WO2020087696A1 - 微型计算机系统及无人机 - Google Patents

微型计算机系统及无人机 Download PDF

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Publication number
WO2020087696A1
WO2020087696A1 PCT/CN2018/122059 CN2018122059W WO2020087696A1 WO 2020087696 A1 WO2020087696 A1 WO 2020087696A1 CN 2018122059 W CN2018122059 W CN 2018122059W WO 2020087696 A1 WO2020087696 A1 WO 2020087696A1
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WIPO (PCT)
Prior art keywords
microcomputer
accessory
interface
mounting
along
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Ceased
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PCT/CN2018/122059
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English (en)
French (fr)
Inventor
任冠男
吴易霖
李琳
苗向鹏
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SZ DJI Technology Co Ltd
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SZ DJI Technology Co Ltd
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Publication date
Application filed by SZ DJI Technology Co Ltd filed Critical SZ DJI Technology Co Ltd
Publication of WO2020087696A1 publication Critical patent/WO2020087696A1/zh
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    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/16—Constructional details or arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography

Definitions

  • Embodiments of the present invention relate to the field of drones, and in particular, to a microcomputer system and drones.
  • the microcomputer system is the "brain" of a high-performance drone. Cooperating with related software tool development kits can greatly improve the computing power of the drone, enabling the drone to interact with the environment in real time and complete complex tasks.
  • the microcomputer system is provided with multiple interfaces, which can be connected to various expansion devices such as sensors and display screens; the microcomputer system can also be connected to the drone through a custom interface to receive and process the real-time carried by the drone in real time.
  • the image information returned by the gimbal camera provides developers with richer application possibilities.
  • the microcomputer system needs to be equipped with more accessories, which brings the microcomputer system to take up too much space and seriously affects the installation of other components on the drone.
  • the purpose of the embodiments of the present invention is to provide a microcomputer system and an unmanned aerial vehicle.
  • the microcomputer system can be installed more conveniently and save space.
  • An embodiment of the present invention provides a microcomputer system, which includes a microcomputer and at least one accessory, and further includes a mounting rack, the accessory and the microcomputer are stacked along the extending direction of the mounting rack, and the microcomputer And the accessories are fixed with the mounting frame.
  • microcomputer system as described above, optionally, there are a plurality of accessories, and the microcomputer and the plurality of accessories are stacked in order along the extending direction of the mounting frame.
  • the accessory includes a multifunctional power module, and the multifunctional power module is stacked on the microcomputer along the extending direction of the mounting frame.
  • the accessory further includes a switch control module, and the switch control module is stacked on the microcomputer along the extending direction of the mounting frame.
  • the accessory further includes a hub, and the hub is stacked on the microcomputer along the extending direction of the mounting bracket.
  • the accessory further includes an antenna module, and the antenna module is stacked on the microcomputer along the extending direction of the mounting bracket.
  • At least two antenna modules are provided, and the two antenna modules are arranged at intervals.
  • the accessory further includes another microcomputer.
  • the mounting bracket includes at least two mounting rods arranged at intervals, and each of the mounting rods is fixed to the microcomputer and the accessory.
  • the mounting rod is provided with a plurality of fixing portions for fixing the accessory and the microcomputer, and a plurality of the fixing portions are along the extending direction of the mounting rod It is provided that the accessory and the microcomputer are fixed to the fixing part through fasteners.
  • a plurality of the fixing portions are arranged at equal intervals along the extending direction of the mounting rod.
  • the fixing portion is a screw hole opened on the mounting rod.
  • a gap is provided between at least two of the accessory stacked on the mounting frame and the microcomputer.
  • the microcomputer system is optionally provided with a power interface, a USB interface, an Ethernet interface, an OTG interface, a high-definition multimedia interface, an asynchronous transceiver interface, a controller area network interface, One or more of input / output interface and antenna interface.
  • Another embodiment of the present invention provides an unmanned aerial vehicle, including a base, on which a microcomputer system as described above is provided.
  • the microcomputer system and drone provided by the embodiments of the present invention integrate scattered accessories and microcomputers on the mounting frame.
  • the microcomputers and accessories are fixed to the mounting frame and are stacked along the extending direction of the mounting frame, thereby saving
  • the installation space allows the UAV under the same volume to adapt to more accessories and achieve more functions.
  • FIG. 1 is a schematic structural diagram of a microcomputer system provided by an embodiment of the present invention.
  • FIG. 2 is a schematic structural diagram of a microcomputer system provided by another embodiment of the present invention.
