WO2016049906A1 - 一种飞行指示方法、装置及飞行器 - Google Patents

一种飞行指示方法、装置及飞行器 Download PDF

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Publication number
WO2016049906A1
WO2016049906A1 PCT/CN2014/088029 CN2014088029W WO2016049906A1 WO 2016049906 A1 WO2016049906 A1 WO 2016049906A1 CN 2014088029 W CN2014088029 W CN 2014088029W WO 2016049906 A1 WO2016049906 A1 WO 2016049906A1
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WIPO (PCT)
Prior art keywords
flight
aircraft
meteorological
information
limited
Prior art date
Application number
PCT/CN2014/088029
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English (en)
French (fr)
Inventor
欧泽林
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深圳市大疆创新科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to PCT/CN2014/088029 priority Critical patent/WO2016049906A1/zh
Priority to CN201911078462.4A priority patent/CN110780679B/zh
Priority to JP2016528201A priority patent/JP6174258B2/ja
Priority to CN201480007288.3A priority patent/CN104981748B/zh
Publication of WO2016049906A1 publication Critical patent/WO2016049906A1/zh
Priority to US15/468,430 priority patent/US10943494B2/en
Priority to US17/194,199 priority patent/US20210217315A1/en

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    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/003—Flight plan management
    • G08G5/0039—Modification of a flight plan
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0069—Navigation or guidance aids for a single aircraft specially adapted for an unmanned aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0091—Surveillance aids for monitoring atmospheric conditions
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/18502—Airborne stations
    • H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
    • 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
    • Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Definitions

  • the present invention relates to the field of flight technology, and in particular, to a flight prompting method, device and aircraft.
  • Aircraft such as UAV (Unmanned Aerial Vehicle) have been applied to certain scenarios.
  • the aircraft can perform high-altitude photography, unmanned reconnaissance, surveying and mapping, and highway surveying in automatic mode or user manual mode. , urban planning, ecological environmental monitoring, scientific investigation, oil exploration, aviation remote sensing, border patrol, forest fire prevention, disaster assessment and other tasks.
  • the technical problem to be solved by the embodiments of the present invention is to provide a flight prompting method and device, which can automatically and intelligently determine flight parameters affected by meteorological conditions in certain areas.
  • an embodiment of the present invention provides a flight indication method, including:
  • a flight limited indication is issued based on the determined restricted flight parameter object.
  • the acquiring meteorological information of the target flight area includes:
  • the weather reference information includes: specified weather reference information, or weather reference information generated based on the type of the aircraft.
  • the determining, according to the acquired meteorological information, the limited flight parameter object of the aircraft in the target flight area including:
  • the found flight parameters are determined as restricted flight parameter objects of the aircraft at the target flight area.
  • the mapping relationship between the preset meteorological information and the flight parameter includes a mapping relationship between the meteorological and its level information and the flight parameter;
  • the analysis determines the meteorological level of the acquired meteorological information
  • the associated flight parameters are searched for in the preset meteorological and flight parameter mapping relationship.
  • the determining, according to the acquired meteorological information, the limited flight parameter object of the aircraft in the target flight area including:
  • Parameter object Performing a preset simulator based on the acquired meteorological information as a simulated meteorological input parameter to determine the flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, thereby determining the limited flight of the aircraft in the target flight area.
  • the method further includes:
  • the issuing a flight limited indication based on the determined restricted flight parameter object includes: displaying the determined restricted flight parameter object; or generating, according to the determined limited flight parameter A flight limited indication of the aircraft limited flight is controlled and the flight limited indication is issued to control the aircraft restricted flight.
  • the issuing a flight limitation indication based on the determined restricted flight parameter object includes:
  • the flight limited indication is issued to control the aircraft to fly restricted.
  • the determined restricted flight parameter object comprises: a combination of any one or more of a flight speed parameter object, a flight altitude parameter object, and a flight distance range parameter object.
  • an embodiment of the present invention further provides a flight indication device, including:
  • An acquisition module configured to acquire weather information of a target flight area
  • a determining module configured to determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area
  • an indication module configured to issue a flight limited indication based on the determined restricted flight parameter object.
  • the obtaining module includes:
  • a region determining unit configured to use the current area of the aircraft or the designated area of the aircraft as the target flying area
  • a network unit configured to access, according to meteorological reference information of the aircraft, into the network and search for meteorological information indicated by the meteorological reference information of the target flight area;
  • the meteorological reference information includes: a specified meteorological reference Information, or meteorological reference information generated based on the type of aircraft.
  • the determining module includes:
  • a searching unit configured to search for a flight parameter associated with the acquired meteorological information according to the preset meteorological information and the flight parameter mapping relationship;
  • An object determining unit is configured to determine the found flight parameter as a limited flight parameter object of the aircraft in the target flight area.
  • the mapping relationship between the preset meteorological information and the flight parameter includes a mapping relationship between the meteorological and its level information and the flight parameter;
  • the searching unit is specifically configured to analyze and determine a meteorological level of the acquired meteorological information; and search for the associated flight parameter in the preset meteorological and flight parameter mapping relationship based on the meteorological information and the level thereof.
