WO2024041370A1 - 一种飞行器状态指示方法、飞行器及存储介质 - Google Patents

一种飞行器状态指示方法、飞行器及存储介质 Download PDF

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Publication number
WO2024041370A1
WO2024041370A1 PCT/CN2023/111663 CN2023111663W WO2024041370A1 WO 2024041370 A1 WO2024041370 A1 WO 2024041370A1 CN 2023111663 W CN2023111663 W CN 2023111663W WO 2024041370 A1 WO2024041370 A1 WO 2024041370A1
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Prior art keywords
aircraft
formation
status
indication method
working
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PCT/CN2023/111663
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English (en)
French (fr)
Inventor
胡华智
王栋
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亿航智能设备（广州）有限公司
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Publication of WO2024041370A1 publication Critical patent/WO2024041370A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/006—Indicating maintenance
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/008—Registering or indicating the working of vehicles communicating information to a remotely located station
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration

Definitions

  • the invention relates to the technical field of aircraft, and in particular to an aircraft status indication method, an aircraft and a storage medium.
  • the purpose of embodiments of the present invention is to provide an aircraft status indication method, aircraft and storage medium to solve the current technical problem of being unable to quickly obtain the real-time status of one or some aircraft in an aircraft formation cluster.
  • a method for indicating aircraft status includes:
  • abnormal state information is reported to the ground station.
  • the abnormal state information includes positioning information used to indicate its position in the formation and the abnormal state.
  • the preset conditions include arrival of its own working status detection timing time and/or receipt of a working status detection instruction sent by the ground station.
  • detecting its own working status includes: detecting whether at least one of its own positioning device, battery, sensor, indicator light, performance light, and motor is working normally.
  • the positioning information used to indicate one's position in the formation includes one's position code in the formation.
  • the method before detecting its own working status when the preset conditions are met, the method further includes:
  • Preset positioning information used to indicate your position in the formation.
  • the presetting the positioning information used to indicate the position of the aircraft in the formation includes presetting the position code of the aircraft in the formation or the correspondence table between the aircraft serial number and its position code in the formation.
  • the positioning information used to indicate its position in the formation includes its own aircraft serial number, so that the ground station can determine its position code in the formation based on the aircraft serial number.
  • the method further includes:
  • an aircraft includes a memory, a processor, and a computer program stored on the memory and executable on the processor.
  • the computer program is processed by the The steps to implement the above aircraft status indication method when the aircraft is executed.
  • a computer-readable storage medium is provided.
  • An aircraft status indication program is stored on the computer-readable storage medium.
  • the aircraft status indication program is executed by a processor, the above-mentioned aircraft status indication method is implemented. A step of.
  • the preset conditions when the preset conditions are met, its own working status is detected; if the working status is an abnormal status, abnormal status information is reported to the ground station.
  • the abnormal status information includes positioning information used to indicate its position in the formation and the abnormal status.
  • the staff at the ground station can quickly determine the position of the faulty aircraft in the formation based on the positioning information indicating the position of the aircraft in the formation, thereby quickly finding the faulty aircraft and completing the repair or replacement of the faulty aircraft, which improves the safety of the ground station staff. Work efficiency.
  • Figure 1 is a flow chart of an aircraft status indication method provided by an embodiment of the present invention.
  • Figure 2 is a flow chart of another aircraft status indication method provided by an embodiment of the present invention.
  • Figure 3 is a flow chart of yet another aircraft status indication method provided by an embodiment of the present invention.
  • Figure 4 is a schematic structural diagram of an aircraft provided by an embodiment of the present invention.
  • Figure 1 is a flow chart of an aircraft status indication method provided by an embodiment of the present invention.
  • the method in this embodiment is automatically run by the aircraft in the formation cluster. When running, each step can be performed one after another in the order as shown in the flow chart, or multiple steps can be performed simultaneously according to the actual situation, which are not mentioned here. No restrictions.
  • the aircraft status indication method provided by the present invention includes:
  • Step S100 When the preset conditions are met, detect its own working status.