  • FIG. 3 is a schematic structural diagram of a microcomputer system provided by still another embodiment of the present invention.
  • the microcomputer system is provided with multiple interfaces, which can be connected to various expansion devices such as sensors and display screens; the microcomputer system can also be connected to the drone through a custom interface, and receive and process real-time
  • the image information returned by the gimbal camera provides developers with richer application possibilities.
  • the microcomputer system needs to be equipped with more accessories, which brings the microcomputer system to take up too much space. Due to the limited internal space of the drone, it is equipped with multiple accessories After installation, the microcomputer system seriously affected the installation of other components on the drone, causing inconvenience in installation.
  • FIG. 1 is a schematic diagram of a microcomputer system provided by an embodiment of the present invention
  • FIG. 2 is a schematic diagram of a microcomputer system provided by another embodiment of the present invention
  • FIG. 3 is a microcomputer provided by yet another embodiment of the present invention Schematic diagram of the system structure; please refer to Figure 1-3.
  • This embodiment provides a microcomputer system, which includes a microcomputer 100 and at least one accessory, and further includes a mounting rack 200.
  • the accessory and the microcomputer 100 are stacked along the extending direction of the mounting rack 200, and the microcomputer 100 and the accessories are both installed and installed.
  • the frame 200 is fixed.
  • the microcomputer system of this embodiment may be connected to drones and other devices through various interfaces to implement information interaction and provide users with a rich application experience.
  • One or more of the power interface, USB interface, Ethernet interface, OTG interface, high-definition multimedia interface, asynchronous transceiver interface, controller local area network interface, input / output interface, and antenna interface can be provided on the microcomputer Species.
  • the microcomputer system can connect various expansion devices such as sensors and display screens through various interfaces.
  • the microcomputer system can also be connected to the drone through a custom interface, and receive and process the image information of the mounted gimbal camera in real time, providing developers with rich application possibilities.
  • the USB interface may be a USB2.0 interface, a USB3.0 interface, etc., to access an external device supporting the corresponding USB.
  • the Ethernet interface can be connected to a network cable to connect to the Internet.
  • the OTG interface allows the microcomputer to be used as both a host and a device; specifically, when the microcomputer is used as a host, connect the OTG line to the microcomputer, and connect the USB device to the other end of the OTG line; When used as a device, the microcomputer is connected to another microcomputer using a USB cable. At this time, the other microcomputer is used as a host, and the microcomputer is used as a device to perform operations such as image backup or restore.
  • the OTG interface can also be regarded as a USB 3.0 interface.
  • a high-definition multimedia interface (such as HDMI) can be connected to the display screen to present the corresponding image in real time.
  • Asynchronous Transceiver Transmitter (UART) interface is a universal serial data bus interface used for asynchronous communication; the bus interface is bidirectional communication, which can achieve full-duplex transmission and reception.
  • the controller area network (CAN) interface is a standardized serial communication protocol interface that effectively supports distributed control or real-time control.
  • the input / output interface (I / O interface) can be connected to the switch control module 500 using an I / O connection line.
  • the interface of the microcomputer 100 is not limited to the above interface, and other suitable interfaces may also be provided.
  • This embodiment is merely an exemplary description and is not limited herein.
  • the microcomputer 100 in this embodiment may be a small computer and other devices.
  • the microcomputer 100 is the main computing and processing device of the microcomputer system. Cooperating with related software programs can greatly improve the computing power of the drone and realize the real-time interaction between the drone and the environment And complete complex tasks. There are a number of accessories, and the specific number can be configured as needed to achieve the needs of a variety of different functions.
  • the microcomputer and a plurality of accessories are stacked one after another along the extending direction of the mounting frame 200.
  • the accessory includes a multi-function power module 300, which is stacked on the microcomputer 100 along the extending direction of the mounting frame.
  • the multi-function power module 300 is connected to the input power and supplies power to the microcomputer 100 and its external devices.
  • the multi-function power module 300 includes a power input interface (power adapter input interface, a high-power power input interface) and a power output interface (low-power power output interface, a high-power power output interface), thereby providing two independent power sources for the microcomputer 100 Enter.
  • the accessory further includes a hub 400, which is stacked on the microcomputer 100 along the extending direction of the mounting bracket.
  • the hub 400 may be, for example, a USB3.0 hub, which is used to extend a USB interface to simultaneously connect multiple devices with a USB interface.
  • the accessory further includes a switch control module 500, which is stacked on the microcomputer 100 along the extending direction of the mounting frame.