  • the determining module is specifically configured to run a preset simulator according to the acquired meteorological information as a simulated meteorological input parameter to determine a flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, and further A restricted flight parameter object of the aircraft at the target flight area is determined.
  • the device further includes:
  • a flight processing module configured to determine whether a flight path of the target flight area is included in a flight mission of the aircraft; if yes, modify and update the determined limited flight parameter object according to the meteorological information, In order to make the aircraft fly normally.
  • the indication module is specifically configured to display the determined limited flight parameter object; or generate a flight limitation for controlling the limited flight of the aircraft according to the determined limited flight parameter. Instructing and issuing the flight limited indication to control the aircraft to be restricted in flight.
  • the indicating module is specifically configured to provide the limited flight parameter object to a user selection; and according to the selecting operation of the limited flight parameter object provided, generating, for controlling the limited aircraft Flight limited indication of flight; the flight limited indication is issued to control the aircraft to fly restricted.
  • an embodiment of the present invention further provides an aircraft, including: a communication device and a processor, wherein the processor is configured to acquire weather information of a target flight area by using the communication device; and determine, according to the acquired meteorological information A restricted flight parameter object of the aircraft at the target flight area; a flight limited indication is issued based on the determined restricted flight parameter object.
  • the embodiment of the present invention may determine the limited flight parameter based on the acquired meteorological information of the target flight area, thereby making an indication of flight limitation, and may promptly remind the user or directly control the drone to perform safely in the target flight area.
  • the mission of the aircraft better guarantees the flight safety of the aircraft and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • FIG. 1 is a schematic flow chart of a flight prompting method according to an embodiment of the present invention.
  • FIG. 2 is a schematic flow chart of another flight prompting method according to an embodiment of the present invention.
  • FIG. 3 is a schematic flow chart of still another flight prompting method according to an embodiment of the present invention.
  • FIG. 4 is a schematic flow chart of still another flight prompting method according to an embodiment of the present invention.
  • FIG. 5 is a schematic structural diagram of a flight indicating device according to an embodiment of the present invention.
  • Fig. 6 is a schematic structural view of an aircraft according to an embodiment of the present invention.
  • the embodiment of the invention can automatically acquire the meteorological information of a certain target area, and then determine one or more flight parameter objects that may be subject to meteorological conditions according to the meteorological information, so that the user or the aircraft can select whether according to the needs of the flight task. Cancel the mission or modify the mission.
  • the target area may refer to an area that the aircraft needs to pass when performing the flight automatic flight, or may also be some areas designated by the user as needed.
  • FIG. 1 is a schematic flowchart of a flight prompting method according to an embodiment of the present invention.
  • the method according to an embodiment of the present invention may be provided by a smart phone, a tablet computer, a smart wearable device, and the like with network function capable of controlling an aircraft.
  • the mobile terminal implementation can also be implemented by a flight controller with a network communication function provided on the aircraft.
  • the embodiment of the present invention is described by using an implementation in an intelligent mobile terminal as an example. Specifically, the method includes:
  • the weather information of the target flight area may be queried by accessing the server that provides the meteorological information through the Internet, etc., and the meteorological information that needs to be queried may be all meteorological information that the server can provide, or
  • the intelligent mobile terminal determines relevant flight parameters of its existence based on the model and performance of the aircraft, and then queries or selects the required weather information from all weather information based on the determined parameters.
  • the smart mobile terminal or aircraft may have its own meteorological monitoring function, such as a monitoring mechanism with simple wind speed, wind direction, air temperature, air pressure, etc., so that it is necessary to fly based on these monitoring when flying in a certain area.
  • meteorological monitoring function such as a monitoring mechanism with simple wind speed, wind direction, air temperature, air pressure, etc.
  • S102 Determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area.
  • the mobile terminal can evaluate the flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft according to the preset simulator, thereby calculating one or more flight parameters (limited flight) that may be limited by the aircraft.
  • Parameter object In the simulator of the mobile terminal, the meteorological environment can be simulated based on the level of the wind speed, the temperature level of the air temperature, and the air pressure value, and the simulated aircraft in the simulator can be used to accurately estimate the limited flight parameters. Object.
  • a mapping table including a mapping relationship between climate information and flight parameters may be set.
  • the mapping table may specifically include a one-to-one mapping relationship between climate and its rating information and climate parameters.
  • the S103 may specifically include: displaying the determined limited flight parameter object; or issuing a flight limit control instruction according to the determined limited flight parameter.
  • the flight limitation indication may be only a prompt information for prompting the user in a preset format, and the mobile terminal may display the limited flight parameter object as a flight restriction indication in a list form in the display screen.
  • the flight restriction indication may also include suggestion information to the user, for example, after determining the visibility information based on the smog level, the recommendation information of the flight limit and the limit is issued. Specifically, if the visibility is 100 meters, the limitation is issued. Flight limited indication with a flying altitude of 100 meters.
  • the flight controller may send relevant information to the designated user terminal in the S103 to achieve the purpose of prompting the user for the limited flight parameters.
  • the flight limited indication information may also be a flight control command issued based on the restricted flight parameters and the corresponding climate information.
