述箱体内的停机坪,所述停机坪通过推动装置从所述箱体的侧面推出或从所述箱体的侧面推入所述箱体内;A box body and a parking pad arranged in the box body, the parking pad is pushed out from the side of the box body or pushed into the box body from the side of the box body by a pushing device;
所述停机坪设置有充电模块,用于为停放在所述停机坪的充电位上的所述无人机进行充电;The parking apron is provided with a charging module for charging the unmanned aerial vehicle parked on the charging position of the parking apron;
所述停机坪上设置有位置移动机构,用于在所述无人机降落在所述停机坪上后,将所述无人机的位置移动到所述充电位,还用于在所述无人机需要从所述停机坪起飞时,将所述无人机的位置从所述充电位移动到所述停机坪上的起飞位。The parking apron is provided with a position moving mechanism, which is used to move the position of the drone to the charging position after the drone lands on the parking pad, and is also used to move the drone to the charging position when the drone is landed on the parking pad. When the man-machine needs to take off from the apron, the position of the drone is moved from the charging position to the take-off position on the apron.
进一步地,所述停机坪从所述箱体内推出来后,所述充电位比所述起飞位更靠近所述箱体。Further, after the apron is pushed out of the box, the charging position is closer to the box than the take-off position.
进一步地,所述停机坪从所述箱体内推出来后,所述无人机在所述起飞位时,所述无人机靠近所述箱体的机翼距离所述箱体的所述停机坪的出口处大于等于预设距离。Further, after the parking pad is pushed out from the box, when the drone is in the take-off position, the drone is close to the wing of the box and is far away from the stop of the box. The exit of the ping is greater than or equal to the preset distance.
进一步地,所述预设距离为40厘米。Further, the preset distance is 40 cm.
进一步地,所述位置移动机构包括杆驱动机构和多个推动杆,所述多个推动杆分别沿所述停机坪的边沿设置;Further, the position moving mechanism includes a rod driving mechanism and a plurality of push rods, and the plurality of push rods are respectively arranged along the edge of the apron;
在所述无人机停靠在所述停机坪上后,所述杆驱动机构驱动所述推动杆移动进而带动所述无人机向所述充电位移动;After the drone is parked on the parking apron, the rod driving mechanism drives the push rod to move, thereby driving the drone to move to the charging position;
在所述无人机需要从所述停机坪起飞时,所述杆驱动机构驱动所述推动杆移动进而带动所述无人机向所述起飞位移动。When the drone needs to take off from the apron, the rod driving mechanism drives the push rod to move, thereby driving the drone to move to the take-off position.
进一步地,所述停机坪为方形板状结构;Further, the parking apron is a square plate-like structure;
所述推动杆设有四个,其中两个所述推动杆前后平行设置,另外两个所述推动杆左右平行设置;There are four push rods, two of which are arranged in parallel front and rear, and the other two are arranged in parallel left and right;
前后平行的两所述推动杆可沿前后相向或背向移动,左右平行的两所述推动杆可沿左右相向或背向移动。The two push rods parallel to the front and the rear can move in the front and back directions or backward, and the two push rods parallel to the left and right can move in the left and right directions or the back.
进一步地,在所述无人机停靠在所述停机坪上后,所述杆驱动机构驱动四个所述推动杆移动进而带动所述无人机向所述充电位移动;Further, after the drone is parked on the parking apron, the rod driving mechanism drives the four push rods to move, thereby driving the drone to move to the charging position;
在所述无人机需要从所述停机坪起飞时,所述杆驱动机构至少驱动目标推动杆移动进而带动所述无人机向所述起飞位移动,所述目标推动杆为四个所述推动杆中设置在所述停机坪的推出方向上、且所述停机坪处于完全推出状态时靠近所述箱体的所述推动杆。When the drone needs to take off from the apron, the rod driving mechanism drives at least a target push rod to move and then drives the drone to move to the take-off position, and the target push rods are four of the The push rod is disposed in the push-out direction of the apron and is close to the box when the apron is in a fully pushed-out state.
进一步地,所述充电模块为无线充电模块,用于为停放在所述停机坪的所述充电位上的所述无人机进行无线充电。Further, the charging module is a wireless charging module for wirelessly charging the drone parked on the charging position of the apron.