  • Step S200 If the working state is an abnormal state, abnormal state information is reported to the ground station.
  • the abnormal state information includes positioning information used to indicate its position in the formation and the abnormal state.
  • the abnormal status information includes instructions for Positioning information of the position in the formation and the abnormal status. Since the aircraft automatically reports abnormal status information to the ground station when it detects an abnormality in its own working status.
  • the abnormal status information includes positioning information used to indicate its position in the formation, so the staff at the ground station can use the positioning information to Quickly determine the position of the faulty aircraft in the formation, thereby quickly finding the faulty aircraft and completing the repair or replacement of the faulty aircraft, which improves the work efficiency of ground station staff.
  • the preset conditions when the preset conditions are met, its own working status is detected; if the working status is an abnormal status, abnormal status information is reported to the ground station.
  • the abnormal status information This includes positioning information used to indicate its position in the formation and the abnormal status.
  • the aircraft detects that its own working status is abnormal it automatically reports abnormal status information to the ground station.
  • the abnormal status information includes positioning information used to indicate its position in the formation, so that the staff at the ground station can instruct the aircraft to
  • the positioning information of the position in the formation can quickly determine the position of the faulty aircraft in the formation, thereby quickly finding the faulty aircraft and completing the repair or replacement of the faulty aircraft, which improves the work efficiency of the ground station staff.
  • step S100 when the preset conditions are met, its own working status is detected.
  • the preset conditions include the arrival of its own working status detection timing time and/or the receipt of the working status detection instruction sent by the ground station, that is, setting the working status detection cycle in the aircraft, and detecting itself every time the working status detection timing time arrives. or, when you need to know the working status of the aircraft, send a working status detection command to the aircraft through the ground station, and the aircraft detects its own working status when receiving the working status detection command sent by the ground station.
  • the preset conditions can also be set to enable the aircraft to detect its own working status. This embodiment does not limit the specific type of preset conditions.
  • detecting its own working status includes: detecting whether at least one of its own positioning device, battery, sensor, indicator light, performance light, and motor is working normally.
  • the aircraft detects whether at least one of its positioning device, battery, sensor, indicator light, performance light, and motor is working normally through the flight control system to discover its own abnormal status and report it to the ground station to facilitate the work of the ground station. Personnel handles discovered abnormal conditions.
  • step S200 if the working state is an abnormal state, abnormal state information is reported to the ground station.
  • the abnormal state information includes positioning information used to indicate its position in the formation and the abnormal state.
  • the abnormal status information includes positioning information used to indicate its position in the formation and the abnormality. state.
  • the positioning information used to indicate its position in the formation can enable the ground station staff to know the abnormal status of the aircraft and at the same time determine the specific position of the aircraft in the abnormal status in the formation, thereby quickly finding the abnormal status. aircraft, and repair or replace them to ensure the normal performance of the aircraft formation cluster mission.
  • the positioning information used to indicate one's position in the formation includes one's position code in the formation.
  • the aircraft reports its position code in the formation, allowing ground station staff to quickly and accurately locate the faulty aircraft, thus saving time in finding the faulty aircraft.
  • the position code is 12/20, which means that the 20th aircraft in row 12 has a malfunction.
  • the positioning information used to indicate its position in the formation includes its own aircraft serial number, so that the ground station can determine its position code in the formation based on the aircraft serial number.
  • the correspondence table between the aircraft serial number and its position code in the formation can also be preset at the ground station.
  • the aircraft serial number of the failed aircraft is sent to the ground station, and the ground station The station can obtain the position code of the failed aircraft in the formation by querying the correspondence table between the preset aircraft serial number and its position code in the formation, thereby quickly locating the failed aircraft.
  • Figure 2 is a flow chart of another aircraft status indication method provided by an embodiment of the present invention. Before detecting its own working status when the preset conditions are met, the method also includes:
  • Step S300 Preset positioning information indicating its position in the formation.
  • the positioning information indicating the position of the aircraft in the formation is preset in the aircraft in the formation.