  • the switch control module 500 is connected to the I / O interface of the microcomputer 100 and can control part of the operation of the microcomputer 100 by pressing keys.
  • the buttons on the switch control module 500 include a restart button, a power button, and a resume button.
  • Other suitable expansion interfaces such as SPI and 12C interfaces, can also be set, which are not limited herein.
  • the accessory further includes an antenna module 600, which is stacked on the microcomputer 100 along the extending direction of the mounting bracket.
  • the antenna module 600 may be, for example, a WiFi antenna module, and may be connected to the Internet through a WiFi antenna.
  • At least two antenna modules 600 are provided, and the two antenna modules 600 are spaced apart. Preferably, the two antenna modules 600 are arranged perpendicular to each other or toward the signal source.
  • the accessory may also include another microcomputer, and the two microcomputers are connected through an OTG interface to achieve more functions.
  • the multi-function power module 300, the hub 400, the switch control module 500, and the antenna module 600 in this embodiment do not have specific installation location restrictions, and can theoretically be combined with each other to install side by side or up and down along the extension direction of the mounting frame Installation, the specific arrangement can be selected according to actual needs.
  • the microcomputer 100 is provided at one end of the mounting frame 200.
  • the multi-function power module 300 and the switch control module 500 are both stacked on the microcomputer 100, and the multi-function power module 300 and the switch control module 500 are arranged on the same layer.
  • the hub 400 and the antenna module 600 are stacked on the multi-function power module 300 and the switch control module 500, and the hub 400 and the antenna module 600 are arranged on the same layer; specifically, the hub 400 is stacked on the multi-function power module 300, the antenna module The 600 stack is provided above the switch control module 500.
  • the multi-function power module 300 and the switch control module 500 are arranged on the same layer and located at one end of the mounting frame 200.
  • the microcomputer 100 is stacked above the multi-function power module 300 and the switch control module 500 along the extending direction of the mounting frame.
  • the hub 400 and the antenna module 600 are stacked on top of the microcomputer 100, and the hub 400 and the antenna module 600 are arranged in the same layer; specifically, the hub 400 corresponds to the multifunctional power module 300 in the extending direction of the mounting frame, and the antenna module 600 It corresponds to the switch control module 500 in the extending direction of the mounting frame.
  • the microcomputer 100 is disposed at one end of the mounting frame 200.
  • the hub 400 and the switch control module 500 are both stacked on the microcomputer 100 along the extending direction of the mounting frame, and the hub 400 and the switch control module 500 are arranged on the same layer.
  • the multi-function power module 300 and the antenna module 600 are stacked on the hub 400 and the switch control module 500, and the multi-function power module 300 and the antenna module 600 are set on the same layer; specifically, the multi-function power module 300 is stacked on the hub 400
  • the antenna module 600 is stacked above the switch control module 500.
  • the microcomputer system provided in this embodiment integrates scattered accessories and the microcomputer 100 on the mounting frame 200.
  • the microcomputer 100 and the accessories are fixed to the mounting frame 200 and are stacked along the extending direction of the mounting frame 200, thereby saving
  • the installation space allows the UAV under the same volume to adapt to more accessories and achieve more functions.
  • the mounting bracket 200 of this embodiment includes at least two mounting rods arranged at intervals, each mounting rod is fixed to the microcomputer 100 and the accessory, and the microcomputer 100 and the accessory can be firmly fixedly installed through a plurality of mounting rods, The arrangement of mounting rods can also be set as required.
  • At least two mounting rods are provided on the same side of the microcomputer 100, and when the length of the microcomputer 100 is longer on one side, the two mounting rods are used to fix the Both ends can ensure good fixing effect.
  • At least one mounting rod is provided on each of the opposite sides of the microcomputer 100, and installing the mounting rods on the opposite sides of the microcomputer 100 can make the mounting rod evenly bear the microcomputer The gravity of 100 avoids uneven stress.
  • the two opposite sides of the microcomputer 100 may be provided with two mounting rods, so as to have the advantages of the above two embodiments at the same time.
  • each side of the microcomputer 100 is provided with at least one mounting rod, so that the force of the mounting rod is more uniform.
  • the mounting rod is provided with a plurality of fixing portions for fixing the accessory and the microcomputer 100, and the plurality of fixing portions are provided along the extending direction of the mounting rod, and the accessory and the microcomputer 100 are fixed to the fixing portion by fasteners.
  • the fixing portion is a threaded hole opened on the mounting rod
  • the fastener is a fastening screw
  • the accessory and the microcomputer 100 are fixedly connected to the mounting frame 200 by means of screw connection.
