WO2017035983A1 - Circuit integration device for unmanned aerial vehicle - Google Patents

Circuit integration device for unmanned aerial vehicle Download PDF

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Publication number
WO2017035983A1
WO2017035983A1 PCT/CN2015/097435 CN2015097435W WO2017035983A1 WO 2017035983 A1 WO2017035983 A1 WO 2017035983A1 CN 2015097435 W CN2015097435 W CN 2015097435W WO 2017035983 A1 WO2017035983 A1 WO 2017035983A1
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module
interface
power
circuit board
control
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PCT/CN2015/097435
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French (fr)
Chinese (zh)
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杨华东
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杨华东
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    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00—Programme-control systems
    • G05B19/02—Programme-control systems electric
    • G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/72—Means for accommodating flexible lead within the holder

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  • the present application belongs to the technical field of unmanned aerial vehicles, and particularly relates to a drone assembly device.
  • connection lines including power supply, voltmeter, galvanometer, GPS, digital transmission, airspeed sensor, navigation light and other connection lines.
  • the connection lines are intertwined. Installation is time consuming and requires a one-to-one connection by a professional.
  • the existing drones usually use two power sources to supply power to the circuit modules, which are large in weight and volume, and high in cost.
  • the present invention provides the following technical solutions:
  • the embodiment of the present application discloses a UAV hub device, including a circuit board, and a control module, a video switching module, a power conversion module, and a peripheral interface integrated on the circuit board, where the video switching module is connected to the An output end of the control module, the power conversion module is connected to an external power source and converts the input voltage, including the first power module, the second power module, and the third power module, and the external power source passes through the first power module,
  • the two power modules and the third power module respectively output 5V, 12V, and 3.3V voltages
  • the peripheral interface includes three video signal input interfaces connected to the input end of the video switching module; and the navigation light connected to the output end of the control module An interface;
  • the flight control interface includes a connector plugged into the flight control interface and an FPC flexible cable connected between the connector and the circuit board; and a power interface connected to the power conversion module and extending out of the circuit board through the wire outer.
  • the navigation light interface includes a left navigation light interface, a right navigation light interface, and a tail light interface.
  • the circuit board includes a first circuit board and a second circuit board which are oppositely disposed, and the control module, the video switching module, the airspeed sensor, and the peripheral interface are integrated in the first On the circuit board, the power conversion module, the voltmeter, and the ammeter are integrated on the second circuit board.
  • control module is preferably STC15F204EA.
  • an airspeed sensor, a voltmeter and an ammeter are integrated on the circuit board, and the airspeed sensor is used to detect the flight speed of the drone in real time, and passes through the flight control interface.
  • the signal is transmitted to the flight control, the voltmeter is connected to the external power supply, the residual voltage of the power supply is detected in real time, and the detection signal is transmitted to the controller in real time, and the current meter is used to measure the current of the entire power supply system, and the data is passed through the flight control interface in real time. Transfer to the flight control.
  • the peripheral interface further includes a GPS interface, is connected to an external GPS module, and can supply power to the GPS module.
  • the peripheral interface further includes a digital transmission interface and an expansion interface.
  • the peripheral interface further includes a flap interface, the flap interface is connected to the controller, and can be plugged with an external flap connection line, and the controller receives the space in real time.
  • the controller controls the flap to automatically retract; when the airspeed is less than the set value, the controller controls the flap to be automatically lowered.
  • the invention Compared with the prior art, the invention has the advantages that the invention integrates the existing multiple lines into one device, can realize rapid assembly, is convenient to operate, and reduces cost; the invention is applied to the drone, and can pass A power supply provides voltage supply to a variety of different circuit modules.
  • FIG. 1 is a schematic diagram showing the principle of a line assembly device for a drone according to a specific embodiment of the present invention.
  • the UAV hub device includes a circuit board, and a control module, a video switching module, a power conversion module, an airspeed sensor, a voltmeter, an ammeter, and a peripheral interface integrated on the circuit board.
  • the circuit board includes a first circuit board and a second circuit board which are oppositely disposed, the control module, the video switching module, the airspeed sensor, and the peripheral interface are integrated on the first circuit board, and the power conversion module, the voltmeter and the ammeter are integrated in the first Two circuit boards.