  • the position code of the aircraft in the formation is preset in the aircraft in the formation.
  • presetting the positioning information used to indicate the position of the aircraft in the formation includes presetting a position code of the aircraft in the formation or a correspondence table between the aircraft serial number and its position code in the formation.
  • the aircraft in the formation are preset with its own position code in the formation or the correspondence table between the aircraft serial number and its position code in the formation.
  • the aircraft serial number and its position code in the formation are preset in the aircraft,
  • the aircraft detects that its working status is abnormal it will obtain its position code in the formation by looking up the correspondence table between the aircraft serial number and its position code in the formation based on its own aircraft serial number.
  • FIG. 3 is a flow chart of yet another aircraft status indication method provided by an embodiment of the present invention.
  • the step S200 includes:
  • Step S210 if the working state is an abnormal state, report the abnormal state information to the ground station and trigger the status indicator light corresponding to the abnormal state.
  • the abnormal state information includes an indicator light used to indicate its position in the formation. Positioning information and the abnormal status.
  • an aircraft in the formation detects that its working status is abnormal, it reports abnormal status information to the ground station and triggers a status indicator light corresponding to the abnormal status.
  • This status indicator light can help the ground station The station staff can find the malfunctioning aircraft more quickly, thereby further improving the work efficiency of the ground station staff.
  • aircraft in a formation cluster usually have several indicator lights, including but not limited to head lights, arm lights, and performance lights loaded on the fuselage for light shows.
  • Each indicator light and performance light can There are bright and dark and various color changes. Through the on and off and color changes of the indicator lights and performance lights, as well as their combinations, tens of thousands of light status combinations can be formed, from which the most recognizable combinations can be selected to display the corresponding status of the aircraft.
  • the implementation logic is as follows: the flight control system of the aircraft determines the working status of the aircraft. If the working status is an abnormal status, it controls a combination of one or more lights to correspond to the abnormal working status.
  • the abnormal working status includes but is not limited to: aircraft positioning failure, aircraft battery abnormality, aircraft sensor abnormality, etc.
  • the relevant working status is displayed through the corresponding lights.
  • the staff can quickly The indicator light status screens out aircraft with abnormal status and takes corresponding measures to improve work efficiency.
  • the preset conditions when the preset conditions are met, its own working status is detected; if the working status is an abnormal status, abnormal status information is reported to the ground station, and the abnormal status information includes instructions for indicating that it is in the formation.
  • the staff at the ground station can quickly determine the position of the faulty aircraft in the formation based on the positioning information indicating the position of the aircraft in the formation, thereby quickly finding the faulty aircraft and completing the repair or replacement of the faulty aircraft, which improves the safety of the ground station staff. Work efficiency.
  • An embodiment of the present invention also provides an aircraft 400.
  • the aircraft includes a memory 401, a processor 402, and a computer program stored on the memory and executable on the processor (not shown in the figure). ), when the computer program is executed by the processor 402, the steps of the aircraft status indicating method described in the first embodiment are implemented.
  • the aircraft in the embodiment of the present invention has the same concept as the aircraft status indication method in the above-mentioned Embodiment 1. Please refer to the corresponding method embodiment for details of its specific implementation process, and the technical features in the method embodiment are all applicable to this aircraft embodiment. I won’t go into details here.
  • An embodiment of the present invention also provides a computer-readable storage medium.
  • the computer-readable storage medium stores an aircraft status indication program.
  • the aircraft status indication program is executed by the processor, the aircraft as described in the first embodiment is implemented. The steps of the status indication method.
  • the computer-readable storage medium of the embodiment of the present invention belongs to the same concept as the method of the above-mentioned Embodiment 1.
  • the specific implementation process is detailed in the corresponding method embodiment, and the technical features in the method embodiment are described in the computer-readable storage medium embodiment. Both are applicable and will not be repeated here.