  • the flight control command of the limit height and the limit distance may be generated as the flight restriction instruction, so as to limit the flight altitude, the flight distance, etc. when the aircraft is flying in the target flight area, and determine Flight safety.
  • the prompt information suitable for flight may be issued.
  • the obtained meteorological information can be displayed at the position specified by the display screen, and further displayed in the form of an icon, so that the user can intuitively view the weather of the target area.
  • the embodiment of the present invention may determine the limited flight parameter based on the acquired meteorological information of the target flight area, thereby making an indication of flight limitation, and may promptly remind the user or directly control the drone to perform safely in the target flight area.
  • the mission of the aircraft better guarantees the flight safety of the aircraft and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • FIG. 2 it is a schematic flowchart of another flight prompting method according to an embodiment of the present invention.
  • the method according to the embodiment of the present invention may be provided with a network function such as a smart phone, a tablet computer, and a smart wearable device capable of controlling an aircraft.
  • the intelligent mobile terminal is implemented, or it can also be implemented by a flight controller provided on the aircraft and having a network communication function.
  • the method includes:
  • the S201 may include: using a current area of the aircraft or a user designated area as a target flight area; accessing the network and searching for the target flight area according to the meteorological reference information of the aircraft; Meteorological information indicated by the information; the meteorological reference information includes: specified meteorological reference information, or meteorological reference information generated based on the type of the aircraft; the meteorological reference information is used to indicate that the meteorological information needs to be searched, for example, the meteorological reference information includes the wind speed Indication, wind direction indication, etc., which can make the amount of data searched smaller.
  • S203 Determine the found flight parameter as a limited flight parameter object of the aircraft in the target flight area.
  • the mapping relationship between the preset meteorological information and the flight parameter includes mapping relationship between the meteorological and its level information and the flight parameter; and searching for the flight associated with the acquired meteorological information according to the preset mapping relationship between the meteorological and flight parameters
  • the parameters include: analyzing and determining the meteorological level of the acquired meteorological information; and searching for the associated flight parameters in the preset meteorological and flight parameter mapping relationship based on the meteorological information and its level. For example, a slightly graded haze does not correlate flight range parameters and flight altitude parameters, and flight range parameters and fly height parameters are not determined to be restricted flight parameters under mild grade haze weather conditions.
  • the determined restricted flight parameter object includes a combination of any one or more of a flight speed parameter object, a fly height parameter object, and a flight distance range parameter object.
  • the flight limited indication is directly presented to the aircraft user as a reminder message.
  • S205 Determine whether a flight path of the target flight area is included in a flight mission of the aircraft.
  • the flight path can be modified to avoid the target flight zone or to increase flight restrictions such as limits on flight height in the flight zone.
  • the limited flight parameters of the plurality of different regions may be simultaneously acquired in the S201 to the S203, and each region is determined in S205 and S206 to determine whether the aircraft is required The executed mission is modified.
  • the embodiment of the present invention can quickly determine the limited flight parameters based on the acquired meteorological information and the mapping table of the target flight area, thereby making an indication of flight limitation, and can promptly remind the user and modify the flight task of the aircraft.
  • the UAV can safely perform flight missions in various areas, which better ensures the flight safety of the aircraft and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • FIG. 3 it is a schematic flowchart of still another method for flying prompts according to an embodiment of the present invention.
  • the method of the embodiment of the present invention may be provided with a network function such as a smart phone, a tablet computer, and a smart wearable device capable of controlling an aircraft.
  • the intelligent mobile terminal is implemented, or it can also be implemented by a flight controller provided on the aircraft and having a network communication function.
  • the method includes:
  • the S301 may include: using a current area of the aircraft or a user designated area as a target flight area; accessing the network and searching for the target flight area according to the weather reference information of the aircraft; Meteorological information indicated by the information; the meteorological reference information includes: specified meteorological reference information, or meteorological reference information generated based on the type of the aircraft.
  • S302 Run a preset simulator according to the acquired meteorological information as a simulated meteorological input parameter to determine a flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, thereby determining the aircraft being subjected to the target flight area.
  • Limited flight parameter object Run a preset simulator according to the acquired meteorological information as a simulated meteorological input parameter to determine a flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, thereby determining the aircraft being subjected to the target flight area.
  • the determined restricted flight parameter object includes: a combination of any one or more of a flight speed parameter object, a flight altitude parameter object, and a flight distance range parameter object.
  • the flight limited indication may be directly presented to the aircraft user as a reminder message.
  • S304 Determine whether a flight path of the target flight area is included in a flight mission of the aircraft.
  • the flight path can be modified to avoid the target flight zone or to increase flight restrictions such as limits on flight height in the flight zone.
  • the limited flight parameters of the plurality of different regions may be simultaneously acquired in the S301 to the S302, and each region is determined in S304 and S305 to determine whether the aircraft is required to be The executed mission is modified.
  • the embodiment of the present invention can determine the limited flight parameters based on the acquired meteorological information and the simulator of the target flight area, thereby making an indication of flight limitation, and can promptly remind the user and modify the flight task of the aircraft. It enables the drone to perform flight missions in various areas more safely, better guarantees the flight safety of the aircraft, and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • FIG. 4 it is a schematic flowchart of another flight prompting method according to an embodiment of the present invention.