  • the control module is preferably STC15F204EA.
  • a video switching module is coupled to the output of the control module. According to the control signal of the control module, one of the input multiple channels of video is selected for output.
  • the power conversion module is connected to an external power source and converts the input voltage, including the first power module, the second power module, and the third power module, and the external power source passes through the first power module, the second power module, and the third power module After that, 5V, 12V, and 3.3V voltages are respectively output.
  • the 5V voltage supplies power to the control module, airspeed meter and video switching module, and supplies power to the external steering gear and navigation light through the peripheral interface; 12V voltage supplies power to the picture transmission module, camera and pan/tilt through the peripheral interface; 3.3V voltage passes The peripheral interface supplies power to the GPS.
  • the airspeed sensor is used to detect the flight speed of the drone in real time and transmit the signal to the controller and flight controller.
  • the voltmeter is connected to an external power supply to detect the residual voltage of the power supply in real time, and transmits the detection signal to the controller in real time.
  • the controller controls the alarm light to flash when the power is lower than the set value.
  • An ammeter to measure the current of the entire power supply system. And transmit the data to the flight controller in real time.
  • Peripheral interfaces include:
  • Three video signal input interfaces connected to the input end of the video switching module
  • An navigation light interface connected to an output end of the control module, the navigation light interface includes a left navigation light interface, a right navigation light interface, and a taillight light interface
  • the flight control interface includes a connector plugged into the flight control interface and an FPC flexible cable connected between the connector and the circuit board, and the FPC flexible cable and the voltmeter, ammeter, and video switching module respectively on the circuit board Airspeed sensor connection.
  • the power interface is connected to the power conversion module and extends out of the circuit board through wires.
  • the GPS interface is connected to an external GPS module and can supply power to the GPS module.
  • the flap interface is connected to the controller and can be connected with an external flap connection line, and the controller receives the data of the airspeed sensor in real time. When the airspeed is greater than the set value, the controller controls the flap automatically. Collapse; when the airspeed is less than the set value, the controller controls the flap to be automatically lowered.
  • a digital transmission interface and an expansion interface may also be included.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
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  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Provided is a circuit integration device for an unmanned aerial vehicle, comprising: a circuit board, and a control module, a video switching module, a power conversion module and peripheral interfaces integrated on the circuit board. The video switching module is connected to an output terminal of the control module. The power conversion module is connected to an external power supply to convert an inputted voltage. The power conversion module comprises a first power module, a second power module and a third power module. The external power supply outputs a 5 V voltage, a 12 V voltage and a 3.3 V voltage respectively via the first power module, the second power module and the third power module. The peripheral interfaces comprise 3 video signal input interfaces, a navigation light interface, a flight control interface and a power interface. The circuit integration device integrates multiple existing circuits into one device, thereby achieving rapid assembly, simple operation and reduced costs. The circuit integration device can be applied to an unmanned aerial vehicle to supply voltages to various different circuit modules by one power supply.

Description

无人机集线装置UAV hub 技术领域Technical field
本申请属于无人飞行器技术领域，特别是涉及一种无人机集线装置。The present application belongs to the technical field of unmanned aerial vehicles, and particularly relates to a drone assembly device.
背景技术Background technique
现有无人飞行器中，存在复杂的接线线路，包括电源、电压计、电流计、GPS、数字传输、空速传感器、航灯等多种连接线路，在连接过程中，连接线交织在一起，安装耗时大，而且需要专业人员进行一一连接。In the existing unmanned aerial vehicles, there are complicated wiring lines, including power supply, voltmeter, galvanometer, GPS, digital transmission, airspeed sensor, navigation light and other connection lines. During the connection process, the connection lines are intertwined. Installation is time consuming and requires a one-to-one connection by a professional.
另外，现有的无人机通常采用2个电源对电路模块进行供电，重量和体积都较大，成本高。In addition, the existing drones usually use two power sources to supply power to the circuit modules, which are large in weight and volume, and high in cost.
发明内容Summary of the invention
本发明的目的在于提供一种无人机集线装置，以克服现有技术中的不足。It is an object of the present invention to provide a drone gathering device that overcomes the deficiencies of the prior art.