  • the methods of the above embodiments can be implemented by means of software plus the necessary general hardware platform. Of course, it can also be implemented by hardware, but in many cases the former is better. implementation. Based on this understanding, the technical solution of the present invention can be embodied in the form of a software product in essence or that contributes to the existing technology.
  • the computer software product is stored in a storage medium (such as ROM/RAM, disk, (optical disk), including a number of instructions for causing an aircraft to execute the methods described in various embodiments of the present invention.
  • the preset conditions when the preset conditions are met, its own working status is detected; if the working status is an abnormal status, abnormal status information is reported to the ground station.
  • the abnormal status information includes positioning information used to indicate its position in the formation and the abnormal status.
  • the staff at the ground station can quickly determine the position of the faulty aircraft in the formation based on the positioning information indicating the position of the aircraft in the formation, thereby quickly finding the faulty aircraft and completing the repair or replacement of the faulty aircraft, which improves the safety of the ground station staff. Work efficiency. Therefore, it has industrial practicality.

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  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
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Abstract

本发明公开了一种飞行器状态指示方法、飞行器及存储介质，属于飞行器技术领域，其中，该飞行器状态指示方法包括：当满足预设条件时，检测自身的工作状态（S100）；若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态（S200）。地面站的工作人员能够根据指示飞行器在编队中的位置的定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。

Description

一种飞行器状态指示方法、飞行器及存储介质 技术领域
本发明涉及飞行器技术领域，具体涉及一种飞行器状态指示方法、飞行器及存储介质。
 背景技术
目前，无人机等飞行器编队集群的规模越来越大，通常是几百架甚至上千架飞行器。如此众多的飞行器在准备工作以及飞行时，想要快速的得知其中的某一台或某一些飞行器的实时状态就变得非常困难，传统方法是逐一的去确认，需要花费较多的人力和时间。
 技术问题
有鉴于此，本发明实施例的目的在于提供一种飞行器状态指示方法、飞行器及存储介质，以解决目前无法快速得知飞行器编队集群中的某一台或某一些飞行器的实时状态的技术问题。
 技术解决方案