  • the plurality of fixing portions may be arranged at equal intervals along the extending direction of the mounting rod, or the spacing between adjacent fixing portions may be set as needed, which is not further limited in this embodiment.
  • This embodiment provides a drone including a base, and the base is provided with the microcomputer system described in the first embodiment above.
  • the drone in this embodiment may be an unmanned aerial vehicle, unmanned vehicle, unmanned boat, robot, or the like.
  • the base of the UAV can be connected to the mounting rack of the microcomputer system through a connecting piece to achieve the installation and fixation of the microcomputer system.
  • the drone provided in this embodiment integrates scattered accessories and microcomputers of the microcomputer system on the mounting frame.
  • the microcomputers and accessories are fixed to the mounting frame, and are stacked along the extending direction of the mounting frame, thereby saving installation Space allows UAVs of the same size to fit more accessories and achieve more functions.
  • the microcomputer system in this embodiment may be the main computing and processing equipment of the drone, and the related software programs can greatly improve the computing power of the drone.
  • a variety of interfaces are provided to adapt to different external devices, flexibility And strong scalability.
  • the terms “installation”, “connected”, “connected”, “fixed” and other terms should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection , Or integrated; it can be directly connected or indirectly connected through an intermediary, it can be the connection between the two elements or the interaction between the two elements.
  • installation can be a fixed connection or a detachable connection , Or integrated; it can be directly connected or indirectly connected through an intermediary, it can be the connection between the two elements or the interaction between the two elements.
  • first and second are only used to describe different components conveniently, and cannot be understood as indicating or implying a sequence relationship, relative importance, or implicitly indicating the indication The number of technical features.
  • the features defined with “first” and “second” may include at least one of the features either explicitly or implicitly.