为实现上述目的，本发明提供如下技术方案：To achieve the above object, the present invention provides the following technical solutions:
本申请实施例公开了一种无人机集线装置，包括电路板、以及集成于所述电路板上的控制模块、视频切换模块、电源转换模块和外围接口，所述视频切换模块连接于所述控制模块的输出端，所述电源转换模块与外部的电源连接并对输入的电压进行转换，包括第一电源模块、第二电源模块和第三电源模块，外部电源经过第一电源模块、第二电源模块和第三电源模块后分别输出5V、12V和3.3V电压，所述外围接口包括连接于所述视频切换模块输入端的3个视频信号输入接口；连接于所述控制模块输出端的航灯接口；飞控接口，包括与飞控接口插接的连接头以及连接在连接头和电路板之间的FPC软排线；以及电源接口，连接于电源转换模块并通过导线延伸出所述电路板外。 The embodiment of the present application discloses a UAV hub device, including a circuit board, and a control module, a video switching module, a power conversion module, and a peripheral interface integrated on the circuit board, where the video switching module is connected to the An output end of the control module, the power conversion module is connected to an external power source and converts the input voltage, including the first power module, the second power module, and the third power module, and the external power source passes through the first power module, The two power modules and the third power module respectively output 5V, 12V, and 3.3V voltages, and the peripheral interface includes three video signal input interfaces connected to the input end of the video switching module; and the navigation light connected to the output end of the control module An interface; the flight control interface includes a connector plugged into the flight control interface and an FPC flexible cable connected between the connector and the circuit board; and a power interface connected to the power conversion module and extending out of the circuit board through the wire outer.
优选的，在上述的无人机集线装置中，所述航灯接口包括左航灯接口、右航灯接口和尾航灯接口Preferably, in the above-mentioned UAV hub device, the navigation light interface includes a left navigation light interface, a right navigation light interface, and a tail light interface.
优选的，在上述的无人机集线装置中，所述电路板包括相对设置的第一电路板和第二电路板，控制模块、视频切换模块、空速传感器、和外围接口集成于第一电路板上，电源转换模块、电压计和电流计集成于第二电路板上。Preferably, in the above-mentioned UAV hub device, the circuit board includes a first circuit board and a second circuit board which are oppositely disposed, and the control module, the video switching module, the airspeed sensor, and the peripheral interface are integrated in the first On the circuit board, the power conversion module, the voltmeter, and the ammeter are integrated on the second circuit board.
优选的，在上述的无人机集线装置中，所述控制模块优选为STC15F204EA。Preferably, in the above-mentioned UAV hub device, the control module is preferably STC15F204EA.
优选的，在上述的无人机集线装置中，所述电路板上还集成有空速传感器、电压计和电流计，空速传感器用以实时检测无人机飞行速度，并通过飞控接口将信号传输给飞控，电压计连接于外部的电源，实时检测电源剩余电压，并将检测信号实时传递给控制器，电流计用以测量整个供电系统的电流，并将数据通过飞控接口实时传输给飞控。Preferably, in the above-mentioned UAV hub device, an airspeed sensor, a voltmeter and an ammeter are integrated on the circuit board, and the airspeed sensor is used to detect the flight speed of the drone in real time, and passes through the flight control interface. The signal is transmitted to the flight control, the voltmeter is connected to the external power supply, the residual voltage of the power supply is detected in real time, and the detection signal is transmitted to the controller in real time, and the current meter is used to measure the current of the entire power supply system, and the data is passed through the flight control interface in real time. Transfer to the flight control.
优选的，在上述的无人机集线装置中，所述外围接口还包括GPS接口，与外部的GPS模块连接，并可为GPS模块供电。Preferably, in the above-mentioned UAV hub device, the peripheral interface further includes a GPS interface, is connected to an external GPS module, and can supply power to the GPS module.
优选的，在上述的无人机集线装置中，所述外围接口还包括数字传输接口和扩展接口。Preferably, in the above-mentioned UAV hub device, the peripheral interface further includes a digital transmission interface and an expansion interface.