本发明解决上述技术问题所采用的技术方案如下：
根据本发明实施例的一个方面，提供一种飞行器状态指示方法，该方法包括：
当满足预设条件时，检测自身的工作状态；
若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。
可选地，所述预设条件包括自身的工作状态检测定时时间到达和/或接收到地面站发送的工作状态检测指令。
可选地，所述检测自身的工作状态包括：检测自身的定位装置、电池、传感器、指示灯、表演灯、电机的至少一种是否正常工作。
可选地，所述用于指示自身在编队中的位置的定位信息包括自身在编队中的位置编码。
可选地，在当满足预设条件时，检测自身的工作状态之前，所述方法还包括：
预置用于指示自身在编队中的位置的定位信息。
可选地，所述预置用于指示自身在编队中的位置的定位信息包括：预置自身在编队中的位置编码或者飞行器序列号与其在编队中的位置编码对应表。
可选地，所述用于指示自身在编队中的位置的定位信息包括自身的飞行器序列号，以便地面站根据所述飞行器序列号确定其在编队中的位置编码。
可选地，在向地面站上报异常状态信息之后，所述方法还包括：
触发与所述异常状态对应的状态指示灯。
根据本发明实施例的另一个方面，提供一种飞行器，该飞行器包括存储器、处理器及存储在所述存储器上并可在所述处理器上运行的计算机程序，所述计算机程序被所述处理器执行时实现上述飞行器状态指示方法的步骤。
根据本发明实施例的又一个方面，提供一种计算机可读存储介质，该计算机可读存储介质上存储有飞行器状态指示程序，所述飞行器状态指示程序被处理器执行时实现上述飞行器状态指示方法的步骤。
 有益效果
本发明实施例提供的飞行器状态指示方法、飞行器及存储介质中，当满足预设条件时，检测自身的工作状态；若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。地面站的工作人员能够根据指示飞行器在编队中的位置的定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。
 附图说明
下面将结合附图及实施例对本发明作进一步说明，附图中：
图1是本发明实施例提供的一种飞行器状态指示方法的流程图。
图2是本发明实施例提供的另一种飞行器状态指示方法的流程图。
图3是本发明实施例提供的又一种飞行器状态指示方法的流程图。
图4是本发明实施例提供的一种飞行器结构示意图。
 本发明的实施方式
应当理解，此处所描述的具体实施例仅用以解释本发明，并不用于限定本发明。
实施例一
图1是本发明实施例提供的一种飞行器状态指示方法的流程图。该实施例的方法通过处于编队集群中的飞行器自动运行，其中，各个步骤在运行的时候可以是按照如流程图中的顺序先后进行，也可以是根据实际情况多个步骤同时进行，在此并不做限定。本发明提供的飞行器状态指示方法包括：
步骤S100，当满足预设条件时，检测自身的工作状态。
步骤S200，若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。
通过上述实施方式，首先，当满足预设条件时，检测自身的工作状态；然后，若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。由于飞行器在检测到自身工作状态异常时，自动向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息，所以地面站的工作人员能够根据该定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。
在本实施例中，首先需要说明的是，考虑到现有技术中，无法快速得知飞行器编队集群中的某一台或某一些飞行器的实时状态的技术问题。因此，为了解决上述技术问题，在本实施例中，当满足预设条件时，检测自身的工作状态；若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。由于飞行器在检测到自身工作状态异常时，自动向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息，使得地面站的工作人员能够根据指示飞行器在编队中的位置的定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。
下面将结合具体实施方式对上述步骤进行具体的描述。
在步骤S100中，当满足预设条件时，检测自身的工作状态。
具体的，编队集群中的飞行器在满足预设条件时，通过飞控系统检测自身的工作状态，以便在自身工作状态异常时及时进行维修或更换，保证整个编队工作任务的正常完成。其中，预设条件包括自身的工作状态检测定时时间到达和/或接收到地面站发送的工作状态检测指令，也即在飞行器中设置工作状态检测周期，每次工作状态检测定时时间到达时检测自身的工作状态，或者，在需要了解飞行器的工作状态时，通过地面站给飞行器发送工作状态检测指令，飞行器在接收到地面站发送的工作状态检测指令时检测自身的工作状态。本领域技术人员可以理解的，还可以设置其他使飞行器检测自身的工作状态的预设条件，本实施例对具体的预设条件类型不作限定。