  • the method according to the embodiment of the present invention may be provided with a network function such as a smart phone, a tablet computer, and a smart wearable device capable of controlling an aircraft.
  • the intelligent mobile terminal implementation can also be implemented by a flight controller with a network communication function provided on the aircraft.
  • the method includes:
  • the S401 may include: using a current area of the aircraft or a user designated area as a target flight area; accessing the network and searching for the target flight area according to the weather reference information of the aircraft; Meteorological information indicated by the information; the meteorological reference information includes: specified meteorological reference information, or meteorological reference information generated based on the type of the aircraft.
  • S402 Determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area.
  • the S402 may specifically include: searching for a flight parameter associated with the acquired meteorological information according to the preset meteorological information and the flight parameter mapping relationship.
  • the found flight parameters are determined as restricted flight parameter objects of the aircraft at the target flight area.
  • the S402 may include: running a preset simulator according to the acquired meteorological information as a simulated meteorological input parameter to determine a flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, thereby determining the aircraft.
  • a restricted flight parameter object at the target flight area may be found.
  • the mapping relationship between the preset meteorological information and the flight parameter includes mapping relationship between the meteorological and its level information and the flight parameter; and searching for the flight associated with the acquired meteorological information according to the preset mapping relationship between the meteorological and flight parameters
  • the parameters include: analyzing and determining the meteorological level of the acquired meteorological information; and searching for the associated flight parameters in the preset meteorological and flight parameter mapping relationship based on the meteorological information and its level.
  • the determined restricted flight parameter object includes a combination of any one or more of a flight speed parameter object, a fly height parameter object, and a flight distance range parameter object.
  • each of the determined limited flight parameter objects may be displayed to the user in the form of a button to facilitate the user to click to select.
  • S404 Generate a flight limited indication for controlling the limited flight of the aircraft according to the selection operation of the limited flight parameter object provided.
  • the user can select one or more parameters that are allowed to be restricted, or select one or more parameters that are not allowed to be restricted, by touch screen clicking or mouse clicking.
  • S405 Issue the flight limited indication to control the aircraft limited flight.
  • Selective flight restrictions are based on the user's actual choice. For example, foggy weather determines the limit of flight distance, but since the user is currently in a sparsely populated area, the user can choose not to be limited by the flight distance, and does not include control when issuing a flight limited indication. Control information for the flight of the aircraft within a limited distance (the distance the aircraft is from the user).
  • the embodiment of the present invention can determine the limited flight parameters based on the acquired meteorological information and the simulator of the target flight area, thereby making an indication of flight limitation, and can promptly remind the user and modify the flight task of the aircraft. It enables the drone to perform flight missions in various areas more safely, better guarantees the flight safety of the aircraft, and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • FIG. 5 is a schematic structural diagram of a flight indication device according to an embodiment of the present invention.
  • the flight indication device according to the embodiment of the present invention may be disposed in a smart terminal device, such as a smart phone, a tablet computer, and a smart wearable device. . It can also be placed directly in the flight controller of the aircraft.
  • the device includes:
  • a determining module 2 configured to determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area;
  • the indicating module 3 is configured to issue a flight limited indication based on the determined limited flight parameter object.
  • the acquiring module 1 can access the meteorological information in the server that provides the meteorological information through the Internet or the like, and query the meteorological information of the target flight area.
  • the meteorological information that needs to be queried may be all meteorological information that the server can provide, or may be intelligent mobile
  • the terminal determines the relevant flight parameters of its existence based on the model and performance of the aircraft, and then queries or selects the required meteorological information from all meteorological information based on the determined parameters.
  • the flight limited indication information may also be a flight control command issued based on the restricted flight parameters and the corresponding climate information.
  • the flight control command of the limit height and the limit distance may be generated as the flight restriction instruction, so as to limit the flight altitude, the flight distance, etc. when the aircraft is flying in the target flight area, and determine Flight safety.
  • the prompt information suitable for flight may be issued.
  • the obtaining module 1 may include:
  • a region determining unit configured to use the current area of the aircraft or the designated area of the aircraft as the target flying area
  • a network unit configured to access, according to meteorological reference information of the aircraft, into the network and search for meteorological information indicated by the meteorological reference information of the target flight area;
  • the meteorological reference information includes: a specified meteorological reference Information, or meteorological reference information generated based on the type of aircraft.
  • the acquisition module 1 can implement meteorological monitoring based on a meteorological monitoring function of the terminal or the aircraft, such as a monitoring mechanism with simple wind speed, wind direction, air temperature, air pressure, and the like.
  • the determining module 2 may specifically determine the restricted parameter in the form of a look-up table or a simulator. Specifically, the determining module 2 may include:
  • a searching unit configured to search for a flight parameter associated with the acquired meteorological information according to the preset meteorological information and the flight parameter mapping relationship;
  • An object determining unit is configured to determine the found flight parameter as a limited flight parameter object of the aircraft in the target flight area.