进一步地,所述箱体内设置至少两层所述停机坪,所述至少两层所述停机坪将所述箱体的内部空间从上至下划分为N个可容纳无人机的停机舱,所述N等于所述停机坪的数量。Further, at least two layers of the parking pads are arranged in the box, and the at least two layers of the parking pads divide the interior space of the box into N parking bays that can accommodate drones from top to bottom, The N is equal to the number of the parking pads.
本申请实施例还提供了一种基于上述任一项所述的无人机机库的控制方法,包括以下步骤:The embodiment of the present application also provides a control method based on any one of the above-mentioned UAV hangars, comprising the following steps:
在所述无人机机库接收到无人机发来的请求降落指令之后,通过推动装置将处于未停靠状态的停机坪从所述无人机机库的箱体的侧面推出以供所述无人机停靠;After the UAV hangar receives the request to land from the UAV, the parking pad in the undocked state is pushed out from the side of the box of the UAV hangar by the pushing device for the said UAV hangar. drone docking;
所述无人机降落在所述停机坪之后,通过所述停机坪上的位置移动机构将所述无人机的位置移动到所述停机坪上的充电位,通过所述推动装置将所述停机坪从所述箱体的侧面推入所述箱体内,通过所述充电位为所述无人机充电;After the drone landed on the apron, the position of the drone is moved to the charging position on the apron by the position moving mechanism on the apron, and the The apron is pushed into the box from the side of the box, and the drone is charged through the charging position;
在所述无人机需要从所述停机坪起飞时,通过所述推动装置将所述停机坪从所述箱体的侧面推出,通过所述位置移动机构将所述无人机的位置从所述充电位移动到所述停机坪上的起飞位。When the unmanned aerial vehicle needs to take off from the apron, the apron is pushed out from the side of the box by the pushing device, and the position of the unmanned aerial vehicle is moved from the position by the position moving mechanism. The charging position is moved to the take-off position on the apron.
有益效果beneficial effect
本申请提供了一种无人机机库及其控制方法,包括:箱体、设置在箱体内的停机坪,停机坪通过推动装置从箱体的侧面推出或从箱体的侧面推入箱体内;停机坪设置有充电模块,用于为停放在停机坪的充电位上的无人机进行充电;停机坪上设置有位置移动机构,用于在无人机降落在停机坪上后,将无人机的位置移动到充电位,还用于在无人机需要从停机坪起飞时,将无人机的位置从充电位移动到停机坪上的起飞位。通过在停机坪上设置无人机的充电位和起飞位,保证无人机能与充电位对准进行充电,同时在无人机需要从停机坪起飞时,将无人机的位置从充电位移动到起飞位,保证无人机起飞时无人机机翼不会碰撞到无人机机库,保证了无人机起飞的安全性,同时也缩短了无人机机库的停机坪的长度,减小了无人机机库整体体积,降低了无人机机库的重量。The present application provides an unmanned aerial vehicle hangar and a control method thereof, comprising: a box body and a parking pad arranged in the box body, the parking pad is pushed out from the side of the box body or pushed into the box body from the side of the box body by a pushing device ;The apron is provided with a charging module, which is used to charge the drone parked on the charging position of the apron; a position moving mechanism is set on the apron, which is used to recharge the drone after landing on the apron. The position of the man-machine is moved to the charging position, and is also used to move the position of the drone from the charging position to the take-off position on the apron when the drone needs to take off from the apron. By setting the charging position and take-off position of the drone on the apron, it is ensured that the drone can be aligned with the charging position for charging, and when the drone needs to take off from the apron, the position of the drone is moved from the charging position. At the take-off position, it ensures that the drone’s wings will not collide with the drone’s hangar when the drone takes off, which ensures the safety of the drone’s take-off, and also shortens the length of the apron of the drone’s hangar. The overall volume of the UAV hangar is reduced, and the weight of the UAV hangar is reduced.
附图说明Description of drawings
为了更清楚地说明本发明具体实施方式或现有技术中的技术方案,下面将对具体实施方式或现有技术描述中所需要使用的附图作简单地介绍。在所有附图中,类似的元件或部分一般由类似的附图标记标识。附图中,各元件或部分并不一定按照实际的比例绘制。In order to illustrate the specific embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that are required to be used in the description of the specific embodiments or the prior art. Similar elements or parts are generally identified by similar reference numerals throughout the drawings. In the drawings, each element or section is not necessarily drawn to actual scale.