可选地，所述检测自身的工作状态包括：检测自身的定位装置、电池、传感器、指示灯、表演灯、电机的至少一种是否正常工作。
具体的，飞行器通过飞控系统检测自身的定位装置、电池、传感器、指示灯、表演灯、电机的至少一种是否正常工作，以发现自身的异常状态并上报给地面站，方便地面站的工作人员对发现的异常状态进行处理。
在步骤S200中，若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。
具体的，编队集群中的飞行器在检测到自身的工作状态为异常状态时，向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。其中，用于指示自身在编队中的位置的定位信息可以使地面站的工作人员在得知飞行器的异常状态的同时确定处于异常状态的飞行器在编队中的具体位置，从而迅速的找到处于异常状态的飞行器，并对其进行修理或更换，以保证飞行器编队集群工作任务的正常进行。
可选地，所述用于指示自身在编队中的位置的定位信息包括自身在编队中的位置编码。
具体的，飞行器通过上报自身在编队中的位置编码，使得地面站工作人员能够快速准确的定位到故障飞行器，从而节省了查找故障飞行器的时间。例如，位置编码为12/20，表示第12排的第20个飞行器出现故障。
可选地，所述用于指示自身在编队中的位置的定位信息包括自身的飞行器序列号，以便地面站根据所述飞行器序列号确定其在编队中的位置编码。
具体的，也可以在地面站预置飞行器序列号与其在编队中的位置编码的对应表，如此，在编队中的飞行器出现故障时，将出现故障的飞行器的飞行器序列号发送给地面站，地面站就可以通过查询预置的飞行器序列号与其在编队中的位置编码的对应表得到出现故障的飞行器在编队中的位置编码，从而迅速定位到出现故障的飞行器。
在一种实施方式中，请参考图2，图2是本发明实施例提供的另一种飞行器状态指示方法的流程图，在当满足预设条件时，检测自身的工作状态之前，所述方法还包括：
步骤S300，预置用于指示自身在编队中的位置的定位信息。
本实施方式中，将指示自身在编队中的位置的定位信息预置在编队中的飞行器中，例如，将飞行器自身在编队中的位置编码预置在编队中的飞行器中，如此，在飞行器检测到自身工作状态为异常状态时，即可读取该预置的自身在编队中的位置编码，将其与所述异常状态共同作为异常状态信息上报给地面站。
在一种实施方式中，所述预置用于指示自身在编队中的位置的定位信息包括：预置自身在编队中的位置编码或者飞行器序列号与其在编队中的位置编码对应表。
本实施方式中，在编队中的飞行器中预置自身在编队中的位置编码或者飞行器序列号与其在编队中的位置编码对应表，当在飞行器中预置飞行器序列号与其在编队中的位置编码对应表时，若飞行器检测到自身的工作状态为异常状态，则根据自身的飞行器序列号，通过查找飞行器序列号与其在编队中的位置编码对应表得到自身在编队中的位置编码。
在一种实施方式中，请参考图3，图3是本发明实施例提供的又一种飞行器状态指示方法的流程图，所述步骤S200包括：
步骤S210，若所述工作状态为异常状态，则向地面站上报异常状态信息，并触发与所述异常状态对应的状态指示灯，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。
本实施方式中，编队中的飞行器在检测到自身的工作状态为异常状态时，则向地面站上报异常状态信息，并且触发与所述异常状态对应的状态指示灯，该状态指示灯能够帮助地面站的工作人员更快的找到出现故障的飞行器，从而进一步提高地面站的工作人员的工作效率。
举例而言，编队集群中的飞行器通常带有若干指示灯，包括但不限于机头灯、机臂灯，以及机身加载的用于灯光秀的表演灯，每个指示灯及表演灯都可以有亮灭以及多种颜色的变化。通过指示灯及表演灯的亮灭和颜色的变化以及它们的组合，可以形成上万种灯光状态组合，可以从其中挑选出辨识度较高的组合来显示飞行器对应的状态。实现逻辑如下：飞行器的飞控系统判断飞行器的工作状态，若所述工作状态为异常状态，则控制一种或多种灯光的组合来对应表示该异常的工作状态。该异常的工作状态包括但不限于：飞行器定位不成功、飞行器电池异常、飞行器传感器异常等，通过对应的灯光显示相关工作状态，当编队集群中的飞行器进行准备工作时，工作人员可以快速的从指示灯状态筛选出状态异常的飞行器，并且做出相应的处置措施，从而提高工作效率。
本发明实施例中，当满足预设条件时，检测自身的工作状态；若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。地面站的工作人员能够根据指示飞行器在编队中的位置的定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。
实施例二