  • mapping relationship between the preset meteorological information and the flight parameter includes a mapping relationship between the meteorological and its grade information and the flight parameter;
  • the searching unit is specifically configured to analyze and determine a meteorological level of the acquired meteorological information; and search for the associated flight parameter in the preset meteorological and flight parameter mapping relationship based on the meteorological information and the level thereof.
  • the determining module 2 is specifically configured to run a preset simulator according to the acquired meteorological information as a simulated meteorological input parameter to determine a flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft. A restricted flight parameter object of the aircraft in the target flight area is then determined.
  • the device of the embodiment of the present invention may automatically perform the update modification of the flight task, and the device of the embodiment of the present invention may further include:
  • a flight processing module 4 configured to determine whether a flight path of the target flight area is included in a flight mission of the aircraft; if yes, modify and update the determined limited flight parameter object according to the meteorological information In order to make the aircraft fly normally.
  • the indication module 3 may be used to display the determined limited flight parameter object when used to issue a flight limited indication; or generated according to the determined limited flight parameter.
  • a flight limited indication of the aircraft limited flight is controlled and the flight limited indication is issued to control the aircraft restricted flight.
  • the indicating module 3 is further configured to provide the limited flight parameter object to the user for selecting when the flight limited indication is issued; according to the limited flight parameter object provided A selection operation is generated to generate a flight limited indication for controlling the aircraft limited flight; the flight limited indication is issued to control the aircraft restricted flight.
  • the embodiment of the present invention may determine the limited flight parameter based on the acquired meteorological information of the target flight area, thereby making an indication of flight limitation, and may promptly remind the user or directly control the drone to perform safely in the target flight area.
  • the mission of the aircraft better guarantees the flight safety of the aircraft and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • the aircraft of the embodiment of the present invention includes an existing related structure for implementing flight, specifically including an aircraft main body, a power supply, a power component, and some The attached camera, the pan-tilt device, and the like, further includes a memory for storing the flight indication application.
  • the aircraft includes: the communication device 100 and the processor 200, wherein the processing And the related application in the memory is used to acquire meteorological information of the target flight area through the communication device 100; and determine a limited flight parameter object of the aircraft in the target flight area according to the acquired meteorological information; A flight limited indication is issued based on the determined restricted flight parameter object.
  • the processor 200 is connected to the meteorological information of the network search target flight area through the communication device 100, and can transmit the restricted flight object as a flight restriction indication to the designated user terminal through the communication device 100.
  • the processor 200 calls an application in the memory, and can also be used to determine whether a flight path of the target flight area is included in the flight mission of the aircraft; if yes, according to the meteorological information pair The determined restricted flight parameter object is modified to update the aircraft to fly normally.
  • the processor 200 when used to acquire the meteorological information of the target flight area, the processor 200 is specifically configured to use the current area of the aircraft or the designated area of the aircraft as the target flight area; and access according to the meteorological reference information of the aircraft. Go to the network and search for meteorological information indicated by the weather reference information of the target flight area; the weather reference information includes: specified meteorological reference information, or meteorological reference information generated based on the type of the aircraft.
  • the processor 200 is configured to determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area, specifically for searching according to preset mapping relationship between meteorological information and flight parameters.
  • a flight parameter associated with the acquired meteorological information determining the found flight parameter as a restricted flight parameter object of the aircraft in the target flight area.
  • the processor 200 is configured to determine, according to the acquired meteorological information, a limited flight parameter object of the aircraft in the target flight area, and specifically configured to run the pre-prepared weather information according to the acquired meteorological information.
  • the simulator is configured to determine the flight impact of the simulated meteorological environment generated by each climate information on the simulated aircraft, thereby determining the limited flight parameter object of the aircraft in the target flight area.
  • the processor 200 is specifically configured to display the determined limited flight parameter object when the flight limited indication is issued based on the determined limited flight parameter object; or according to the determining The restricted flight parameters generate a flight limited indication for controlling the aircraft limited flight and issue the flight limited indication to control the aircraft restricted flight.
  • the processor 200 is specifically configured to provide the limited flight parameter object to a user selection when the flight limited indication is issued based on the determined limited flight parameter object; Determining a restricted flight parameter object, generating a flight limited indication for controlling the aircraft restricted flight; issuing the flight limited indication to control the aircraft restricted flight.
  • processor 200 of the aircraft in the embodiment of the present invention may refer to the description of the foregoing method and device related content.
  • the embodiment of the present invention may determine the limited flight parameter based on the acquired meteorological information of the target flight area, thereby making an indication of flight limitation, and may promptly remind the user or directly control the drone to perform safely in the target flight area.
  • the mission of the aircraft better guarantees the flight safety of the aircraft and meets the needs of the aircraft users for the automation and intelligence of meteorological information.
  • the related apparatus and method disclosed may be implemented in other manners.
  • the device embodiments described above are merely illustrative.
  • the division of the modules or units is only a logical function division.
  • there may be another division manner for example, multiple units or components may be used. Combinations can be integrated into another system, or some features can be ignored or not executed.
  • the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, device or unit, and may be in an electrical, mechanical or other form.
  • the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, may be located in one place, or may be distributed to multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of the embodiment.
  • each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
  • the above integrated unit can be implemented in the form of hardware or in the form of a software functional unit.