图1为本实施例提供的一种无人机机库的示意图;1 is a schematic diagram of a UAV hangar provided by the present embodiment;
附图标记reference number
箱体10、停机坪20、充电位30、起飞位40、推动杆50。The
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
应当理解,当在本说明书和所附权利要求书中使用时,术语“包括”和“包含”指示所描述特征、整体、步骤、操作、元素和/或组件的存在,但并不排除一个或多个其它特征、整体、步骤、操作、元素、组件和/或其集合的存在或添加。It is to be understood that, when used in this specification and the appended claims, the terms "comprising" and "comprising" indicate the presence of the described features, integers, steps, operations, elements and/or components, but do not exclude one or The presence or addition of a number of other features, integers, steps, operations, elements, components, and/or sets thereof.
还应当理解,在本发明说明书中所使用的术语仅仅是出于描述特定实施例的目的而并不意在限制本发明。如在本发明说明书和所附权利要求书中所使用的那样,除非上下文清楚地指明其它情况,否则单数形式的“一”、“一个”及“该”意在包括复数形式。It should also be understood that the terminology used in the present specification is for the purpose of describing particular embodiments only and is not intended to limit the present invention. As used in this specification and the appended claims, the singular forms "a," "an," and "the" are intended to include the plural unless the context clearly dictates otherwise.
还应当进一步理解,在本发明说明书和所附权利要求书中使用的术语“和/或”是指相关联列出的项中的一个或多个的任何组合以及所有可能组合,并且包括这些组合。It should further be understood that, as used in this specification and the appended claims, the term "and/or" refers to and including any and all possible combinations of one or more of the associated listed items .
实施例一Example 1
为了解决现有技术中,无人机在无人机机库上充完电之后,起飞也是在无人机机库的充电位位置处就地起飞,为了保证无人机起飞时无人机机翼不会碰撞到无人机机库,无人机机库的停机坪的长度设置得比较长,造成无人机机库整体体积较大,增加了无人机机库的重量的问题,本实施例提出一种无人机机库,参见图1,无人机机库包括:In order to solve the problem in the prior art, after the UAV is charged on the UAV hangar, the take-off also takes off at the charging position of the UAV hangar. In order to ensure that the UAV takes off when the UAV takes off The wings will not collide with the UAV hangar. The length of the apron of the UAV hangar is set relatively long, which causes the overall volume of the UAV hangar to be larger and increases the weight of the UAV hangar. The embodiment provides an unmanned aerial vehicle hangar. Referring to FIG. 1, the unmanned aerial vehicle hangar includes:
箱体10、设置在箱体10内的停机坪20,停机坪20通过推动装置从箱体10的侧面推出或从箱体10的侧面推入箱体10内。The
停机坪20设置有充电模块,用于为停放在停机坪20的充电位30上的无人机进行充电。充电模块可以采用接触式充电,也可以采用非接触式充电,在一种实施方式中,充电模块为无线充电模块,用于为停放在停机坪20的充电位30上的无人机进行无线充电,无线充电模块可以采用发射线圈来实现,可以将发射线圈设置在停机坪20的下方,对应的在无人机上设置接收线圈以接收发射线圈传递过来的能量。无人机在停机坪20上充电时,一般是停机坪20完全位于箱体10内,考虑到无人机的翼展,为了最大限度的利用停机坪20的空间,可选地,在本实施例中,设置充电位位于停机坪20的中部,以充分利用停机坪20空间。对于无线充电的情况,接收线圈可能设置在无人机的不同位置,比如无人机两个脚架的其中一个脚架上,或者位于无人机两个脚架之间且位于脚架的后半部分位置,本实施例中,在设置停机坪20的充电位30时,可以将无人机脚架所占停机坪20的整个空间划分为充电位30,例如某种无人机脚架在停机坪20上的投影呈“11”字型,则无人机脚架所占停机坪20的整个空间为将“11”字型首尾相连后形成的“口”字型,也即“口”字型所占的区域为充电位30。可选地,充电位30可以大于等于无人机脚架所占停机坪20的整个空间。The
停机坪20上设置有位置移动机构,用于在无人机降落在停机坪20上后,将无人机的位置移动到充电位30,还用于在无人机需要从停机坪20起飞时,将无人机的位置从充电位30移动到停机坪上的起飞位40。The