优选的，在上述的无人机集线装置中，所述外围接口还包括襟翼接口，该襟翼接口与控制器连接，并可与外部的襟翼连接线插接，控制器实时接收空速传感器的数据，在空速大于设定值时，控制器控制襟翼自动收起；在空速小于设定值时，控制器控制襟翼自动放下。Preferably, in the above-mentioned UAV hub device, the peripheral interface further includes a flap interface, the flap interface is connected to the controller, and can be plugged with an external flap connection line, and the controller receives the space in real time. For the data of the speed sensor, when the airspeed is greater than the set value, the controller controls the flap to automatically retract; when the airspeed is less than the set value, the controller controls the flap to be automatically lowered.
与现有技术相比，本发明的优点在于：本发明将现有的多种线路集成到一个装置中，可以实现快速组装，操作方便，降低成本；本发明应用于无人机中，可以通过一个电源实现对多种不同电路模块的电压供应。Compared with the prior art, the invention has the advantages that the invention integrates the existing multiple lines into one device, can realize rapid assembly, is convenient to operate, and reduces cost; the invention is applied to the drone, and can pass A power supply provides voltage supply to a variety of different circuit modules.
附图说明DRAWINGS
为了更清楚地说明本申请实施例或现有技术中的技术方案，下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本申请中记载的一些实施例，对于本领域普通技术人员 来讲，在不付出创造性劳动的前提下，还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings to be used in the embodiments or the prior art description will be briefly described below. Obviously, the drawings in the following description are only Some embodiments described in this application are for those of ordinary skill in the art In other words, other drawings can be obtained from these drawings without any creative work.
图1所示为本发明具体实施例中无人机集线装置的原理示意图。FIG. 1 is a schematic diagram showing the principle of a line assembly device for a drone according to a specific embodiment of the present invention.
具体实施方式detailed description
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详细的描述，显然，所描述的实施例仅仅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的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 are described in detail below with reference to the accompanying drawings in the embodiments of the present invention. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without creative efforts are within the scope of the present invention.
无人机集线装置，包括电路板、以及集成于所述电路板上的控制模块、视频切换模块、电源转换模块、空速传感器、电压计、电流计和外围接口。The UAV hub device includes a circuit board, and a control module, a video switching module, a power conversion module, an airspeed sensor, a voltmeter, an ammeter, and a peripheral interface integrated on the circuit board.
电路板包括相对设置的第一电路板和第二电路板，控制模块、视频切换模块、空速传感器、和外围接口集成于第一电路板上，电源转换模块、电压计和电流计集成于第二电路板上。The circuit board includes a first circuit board and a second circuit board which are oppositely disposed, the control module, the video switching module, the airspeed sensor, and the peripheral interface are integrated on the first circuit board, and the power conversion module, the voltmeter and the ammeter are integrated in the first Two circuit boards.
控制模块优选为STC15F204EA。The control module is preferably STC15F204EA.
视频切换模块，连接于所述控制模块的输出端。根据控制模块的控制信号，选择将输入的多路视频中的其中一路输出。A video switching module is coupled to the output of the control module. According to the control signal of the control module, one of the input multiple channels of video is selected for output.
电源转换模块，与外部的电源连接并对输入的电压进行转换，包括第一电源模块、第二电源模块和第三电源模块，外部电源经过第一电源模块、第二电源模块和第三电源模块后分别输出5V、12V和3.3V电压。其中5V电压给控制模块、空速计、视频切换模块供电，并通过外围接口给外部的舵机、航灯供电；12V电压通过外围接口给图传模块、摄像头和云台供电；3.3V电压通过外围接口给GPS供电。The power conversion module is connected to an external power source and converts the input voltage, including the first power module, the second power module, and the third power module, and the external power source passes through the first power module, the second power module, and the third power module After that, 5V, 12V, and 3.3V voltages are respectively output. The 5V voltage supplies power to the control module, airspeed meter and video switching module, and supplies power to the external steering gear and navigation light through the peripheral interface; 12V voltage supplies power to the picture transmission module, camera and pan/tilt through the peripheral interface; 3.3V voltage passes The peripheral interface supplies power to the GPS.
空速传感器用以实时检测无人机飞行速度，并将信号传输给控制器和飞控。The airspeed sensor is used to detect the flight speed of the drone in real time and transmit the signal to the controller and flight controller.