  • the integrated unit if implemented in the form of a software functional unit and sold or used as a standalone product, may be stored in a computer readable storage medium.
  • the technical solution of the present invention which is essential or contributes to the prior art, or all or part of the technical solution, may be embodied in the form of a software product stored in a storage medium.
  • a number of instructions are included to cause a computer processor to perform all or part of the steps of the methods described in various embodiments of the present invention.
  • the foregoing storage medium includes: a U disk, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk, or an optical disk, and the like. .

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Abstract

一种飞行指示方法、装置及飞行器，其中，所述方法包括：获取目标飞行区域的气象信息（S101）；根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象（S102）；基于确定出的受限飞行参数对象发出飞行受限指示（S103）。该方法基于获取的目标飞行区域的气象信息来确定受限飞行参数，以此做出飞行受限的指示，可以预先提醒用户或者直接控制无人机较为安全的执行在所述目标飞行区域的飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。

Description

一种飞行指示方法、装置及飞行器 技术领域
本发明涉及飞行技术领域，尤其涉及一种飞行提示方法、装置及飞行器。
背景技术
诸如UAV（Unmanned Aerial Vehicle，无人驾驶飞机）等飞行器已应用到某些特定的场景中，飞行器可以在自动模式或者用户手动模式下，执行诸如高空摄像、无人探测侦察、测量测绘、公路勘测、城市规划、生态环保监控、科学考察、石油勘探、航空遥感、边防巡逻、森林防火、灾情评估等任务。
在飞行器飞行控制过程中，大多数用户并不清楚气候条件会对飞行带来的影响，可能会导致飞行器的损坏。
发明内容
本发明实施例主要解决的技术问题在于，提供了一种飞行提示方法及装置，能够自动化、智能化地确定出某些区域中受气象条件影响的飞行参数。
一方面，本发明实施例提供了一种飞行指示方法，包括：
获取目标飞行区域的气象信息；
根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；
基于确定出的受限飞行参数对象发出飞行受限指示。
其中可选地，所述获取目标飞行区域的气象信息，包括：
将飞行器当前所在区域或用户指定区域作为目标飞行区域；
根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；
所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
其中可选地，所述根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，包括：
根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；
将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
其中可选地，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；
所述根据预置的气象与飞行参数映射关系，查找与获取的气象信息关联的飞行参数，包括：
分析确定出获取的气象信息的气象等级；
基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。
其中可选地，所述根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，包括：
根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
其中可选地，所述方法还包括：
判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；
若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
其中可选地，所述基于确定出的受限飞行参数对象发出飞行受限指示，包括：显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
其中可选地，所述基于确定出的受限飞行参数对象发出飞行受限指示，包括：
将所述受限飞行参数对象提供给用户选择；
根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；
发出所述飞行受限指示以控制所述飞行器受限飞行。
其中可选地，所述确定出的受限飞行参数对象包括：飞行速度参数对象、飞行高度参数对象、飞行距离范围参数对象中的任一种或多种的组合。
另一方面，本发明实施例还提供了一种飞行指示装置，包括：
获取模块，用于获取目标飞行区域的气象信息；
确定模块，用于根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；
指示模块，用于基于确定出的受限飞行参数对象发出飞行受限指示。
其中可选地，所述获取模块包括：
区域确定单元，用于将飞行器当前所在区域或用户指定区域作为目标飞行区域；
网络单元，用于根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
其中可选地，所述确定模块包括：
查找单元，用于根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；
对象确定单元，用于将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
其中可选地，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；
所述查找单元，具体用于分析确定出获取的气象信息的气象等级；基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。
其中可选地，所述确定模块，具体用于根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
其中可选地，所述装置还包括：