通过在停机坪20上设置无人机的充电位30和起飞位40,保证无人机能与充电位30对准进行充电,同时在无人机需要从停机坪20起飞时,将无人机的位置从充电位30移动到起飞位40,保证无人机起飞时无人机机翼不会碰撞到无人机机库,保证了无人机起飞的安全性,同时也缩短了无人机机库的停机坪20的长度,减小了无人机机库整体体积,降低了无人机机库的重量。By setting the UAV's
可选地,在本实施例中,停机坪20从箱体10内推出来后,充电位30比起飞位40更靠近箱体10。将起飞位40设置为远离箱体10的方向,尽可能地避免了无人机起飞时无人机机翼碰撞到无人机机库情况的发生。Optionally, in this embodiment, after the
可选地,在本实施例中,停机坪20从箱体10内推出来后,无人机在起飞位40时,无人机靠近箱体10的机翼距离箱体10的停机坪20的出口处大于等于预设距离。在设置起飞位40时,可以考虑停机坪20从箱体10内推出来后,最靠近箱体10的无人机机翼与箱体10的停机坪20的出口处的距离设置为大于等于预设距离,以尽可能地避免无人机起飞时无人机机翼碰撞到无人机机库,从而保证无人机的顺利起飞。在一种实施方式中,预设距离为40厘米,也即无人机起飞安全间距大于等于40厘米。Optionally, in this embodiment, after the
可选地,在本实施例中,位置移动机构包括杆驱动机构和多个推动杆50,多个推动杆50分别沿停机坪20的边沿设置;Optionally, in this embodiment, the position moving mechanism includes a rod driving mechanism and a plurality of
在无人机停靠在停机坪20上后,杆驱动机构驱动推动杆50移动进而带动无人机向充电位30移动;After the drone is parked on the
在无人机需要从停机坪20起飞时,杆驱动机构驱动推动杆50移动进而带动无人机向起飞位40移动。When the drone needs to take off from the
可选地,在本实施例中,停机坪20为方形板状结构;Optionally, in this embodiment, the
推动杆50设有四个,其中两个推动杆50前后平行设置,另外两个推动杆50左右平行设置;There are four
前后平行的两推动杆50可沿前后相向或背向移动,左右平行的两推动杆50可沿左右相向或背向移动。The two
可选地,在本实施例中,在无人机停靠在停机坪20上后,杆驱动机构驱动四个推动杆50移动进而带动无人机向充电位30移动;Optionally, in this embodiment, after the drone is parked on the
在无人机需要从停机坪20起飞时,杆驱动机构至少驱动目标推动杆50移动进而带动无人机向起飞位40移动,目标推动杆50为四个推动杆50中设置在停机坪20的推出方向上、且停机坪20处于完全推出状态时靠近箱体10的推动杆50。When the drone needs to take off from the
本实施例中,当无人机停靠在停机坪20上后,杆驱动机构开始工作,停机坪20的左侧推动杆50和右侧推动杆50相向的朝停机坪20的充电位30移动,停机坪20的前侧推动杆50和后侧推动杆50相向的朝停机坪20的充电位30移动。在四个推动杆50的推动下,没有停靠在停机坪20的充电位30的无人机朝向充电位30移动,保证了顺利地对无人机进行充电。在将无人机移动到停机坪20的充电位30后,在杆驱动机构的驱动下,四个推动杆50回到原位,回到靠近停机坪20边沿的位置。停机坪20处于完全推出状态时,若在停机坪20的推出方向上、且靠近箱体10的停机坪20出口处的推动杆50为左侧推动杆50,在停机坪20的推出方向上、且远离箱体10的停机坪20出口处的推动杆50为右侧推动杆50,在无人机充完电需要起飞时,左侧推动杆50朝停机坪20的起飞位40移动,进而带动无人机从充电位30移动到起飞位40。在将无人机从充电位30推动到起飞位40时,除了只采用左侧推动杆50工作的方案外,还可以采用左侧推动杆50和前侧推动杆50共同工作,或者采用左侧推动杆50和后侧推动杆50共同工作,或者采用左侧推动杆50、前侧推动杆50和后侧推动杆50共同工作的方案。In this embodiment, when the drone is parked on the
可选地,在本实施例中,箱体10内设置至少两层停机坪20,至少两层停机坪20将箱体10的内部空间从上至下划分为N个可容纳无人机的停机舱,N等于停机坪20的数量,也即停机舱的数量等于停机坪20的数量;每层停机坪20通过对应的推动装置从箱体10内推出或推入箱体10内。本实施例中的至少两层停机坪20的推出方向可以是同向,例如全部都从箱体10的右侧推出,也可以是不同向,例如至少一层停机坪20从箱体10的左侧推出,至少一层停机坪20从箱体10的右侧推出。Optionally, in this embodiment, at least two layers of
实施例二Embodiment 2
本实施例提出一种基于实施例一任一项的无人机机库的控制方法,无人机机库的结构和功能参见实施例一中的描述,这里不再赘述,方法包括以下步骤:This embodiment proposes a method for controlling the unmanned aerial vehicle hangar based on any one of the embodiments. For the structure and function of the unmanned aerial vehicle hangar, refer to the description in the first embodiment, which will not be repeated here. The method includes the following steps:
S1、在所述无人机机库接收到无人机发来的请求降落指令之后,通过无人机机库的推动装置将处于未停靠状态的停机坪20从所述无人机机库的箱体10的侧面推出以供所述无人机停靠。S1. After the unmanned aerial vehicle hangar receives the request to land from the unmanned aerial vehicle hangar, the