请参考图4，本发明实施例还提供一种飞行器400，该飞行器包括存储器401、处理器402及存储在所述存储器上并可在所述处理器上运行的计算机程序（图中未示出），该所述计算机程序被所述处理器402执行时，实现如上述实施例一所述的飞行器状态指示方法的步骤。
本发明实施例的飞行器与上述实施例一的飞行器状态指示方法属于同一构思，其具体实现过程详见对应的方法实施例，且方法实施例中的技术特征在本飞行器实施例中均对应适用，这里不再赘述。
实施例三
本发明实施例还提供一种计算机可读存储介质，该计算机可读存储介质上存储有飞行器状态指示程序，所述飞行器状态指示程序被处理器执行时，实现如上述实施例一所述的飞行器状态指示方法的步骤。
本发明实施例的计算机可读存储介质与上述实施例一的方法属于同一构思，其具体实现过程详细见对应的方法实施例，且方法实施例中的技术特征在本计算机可读存储介质实施例中均对应适用，这里不再赘述。
上述各实施方式中的对应的技术特征在不导致方案矛盾或不可实施的前提下，可以相互使用。
需要说明的是，在本文中，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、物品或者装置不仅包括那些要素，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、物品或者装置所固有的要素。在没有更多限制的情况下，由语句“包括一个……”限定的要素，并不排除在包括该要素的过程、方法、物品或者装置中还存在另外的相同要素。
上述本发明实施例序号仅仅为了描述，不代表实施例的优劣。
通过以上的实施方式的描述，本领域的技术人员可以清楚地了解到上述实施例方法可借助软件加必需的通用硬件平台的方式来实现，当然也可以通过硬件，但很多情况下前者是更佳的实施方式。基于这样的理解，本发明的技术方案本质上或者说对现有技术做出贡献的部分可以以软件产品的形式体现出来，该计算机软件产品存储在一个存储介质（如ROM/RAM、磁碟、光盘）中，包括若干指令用以使得一台飞行器执行本发明各个实施例所述的方法。
上面结合附图对本发明的实施例进行了描述，但是本发明并不局限于上述的具体实施方式，上述的具体实施方式仅仅是示意性的，而不是限制性的，本领域的普通技术人员在本发明的启示下，在不脱离本发明宗旨和权利要求所保护的范围情况下，还可做出很多形式，这些均属于本发明的保护之内。
 工业实用性
本发明实施例提供的飞行器状态指示方法、飞行器及存储介质中，当满足预设条件时，检测自身的工作状态；若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。地面站的工作人员能够根据指示飞行器在编队中的位置的定位信息快速确定故障飞行器在编队中的位置，从而快速找到故障飞行器，并完成故障飞行器的维修或更换，提高了地面站的工作人员的工作效率。因此，具有工业实用性。

Claims (10)

  1. 一种飞行器状态指示方法，所述方法包括：
    当满足预设条件时，检测自身的工作状态；
    若所述工作状态为异常状态，则向地面站上报异常状态信息，所述异常状态信息包括用于指示自身在编队中的位置的定位信息和所述异常状态。
  2. 根据权利要求1所述的飞行器状态指示方法，其中，所述预设条件包括自身的工作状态检测定时时间到达和/或接收到地面站发送的工作状态检测指令。
  3. 根据权利要求1或2所述的飞行器状态指示方法，其中，所述检测自身的工作状态包括：检测自身的定位装置、电池、传感器、指示灯、表演灯、电机的至少一种是否正常工作。
  4. 根据权利要求1或2所述的飞行器状态指示方法，其中，所述用于指示自身在编队中的位置的定位信息包括自身在编队中的位置编码。
  5. 根据权利要求1或2所述的飞行器状态指示方法，其中，在当满足预设条件时，检测自身的工作状态之前，所述方法还包括：
    预置用于指示自身在编队中的位置的定位信息。
  6. 根据权利要求5所述的飞行器状态指示方法，其中，所述预置用于指示自身在编队中的位置的定位信息包括：预置自身在编队中的位置编码或者飞行器序列号与其在编队中的位置编码对应表。
  7. 根据权利要求1或2所述的飞行器状态指示方法，其中，所述用于指示自身在编队中的位置的定位信息包括自身的飞行器序列号，以便地面站根据所述飞行器序列号确定其在编队中的位置编码。
  8. 根据权利要求1所述的飞行器状态指示方法，其中，在向地面站上报异常状态信息之后，所述方法还包括：
    触发与所述异常状态对应的状态指示灯。
  9. 一种飞行器，包括存储器、处理器及存储在所述存储器上并可在所述处理器上运行的计算机程序，所述计算机程序被所述处理器执行时实现如权利要求1至8中任一项所述飞行器状态指示方法的步骤。
  10. 一种计算机可读存储介质，其上存储有飞行器状态指示程序，所述飞行器状态指示程序被处理器执行时实现如权利要求1至8中任一项所述的飞行器状态指示方法的步骤。
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