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  • Human Computer Interaction (AREA)
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Abstract

一种微型计算机系统及无人机，微型计算机系统包括微型计算机（100）和至少一个配件，还包括安装架（200），所述配件和所述微型计算机（100）沿着所述安装架（200）的延伸方向层叠设置，且所述微型计算机（100）以及所述配件均与所述安装架（200）固定。无人机上设有该微型计算机系统。通过将微型计算机系统散乱的配件和微型计算机（100）整合在安装架（200）上，微型计算机（100）以及配件均与安装架（200）固定，且沿着安装架（200）中的延伸方向层叠设置，从而节省了安装空间，使得相同体积下的无人机能够适配更多的配件，实现更多的功能。

Description

微型计算机系统及无人机 技术领域
本发明实施例涉及无人机领域，尤其涉及一种微型计算机系统及无人机。
背景技术
微型计算机系统是高性能无人机的“大脑”，配合相关软件工具开发包可以大幅提升无人机的计算能力，使无人机能够实时与环境互动并完成复杂的任务。
相关技术中，微型计算机系统设置有多种接口，可连接传感器、显示屏等多种扩展设备；微型计算机系统还能通过自定义接口与无人机连接，实时接收并处理无人机所搭载的云台相机回传的图像信息，为开发者提供更丰富的应用可能性。
但是，为了使微型计算机系统具有更多的功能，该微型计算机系统就需要搭配更多的配件，由此带来了微型计算机系统占用空间过大，严重影响了无人机上其他部件的安装。
发明内容
为了克服现有技术下的上述缺陷，本发明实施例的目的在于提供一种微型计算机系统及无人机，通过合理排布微型计算机和配件，使微型计算机系统安装更方便，更节省空间。
本发明一实施例提供一种微型计算机系统，包括微型计算机和至少一个配件，还包括安装架，所述配件和所述微型计算机沿着所述安装架的延伸方向层叠设置，且所述微型计算机以及所述配件均与所述安装架固定。
如上所述的微型计算机系统，可选的，所述配件为多个，所述微型计算机和多个所述配件沿着所述安装架的延伸方向依次层叠设置。
如上所述的微型计算机系统，可选的，所述配件包括多功能电源模块，所述多功能电源模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
如上所述的微型计算机系统，可选的，所述配件还包括开关控制模块，所述开关控制模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
如上所述的微型计算机系统，可选的，所述配件还包括集线器，所述集线器沿着所述安装架的延伸方向层叠在所述微型计算机上。
如上所述的微型计算机系统，可选的，所述配件还包括天线模块，所述天线模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
如上所述的微型计算机系统，可选的，所述天线模块至少设置有两个，并且两个所述天线模块间隔设置。
如上所述的微型计算机系统，可选的，所述配件还包括另一微型计算机。
如上所述的微型计算机系统，可选的，所述安装架包括至少两个间隔设置的安装杆，每个所述安装杆均与所述微型计算机和所述配件固定。
如上所述的微型计算机系统，可选的，所述安装杆上设有用于固定所述配件和所述微型计算机多个固定部，并且多个所述固定部沿着所述安装杆的延伸方向设置，所述配件和所述微型计算机通过紧固件与所述固定部固定。
如上所述的微型计算机系统，可选的，多个所述固定部沿着所述安装杆的延伸方向等间距设置。
如上所述的微型计算机系统，可选的，所述固定部为开设在所述安装杆上的螺纹孔。
如上所述的微型计算机系统，可选的，层叠在所述安装架上的所述配件和所述微型计算机中至少有两个之间设置有间隙。
如上所述的微型计算机系统，可选的，所述微型计算机上设有电源接口、USB接口、以太网接口、OTG接口、高清晰度多媒体接口、异步收发传输器接口、控制器局域网络接口、输入/输出接口、天线接口中的一种 或多种。
本发明另一实施例提供一种无人机，包括底座，所述底座上设有如上任一所述的微型计算机系统。
本发明实施例提供的微型计算机系统及无人机，将散乱的配件和微型计算机整合在安装架上，微型计算机以及配件均与安装架固定，且沿着安装架的延伸方向层叠设置，从而节省了安装空间，使得相同体积下的无人机能够适配更多的配件，实现更多的功能。
附图说明
为了更清楚地说明本发明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一简单地介绍，显而易见地，下面描述中的附图是本发明的一些实施例，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。
图1为本发明一实施方式提供的微型计算机系统的结构简图；
图2为本发明另一实施方式提供的微型计算机系统的结构简图；
图3为本发明再一实施方式提供的微型计算机系统的结构简图。
附图标记：
100-微型计算机；
200-安装架；
300-多功能电源模块；
400-集线器；
500-开关控制模块；
600-天线模块。
具体实施方式
相关技术中，微型计算机系统设置有多种接口，可连接传感器、显示屏等多种扩展设备；微型计算机系统还能通过自定义接口与无人机连接，实时接收并处理无人机所搭载的云台相机回传的图像信息，为开发者提供更丰富的应用可能性。
但是，为了使微型计算机系统具有更多的功能，该微型计算机系统就需要搭配更多的配件，由此带来了微型计算机系统占用空间过大，由于无人机内部空间有限，搭配多个配件的微型计算机系统在安装后严重影响了无人机上其他部件的安装，造成了安装的不便。