电压计，连接于外部的电源，实时检测电源剩余电压，并将检测信号实时传递给控制器，控制器在电量低于设定值时控制报警灯闪烁。The voltmeter is connected to an external power supply to detect the residual voltage of the power supply in real time, and transmits the detection signal to the controller in real time. The controller controls the alarm light to flash when the power is lower than the set value.
电流计，用以测量整个供电系统的电流。并将数据实时传输给飞控。An ammeter to measure the current of the entire power supply system. And transmit the data to the flight controller in real time.
外围接口包括： Peripheral interfaces include:
连接于所述视频切换模块输入端的3个视频信号输入接口；Three video signal input interfaces connected to the input end of the video switching module;
连接于所述控制模块输出端的航灯接口，航灯接口包括左航灯接口、右航灯接口和尾航灯接口An navigation light interface connected to an output end of the control module, the navigation light interface includes a left navigation light interface, a right navigation light interface, and a taillight light interface
飞控接口，包括与飞控接口插接的连接头以及连接在连接头和电路板之间的FPC软排线，该FPC软排线分别与电路板上的电压计、电流计、视频切换模块、空速传感器连接。The flight control interface includes a connector plugged into the flight control interface and an FPC flexible cable connected between the connector and the circuit board, and the FPC flexible cable and the voltmeter, ammeter, and video switching module respectively on the circuit board Airspeed sensor connection.
电源接口，连接于电源转换模块并通过导线延伸出所述电路板外。The power interface is connected to the power conversion module and extends out of the circuit board through wires.
GPS接口，与外部的GPS模块连接，并可为GPS模块供电。The GPS interface is connected to an external GPS module and can supply power to the GPS module.
襟翼接口，该襟翼接口与控制器连接，并可与外部的襟翼连接线插接，控制器实时接收空速传感器的数据，在空速大于设定值时，控制器控制襟翼自动收起；在空速小于设定值时，控制器控制襟翼自动放下。The flap interface is connected to the controller and can be connected with an external flap connection line, and the controller receives the data of the airspeed sensor in real time. When the airspeed is greater than the set value, the controller controls the flap automatically. Collapse; when the airspeed is less than the set value, the controller controls the flap to be automatically lowered.
还可以包括数字传输接口和扩展接口。A digital transmission interface and an expansion interface may also be included.
需要说明的是，在本文中，诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来，而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且，术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含，从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素，而且还包括没有明确列出的其他要素，或者是还包括为这种过程、方法、物品或者设备所固有的要素。在没有更多限制的情况下，由语句“包括一个……”限定的要素，并不排除在包括所述要素的过程、方法、物品或者设备中还存在另外的相同要素。It should be noted that, in this context, relational terms such as first and second are used merely to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply such entities or operations. There is any such actual relationship or order between them. Furthermore, the term "comprises" or "comprises" or "comprises" or any other variations thereof is intended to encompass a non-exclusive inclusion, such that a process, method, article, or device that comprises a plurality of elements includes not only those elements but also Other elements, or elements that are inherent to such a process, method, item, or device. An element that is defined by the phrase "comprising a ..." does not exclude the presence of additional equivalent elements in the process, method, item, or device that comprises the element.
以上所述仅是本申请的具体实施方式，应当指出，对于本技术领域的普通技术人员来说，在不脱离本申请原理的前提下，还可以做出若干改进和润饰，这些改进和润饰也应视为本申请的保护范围。 The above description is only a specific embodiment of the present application, and it should be noted that those skilled in the art can also make several improvements and retouchings without departing from the principles of the present application. It should be considered as the scope of protection of this application.