飞行处理模块，用于判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
其中可选地，所述指示模块，具体用于显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
其中可选地，所述指示模块，具体用于将所述受限飞行参数对象提供给用户选择；根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；发出所述飞行受限指示以控制所述飞行器受限飞行。
相应地，本发明实施例还提供了一种飞行器，包括：通信装置和处理器，其中，所述处理器，用于通过所述通信装置获取目标飞行区域的气象信息；根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；基于确定出的受限飞行参数对象发出飞行受限指示。
本发明实施例可基于获取的目标飞行区域的气象信息来确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户或者直接控制无人机较为安全的执行在所述目标飞行区域的飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
 附图说明
图1是本发明实施例的一种飞行提示方法的流程示意图；
图2是本发明实施例的另一种飞行提示方法的流程示意图；
图3是本发明实施例的再一种飞行提示方法的流程示意图；
图4是本发明实施例的又一种飞行提示方法的流程示意图；
图5是本发明实施例的一种飞行指示装置的结构示意图；
图6是本发明实施例的一种飞行器的结构示意图。
具体实施方式
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。
本发明实施例能够自动获取某个目标区域的气象信息，然后根据气象信息确定出一个或者多个可能会受气象条件限制的飞行参数对象，以便于用户或者飞行器能够根据飞行任务的需要，选择是否取消该飞行任务或者对该飞行任务进行修改。所述的目标区域可以是指飞行器执行飞行任务自动飞行时需要经过的区域，或者也可以是用户根据需要指定的某些区域。
请参见图1，是本发明实施例的一种飞行提示方法的流程示意图，本发明实施例的所述方法可以由能够控制飞行器的智能手机、平板电脑、智能可穿戴设备等带网络功能的智能移动终端实现，当然，也可以由设置在飞行器上的、且带网络通信功能的飞行控制器来实现。本发明实施例以在智能移动终端中实现为例来对所述方法进行说明，具体的，所述方法包括：
S101：获取目标飞行区域的气象信息。
在一种实现方式中，可以通过互联网等接入到提供气象信息的服务器中，查询目标飞行区域的气象信息，需要查询的气象信息可以是该服务器所能够提供的全部的气象信息，也可以是智能移动终端基于飞行器的型号、性能确定其存在的相关飞行参数，然后基于确定出的参数来查询或者从全部气象信息中筛选出所需的气象信息。
在其他实施例中，智能移动终端或飞行器可以自带气象监测功能，例如自带简单的风速、风向、气温、气压等气象信息的监测机构，以便于需要在某个区域飞行时，基于这些监测机构来实现气象信息的监测。
S102：根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象。
移动终端可以根据预置的模拟器来评估由各个气候信息产生的模拟气象环境对其中的模拟飞行器的飞行影响，从而计算确定出飞行器的可能会受限的一个或者多个飞行参数（受限飞行参数对象）。在移动终端的模拟器中，具体可以基于风速的等级，气温的温度等级以及气压值等来模拟出气象环境，并作用于模拟器中的模拟飞行器，以便于较为精确地评估出受限飞行参数对象。
当然，在一种简单的实现方式中，可以设置包括气候信息与飞行参数映射关系的映射表。该映射表中具体可以包括气候及其等级信息与气候参数的一一映射关系。在获取到目标飞行区域的气象信息后，基于气象信息的具体数据（例如风速等级）查找映射表，即可得到可能的飞行受限参数对象，查表的方式相对较为快捷，实现方便。
S103：基于确定出的受限飞行参数对象发出飞行受限指示。
本发明实施例中，所述S103具体可以包括：显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数发出飞行限制控制指令。
其中，所述飞行受限指示可以仅仅是一种预置格式的用于提示用户的提示信息，移动终端可以在显示屏中以列表的形式显示受限飞行参数对象作为飞行受限指示，该类飞行受限指示中还可以加入对用户的建议信息，例如：基于雾霾等级确定出能见度信息后，发出飞行限高、限远的建议信息，具体的，若能见度为100米，则发出包括限制飞行高度为100米的飞行受限指示。
需要说明的是，如果是由飞行器的飞行控制器实现，则在所述S103中飞行控制器可以向指定的用户终端发送相关信息以达到向用户提示受限飞行参数的目的。
所述飞行受限指示信息也可以是基于受限飞行参数以及对应的气候信息，发出的飞行控制指令。如上述，在基于雾霾等级确定出能见度信息后，可以产生限高和限远的飞行控制指令作为飞行受限指示，以便于飞行器在目标飞行区域飞行时，限制飞行高度、飞行距离等，确定飞行安全。
还可以进一步地对应显示警告等级，对于一些非常危险的气象情况，例如强风环境，发出红色报警等。并且，在本发明实施例中，对于条件良好的气象情况，即没有确定出飞行受限指示，则可以发出适宜飞行的提示信息。
另外还可以将获取到的气象信息显示在显示屏指定的位置处，并进一步绘制图标的形式来显示，方便用户直观地查看目标区域的气象。
本发明实施例可基于获取的目标飞行区域的气象信息来确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户或者直接控制无人机较为安全的执行在所述目标飞行区域的飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
再请参见图2，是本发明实施例的另一种飞行提示方法的流程示意图，本发明实施例的所述方法可以由能够控制飞行器的智能手机、平板电脑、智能可穿戴设备等带网络功能的智能移动终端实现，或者，也可以由设置在飞行器上的、且带网络通信功能的飞行控制器来实现。具体的，所述方法包括：
S201：获取目标飞行区域的气象信息。
具体的，所述S201可以包括：将飞行器当前所在区域或用户指定区域作为目标飞行区域；根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息；气象参考信息用于指示需要搜索那些气象信息，例如：气象参考信息包括风速指示、风向指示等，这样可使得搜索的数据量较小。
S202：根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数。
S203：将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
其中具体的，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；所述根据预置的气象与飞行参数映射关系，查找与获取的气象信息关联的飞行参数，包括：分析确定出获取的气象信息的气象等级；基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。例如，轻微等级的雾霾并不会关联飞行距离范围参数和飞行高度参数，在轻微等级的雾霾的气象条件下，飞行距离范围参数和飞行高度参数不会被确定为受限飞行参数。