为使本发明的目的、技术方案和优点更加清楚，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作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。
实施例一
图1为本发明一实施方式提供的微型计算机系统的结构简图；图2为本发明另一实施方式提供的微型计算机系统的结构简图；图3为本发明再一实施方式提供的微型计算机系统的结构简图；请参照图1-图3。本实施例提供一种微型计算机系统，包括微型计算机100和至少一个配件，还包括安装架200，配件和微型计算机100沿着安装架200的延伸方向层叠设置，且微型计算机100以及配件均与安装架200固定。
具体的，本实施例的微型计算机系统可以通过多种接口连接无人机及其他设备，以实现信息的交互，为用户提供丰富的应用体验。微型计算机上可以设有电源接口、USB接口、以太网接口、OTG接口、高清晰度多媒体接口、异步收发传输器接口、控制器局域网络接口、输入/输出接口、天线接口中的一种或多种。微型计算机系统通过多种接口可连接传感器、显示屏等多种扩展设备。此外，微型计算机系统还能通过自定义接口与无人机连接，实时接收并处理所搭载云台相机的图像信息，为开发者提供丰富的应用可能。
其中，USB接口可以为USB2.0接口、USB3.0接口等，以接入支持相应 USB的外部设备。以太网接口可以接入网线以连接至互联网。OTG接口允许微型计算机既可以作为主机(host)进行使用，又可以作为设备(device)进行使用；具体地，微型计算机作为主机使用时，连接OTG线至此微型计算机，OTG线另一端连接USB设备；作为设备使用时，使用USB线将该微型计算机连接至另一微型计算机，此时另一微型计算机作为主机，该微型计算机作为设备，可进行例如镜像备份或还原等操作。此外，在另一种可能的实施例中，OTG接口也可视为USB 3.0接口，此时仅允许将该微型计算机作为主机使用。高清晰度多媒体接口(例如HDMI)可以与显示屏相连接，以实时呈现相应图像。异步收发传输器(UART)接口是一种通用串行数据总线接口，用于异步通信；该总线接口双向通信，可以实现全双工传输和接收。控制器局域网络(CAN)接口是一种标准化的串行通信协议接口，有效支持分布式控制或实时控制。输入/输出接口(I/O接口)可以使用I/O连接线连接至开关控制模块500。
可以理解，微型计算机100的接口不限于上述接口，也可以设置其他合适的接口，本实施例仅为示例性说明，在此不作限定。
本实施例中的微型计算机100可以为小型计算机等设备，微型计算机100是微型计算机系统的主要运算处理设备，配合相关软件程序可以大幅提升无人机的计算能力，实现无人机实时与环境互动并完成复杂的任务。配件为多个，具体数量可以根据需要进行配置，以实现多种不同功能的需要，微型计算机和多个配件沿着安装架200的延伸方向依次层叠设置。
可选的，配件包括多功能电源模块300，多功能电源模块沿着安装架的延伸方向层叠在微型计算机100上。多功能电源模块300连接输入电源，为微型计算机100及其外接设备供电。多功能电源模块300包括功率输入接口(电源适配器输入接口、大功率电源输入接口)和功率输出接口(低功率电源输出接口、大功率电源输出接口)，从而为微型计算机100提供两路独立的电源输入。
可选的，配件还包括集线器400，集线器沿着安装架的延伸方向层叠在微型计算机100上。集线器400例如可以为USB3.0集线器，用于扩展USB接口，以同时连接多个具有USB接口的设备。
可选的，配件还包括开关控制模块500，开关控制模块沿着安装架的延伸方向层叠在微型计算机100上。开关控制模块500连接至微型计算机100的I/O接口，可通过按键控制微型计算机100的部分操作。开关控制模块500上的按键包括重启按键、电源按键、恢复按键等，也可以设置其他合适的扩展接口，如SPI和12C等接口，在此不作限定。
可选的，配件还包括天线模块600，天线模块沿着安装架的延伸方向层叠在微型计算机100上。天线模块600例如可以是WiFi天线模块，可以通过WiFi天线连接至互联网。
天线模块600至少设置有两个，并且两个天线模块600间隔设置。优选地，两个天线模块600相互垂直或朝向信号源设置。
可选的，配件还可以包括另一微型计算机，两个微型计算机之间通过OTG接口实现连接，以便实现更多功能。
需要说明的是本实施例中的多功能电源模块300、集线器400、开关控制模块500以及天线模块600均没有具体的安装位置的限制，理论上可以互相组合并排安装或者沿安装架的延伸方向上下安装，具体的排列方式可以根据实际的需要进行选择。
例如，在一个可选的实施方式中，如图1所示，微型计算机100设置在安装架200的一端。沿着安装架的延伸方向多功能电源模块300和开关控制模块500均层叠设置在微型计算机100上，且多功能电源模块300和开关控制模块500同层设置。集线器400和天线模块600层叠设置在多功能电源模块300和开关控制模块500上，且集线器400和天线模块600同层设置；具体的，集线器400层叠设置在多功能电源模块300的上方，天线模块600层叠设置在开关控制模块500的上方。
又如，在另一个可选的实施方式中，如图2所示，多功能电源模块300和开关控制模块500同层设置，且位于安装架200的一端。沿着安装架的延伸方向微型计算机100层叠设置在多功能电源模块300和开关控制模块500的上方。集线器400和天线模块600层叠设置在微型计算机100的上方，且集线器400和天线模块600同层设置；具体的，集线器400与多功能电源模块300在安装架的延伸方向上相对应，天线模块600与开关控制模块500在 安装架的延伸方向上相对应。