Claims (8)

  1. 一种无人机集线装置，其特征在于，包括电路板、以及集成于所述电路板上的控制模块、视频切换模块、电源转换模块和外围接口，所述视频切换模块连接于所述控制模块的输出端，所述电源转换模块与外部的电源连接并对输入的电压进行转换，包括第一电源模块、第二电源模块和第三电源模块，外部电源经过第一电源模块、第二电源模块和第三电源模块后分别输出5V、12V和3.3V电压，所述外围接口包括连接于所述视频切换模块输入端的3个视频信号输入接口；连接于所述控制模块输出端的航灯接口；飞控接口，包括与飞控接口插接的连接头以及连接在连接头和电路板之间的FPC软排线；以及电源接口，连接于电源转换模块并通过导线延伸出所述电路板外。A UAV hub device, comprising: a circuit board, and a control module, a video switching module, a power conversion module, and a peripheral interface integrated on the circuit board, wherein the video switching module is connected to the control An output end of the module, the power conversion module is connected to an external power source and converts the input voltage, including the first power module, the second power module, and the third power module, and the external power source passes through the first power module and the second power source The module and the third power module respectively output 5V, 12V and 3.3V voltages, the peripheral interface comprises three video signal input interfaces connected to the input end of the video switching module; and the navigation light interface connected to the output end of the control module; The flight control interface includes a connector plugged into the flight control interface and an FPC flexible cable connected between the connector and the circuit board; and a power interface connected to the power conversion module and extending out of the circuit board through the wire.
  2. 根据权利要求1所述的无人机集线装置，其特征在于：所述航灯接口包括左航灯接口、右航灯接口和尾航灯接口The UAV hub device according to claim 1, wherein the navigation light interface comprises a left navigation light interface, a right navigation light interface, and a taillight interface.
  3. 根据权利要求1所述的无人机集线装置，其特征在于：所述电路板包括相对设置的第一电路板和第二电路板，控制模块、视频切换模块、空速传感器、和外围接口集成于第一电路板上，电源转换模块、电压计和电流计集成于第二电路板上。The UAV hub device according to claim 1, wherein the circuit board comprises a first circuit board and a second circuit board disposed opposite to each other, a control module, a video switching module, an airspeed sensor, and a peripheral interface. Integrated on the first circuit board, the power conversion module, voltmeter and galvanometer are integrated on the second circuit board.
  4. 根据权利要求1所述的无人机集线装置，其特征在于：所述控制模块优选为STC15F204EA。The UAV hub apparatus according to claim 1, wherein said control module is preferably STC15F204EA.
  5. 根据权利要求1所述的无人机集线装置，其特征在于：所述电路板上还集成有空速传感器、电压计和电流计，空速传感器用以实时检测无人机飞行速度，并通过飞控接口将信号传输给飞控，电压计连接于外部的电源，实时检测电源剩余电压，并将检测信号实时传递给控制器，电流计用以测量整个供电系统的电流，并将数据通过飞控接口实时传输给飞控。The UAV hub device according to claim 1, wherein the circuit board is further integrated with an airspeed sensor, a voltmeter and an ammeter, and the airspeed sensor is used for detecting the flight speed of the drone in real time, and The signal is transmitted to the flight control through the flight control interface. The voltmeter is connected to the external power supply to detect the residual voltage of the power supply in real time, and the detection signal is transmitted to the controller in real time. The current meter measures the current of the entire power supply system and passes the data. The flight control interface is transmitted to the flight controller in real time.
  6. 根据权利要求1所述的无人机集线装置，其特征在于：所述外围接口还包括GPS接口，与外部的GPS模块连接，并可为GPS模块供电。The UAV hub apparatus according to claim 1, wherein the peripheral interface further comprises a GPS interface, is connected to an external GPS module, and can supply power to the GPS module.
  7. 根据权利要求1所述的无人机集线装置，其特征在于：所述外围接口还包括数字传输接口和扩展接口。The UAV hub apparatus according to claim 1, wherein said peripheral interface further comprises a digital transmission interface and an expansion interface.
  8. 根据权利要求1所述的无人机集线装置，其特征在于：所述外围接口还包括襟翼接口，该襟翼接口与控制器连接，并可与外部的襟翼连接线插接，控制器实时接收空速传感器的数据，在空速大于设定值时，控制器控制襟翼 自动收起；在空速小于设定值时，控制器控制襟翼自动放下。 The UAV hub apparatus according to claim 1, wherein the peripheral interface further comprises a flap interface, the flap interface is connected to the controller, and can be connected to an external flap connection line to control The device receives the data of the airspeed sensor in real time, and the controller controls the flap when the airspeed is greater than the set value. Automatically stowed; when the airspeed is less than the set value, the controller controls the flap to be automatically lowered.
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