S2、所述无人机降落在所述停机坪20之后,通过所述停机坪20上的位置移动机构将所述无人机的位置移动到所述停机坪20上的充电位30,通过所述推动装置将所述停机坪20从所述箱体10的侧面推入所述箱体10内,然后通过所述充电位30为所述无人机充电;S2. After the drone lands on the
无人机降落在所述停机坪20上,其降落位置相对于充电位30很大几率存在偏移情况,若不先将无人机移动到充电位30便将停机坪20推入箱体10内,则无人机可能与箱体10形成碰撞,无人机无法顺利进入箱体10内,所以在将停机坪20推入箱体10内之前,需要先将无人机移动到充电位30,保证无人机顺利进入箱体10内。When the drone lands on the
S3、在所述无人机需要从所述停机坪20起飞时,通过所述推动装置将所述停机坪20从所述箱体10的侧面推出,通过所述位置移动机构将所述无人机的位置从所述充电位30移动到所述停机坪20上的起飞位40。S3. When the UAV needs to take off from the
本实施例通过在停机坪20上设置无人机的充电位30和起飞位40,保证无人机能与充电位30对准进行充电,同时在无人机需要从停机坪20起飞时,将无人机的位置从充电位30移动到起飞位40,保证无人机起飞时无人机机翼不会碰撞到无人机机库,保证了无人机起飞的安全性,同时也缩短了无人机机库的停机坪20的长度,减小了无人机机库整体体积,降低了无人机机库的重量。In this embodiment, by setting the charging
本领域普通技术人员可以意识到,结合本文中所公开的实施例描述的各示例的单元,能够以电子硬件、计算机软件或者二者的结合来实现,为了清楚地说明硬件和软件的可互换性,在上述说明中已经按照功能一般性地描述了各示例的组成。这些功能究竟以硬件还是软件方式来执行,取决于技术方案的特定应用和设计约束条件。专业技术人员可以对每个特定的应用来使用不同方法来实现所描述的功能,但是这种实现不应认为超出本发明的范围。Those of ordinary skill in the art can realize that the units of each example described in conjunction with the embodiments disclosed herein can be implemented in electronic hardware, computer software, or a combination of the two, in order to clearly illustrate the interchangeability of hardware and software In the above description, the composition of each example has been described generally in terms of function. Whether these functions are performed in hardware or software depends on the specific application and design constraints of the technical solution. Skilled artisans may implement the described functionality using different methods for each particular application, but such implementations should not be considered beyond the scope of the present invention.
在本申请所提供的实施例中,应该理解到,单元的划分,仅仅为一种逻辑功能划分,实际实现时可以有另外的划分方式,例如多个单元可结合为一个单元,一个单元可拆分为多个单元,或一些特征可以忽略等。In the embodiments provided in this application, it should be understood that the division of units is only a logical function division. In actual implementation, there may be other division methods. For example, multiple units may be combined into one unit, and one unit may be detached. Divided into multiple units, or some features can be ignored, etc.
最后应说明的是:以上各实施例仅用以说明本发明的技术方案,而非对其限制;尽管参照前述各实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分或者全部技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的范围,其均应涵盖在本发明的权利要求和说明书的范围当中。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, but not to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: The technical solutions described in the foregoing embodiments can still be modified, or some or all of the technical features thereof can be equivalently replaced; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the technical solutions of the embodiments of the present invention. The scope of the invention should be included in the scope of the claims and description of the present invention.
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