再如，在再一个可选的实施方式中，如图3所示，微型计算机100设置在安装架200的一端。沿着安装架的延伸方向集线器400和开关控制模块500均层叠设置在微型计算机100上，且集线器400和开关控制模块500同层设置。多功能电源模块300和天线模块600层叠设置在集线器400和开关控制模块500上，且多功能电源模块300和天线模块600同层设置；具体的，多功能电源模块300层叠设置在集线器400的上方，天线模块600层叠设置在开关控制模块500的上方。
本实施例提供的微型计算机系统，将散乱的配件和微型计算机100整合在安装架200上，微型计算机100以及配件均与安装架200固定，且沿着安装架200的延伸方向层叠设置，从而节省了安装空间，使得相同体积下的无人机能够适配更多的配件，实现更多的功能。
进一步地，本实施例的安装架200包括至少两个间隔设置的安装杆，每个安装杆均与微型计算机100和配件固定，通过多个安装杆可以将微型计算机100和配件牢固的固定安装，安装杆的排列方式也可以根据需要进行设置。
例如，在一个可选的实施方式中，至少有两个安装杆设置在微型计算机100的同一侧，当微型计算机100在一侧的长度较长时利用两个安装杆分别固定住微型计算机100的两端，可以保证良好的固定效果。
又如，在另一个可选的实施方式中，微型计算机100相对的两侧至少各设置有一个安装杆，将安装杆分别设置在微型计算机100的相对两侧可以使安装杆均匀的承受微型计算机100的重力，避免受力不均。
进一步地，微型计算机100相对的两侧可以各设置有两个安装杆，以同时具备上述两种实施方式的优点。
或者，微型计算机100的每一侧均至少各设置有一个安装杆，以使安装杆的受力更加均匀。
进一步地，安装杆上设有用于固定配件和微型计算机100的多个固定部，并且多个固定部沿着安装杆的延伸方向设置，配件和微型计算机100通过紧固件与固定部固定。
具体的，固定部为开设在安装杆上的螺纹孔，紧固件为紧固螺钉，通过螺钉连接的方式将配件和微型计算机100固定连接在安装架200上。多个固定部可以沿着安装杆的延伸方向等间距设置，或者相邻的固定部之间的间距可以根据需要进行设置，本实施例对此不做进一步限定。
进一步地，为保证相邻配件之间的散热，层叠在安装架上的配件和微型计算机100中至少有两个之间具有间隙，相邻配件之间的间隙大小也可以根据需要进行设置。
实施例二
本实施例提供一种无人机，包括底座，底座上设有如上实施例一所述的微型计算机系统。
具体的，本实施例中的无人机可以是无人飞行器、无人车、无人船、机器人等。无人机的底座可以通过连接件与微型计算机系统的安装架连接，以实现对微型计算机系统的安装固定。
本实施例提供的无人机，将微型计算机系统散乱的配件和微型计算机整合在安装架上，微型计算机以及配件均与安装架固定，且沿着安装架的延伸方向层叠设置，从而节省了安装空间，使得相同体积下的无人机能够适配更多的配件，实现更多的功能。
本实施例中的微型计算机系统可以是无人机的主要运算处理设备，配合相关软件程序可以大幅提升无人机的计算能力，同时设置有多种接口，可以适配不同的外部设备，灵活性和扩展性强。
在本发明实施例的描述中，需要理解的是，术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”、“顺时针”、“逆时针”、“轴向”、“径向”、“周向”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本发明和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定 的方位构造和操作，因此不能理解为对本发明的限制。
在本发明中，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或成一体；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言，可以根据具体情况理解上述术语在本发明中的具体含义。
需要说明的是，在本发明的描述中，术语“第一”、“第二”仅用于方便描述不同的部件，而不能理解为指示或暗示顺序关系、相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个该特征。
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。

Claims (28)

  1. 一种微型计算机系统，包括微型计算机和至少一个配件，其特征在于，还包括安装架，所述配件和所述微型计算机沿着所述安装架的延伸方向层叠设置，且所述微型计算机以及所述配件均与所述安装架固定。
  2. 根据权利要求1所述的微型计算机系统，其特征在于，所述配件为多个，所述微型计算机和多个所述配件沿着所述安装架的延伸方向依次层叠设置。
  3. 根据权利要求2所述的微型计算机系统，其特征在于，所述配件包括多功能电源模块，所述多功能电源模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  4. 根据权利要求2所述的微型计算机系统，其特征在于，所述配件还包括开关控制模块，所述开关控制模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  5. 根据权利要求2所述的微型计算机系统，其特征在于，所述配件还包括集线器，所述集线器沿着所述安装架的延伸方向层叠在所述微型计算机上。
  6. 根据权利要求2所述的微型计算机系统，其特征在于，所述配件还包括天线模块，所述天线模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  7. 根据权利要求6所述的微型计算机系统，其特征在于，所述天线模块至少设置有两个，并且两个所述天线模块间隔设置。
  8. 根据权利要求2所述的微型计算机系统，其特征在于，所述配件还包括另一微型计算机。
  9. 根据权利要求1-8中任一所述的微型计算机系统，其特征在于，所述安装架包括至少两个间隔设置的安装杆，每个所述安装杆均与所述微型计算机和所述配件固定。
  10. 根据权利要求9所述的微型计算机系统，其特征在于，所述安装杆上设有用于固定所述配件和所述微型计算机多个固定部，并且多个所述 固定部沿着所述安装杆的延伸方向设置，所述配件和所述微型计算机通过紧固件与所述固定部固定。
  11. 根据权利要求10所述的微型计算机系统，其特征在于，多个所述固定部沿着所述安装杆的延伸方向等间距设置。
  12. 根据权利要求10所述的微型计算机系统，其特征在于，所述固定部为开设在所述安装杆上的螺纹孔。
  13. 根据权利要求1-8中任一项所述的微型计算机系统，其特征在于，层叠在所述安装架上的所述配件和所述微型计算机中至少有两个之间设置有间隙。
  14. 根据权利要求1-8中任一所述的微型计算机系统，其特征在于，所述微型计算机上设有电源接口、USB接口、以太网接口、OTG接口、高清晰度多媒体接口、异步收发传输器接口、控制器局域网络接口、输入/输出接口、天线接口中的一种或多种。
  15. 一种无人机，包括底座，其特征在于，所述底座上设有微型计算机系统，所述微型计算机系统包括微型计算机和至少一个配件，还包括安装架，所述配件和所述微型计算机沿着所述安装架的延伸方向层叠设置，且所述微型计算机以及所述配件均与所述安装架固定。
  16. 根据权利要求15所述的无人机，其特征在于，所述配件为多个，所述微型计算机和多个所述配件沿着所述安装架的延伸方向依次层叠设置。
  17. 根据权利要求16所述的无人机，其特征在于，所述配件包括多功能电源模块，所述多功能电源模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  18. 根据权利要求16所述的无人机，其特征在于，所述配件还包括开关控制模块，所述开关控制模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  19. 根据权利要求16所述的无人机，其特征在于，所述配件还包括集线器，所述集线器沿着所述安装架的延伸方向层叠在所述微型计算机上。
  20. 根据权利要求16所述的无人机，其特征在于，所述配件还包括天线模块，所述天线模块沿着所述安装架的延伸方向层叠在所述微型计算机上。
  21. 根据权利要求20所述的无人机，其特征在于，所述天线模块至少设置有两个，并且两个所述天线模块间隔设置。
  22. 根据权利要求16所述的无人机，其特征在于，所述配件还包括另一微型计算机。
  23. 根据权利要求15-22中任一所述的无人机，其特征在于，所述安装架包括至少两个间隔设置的安装杆，每个所述安装杆均与所述微型计算机和所述配件固定。
  24. 根据权利要求23所述的无人机，其特征在于，所述安装杆上设有用于固定所述配件和所述微型计算机多个固定部，并且多个所述固定部沿着所述安装杆的延伸方向设置，所述配件和所述微型计算机通过紧固件与所述固定部固定。
  25. 根据权利要求24所述的无人机，其特征在于，多个所述固定部沿着所述安装杆的延伸方向等间距设置。
  26. 根据权利要求24所述的无人机，其特征在于，所述固定部为开设在所述安装杆上的螺纹孔。
  27. 根据权利要求15-22中任一项所述的无人机，其特征在于，层叠在所述安装架上的所述配件和所述微型计算机中至少有两个之间设置有间隙。
  28. 根据权利要求15-22中任一所述的无人机，其特征在于，所述微型计算机上设有电源接口、USB接口、以太网接口、OTG接口、高清晰度多媒体接口、异步收发传输器接口、控制器局域网络接口、输入/输出接口、天线接口中的一种或多种。
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CN105676859A (zh) * 2016-03-14 2016-06-15 北京航空航天大学 无人机三自由度空中自主加油装置及其实施方法
CN206757136U (zh) * 2017-05-27 2017-12-15 长春嘉信通信信息技术有限公司 一种便于安装的综合配线柜
CN207764704U (zh) * 2017-12-20 2018-08-24 杭州昊舜视讯科技有限公司 一种无人机机载微计算机系统

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US9019375B1 (en) * 2012-07-10 2015-04-28 The Boeing Company Target locator and interceptor imaging and sensing assembly, system and method
CN105676859A (zh) * 2016-03-14 2016-06-15 北京航空航天大学 无人机三自由度空中自主加油装置及其实施方法
CN206757136U (zh) * 2017-05-27 2017-12-15 长春嘉信通信信息技术有限公司 一种便于安装的综合配线柜
CN207764704U (zh) * 2017-12-20 2018-08-24 杭州昊舜视讯科技有限公司 一种无人机机载微计算机系统

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