所述确定出的受限飞行参数对象包括：飞行速度参数对象、飞行高度参数对象、飞行距离范围参数对象中的任一种或多种的组合。
S204：基于确定出的受限飞行参数对象发出飞行受限指示。
在本发明实施例中，直接将所述飞行受限指示作为一个提示信息展示给飞行器用户。
S205：判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径。
S206：若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
在本发明实施例中，在所述S203中确定出受限飞行参数对象后，如果飞行器在执行自动飞行任务，则判断该飞行器的飞行任务中是否有在所述目标飞行区域的飞行路径，如果是，则可以对该飞行路径进行修改，避开该目标飞行区域或者在该飞行区域中增加关于飞行高度的限制等飞行限制。
在本发明实施例中，可以在所述S201至所述S203中同时获取多个不同区域的受限飞行参数，并在S205和S206中对每一个区域进行判断，以确定是否对所述飞行器所要执行的飞行任务进行修改。
本发明实施例可基于获取的目标飞行区域的气象信息和映射表来快速地确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户、且可以对飞行器的飞行任务进行修改，使得无人机能够较为安全的在各个区域中执行飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
再请参见图3，是本发明实施例的再一种飞行提示方法的流程示意图，本发明实施例的所述方法可以由能够控制飞行器的智能手机、平板电脑、智能可穿戴设备等带网络功能的智能移动终端实现，或者，也可以由设置在飞行器上的、且带网络通信功能的飞行控制器来实现。具体的，所述方法包括：
S301：获取目标飞行区域的气象信息。
具体的，所述S301可以包括：将飞行器当前所在区域或用户指定区域作为目标飞行区域；根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
S302：根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
其中具体的，所述确定出的受限飞行参数对象包括：飞行速度参数对象、飞行高度参数对象、飞行距离范围参数对象中的任一种或多种的组合。
S303：基于确定出的受限飞行参数对象发出飞行受限指示。
在本发明实施例中，可以直接将所述飞行受限指示作为一个提示信息展示给飞行器用户。
S304：判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径。
S305：若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
在本发明实施例中，在所述S302中确定出受限飞行参数对象后，如果飞行器在执行自动飞行任务，则判断该飞行器的飞行任务中是否有在所述目标飞行区域的飞行路径，如果是，则可以对该飞行路径进行修改，避开该目标飞行区域或者在该飞行区域中增加关于飞行高度的限制等飞行限制。
在本发明实施例中，可以在所述S301至所述S302中同时获取多个不同区域的受限飞行参数，并在S304和S305中对每一个区域进行判断，以确定是否对所述飞行器所要执行的飞行任务进行修改。
本发明实施例可基于获取的目标飞行区域的气象信息和模拟器可以较为全面地确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户、且可以对飞行器的飞行任务进行修改，使得无人机能够较为安全的在各个区域中执行飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
再请参见图4，是本发明实施例的又一种飞行提示方法的流程示意图，本发明实施例所述的方法可以由能够控制飞行器的智能手机、平板电脑、智能可穿戴设备等带网络功能的智能移动终端实现，当然，也可以由设置在飞行器上的、且带网络通信功能的飞行控制器来实现。所述方法包括：
S401：获取目标飞行区域的气象信息。
具体的，所述S401可以包括：将飞行器当前所在区域或用户指定区域作为目标飞行区域；根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
S402：根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象。
在本发明实施例中，所述S402具体可以包括：根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数。将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。或者具体的，所述S402可以包括：根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
其中具体的，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；所述根据预置的气象与飞行参数映射关系，查找与获取的气象信息关联的飞行参数，包括：分析确定出获取的气象信息的气象等级；基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。所述确定出的受限飞行参数对象包括：飞行速度参数对象、飞行高度参数对象、飞行距离范围参数对象中的任一种或多种的组合。
S403：将所述受限飞行参数对象提供给用户选择；
具体可以将确定的每一个受限飞行参数对象以按钮的形式显示给用户，以方便用户点击选择。
S404：根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示。
用户可根据需要通过触屏点击或者鼠标点击等方式选择出一个或者多个允许受限的参数，或者选择出一个或者多个不允许受限的参数。
S405：发出所述飞行受限指示以控制所述飞行器受限飞行。
根据用户的实际选择，进行选择性的飞行限制。例如，有雾霾天气确定出对飞行距离的限制，但是由于用户当前处于人烟稀少且空旷的区域，此时用户可以选择不受飞行距离的限制，在发出飞行受限指示时并不包括用于控制飞行器在所限制的距离内（飞行器距离用户的距离）飞行的控制信息。
本发明实施例可基于获取的目标飞行区域的气象信息和模拟器可以较为全面地确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户、且可以对飞行器的飞行任务进行修改，使得无人机能够较为安全的在各个区域中执行飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
下面对本发明实施例的飞行指示装置及飞行器进行详细描述。
请参见图5，是本发明实施例的一种飞行指示装置的结构示意图，本发明实施例所述的飞行指示装置可设置在智能终端设备中，如智能手机、平板电脑以及智能可穿戴设备等。也可以直接设置在飞行器的飞行控制器中。具体的，所述装置包括：
获取模块1，用于获取目标飞行区域的气象信息；
确定模块2，用于根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；
指示模块3，用于基于确定出的受限飞行参数对象发出飞行受限指示。
所述获取模块1可以通过互联网等接入到提供气象信息的服务器中，查询目标飞行区域的气象信息，需要查询的气象信息可以是该服务器所能够提供的全部的气象信息，也可以是智能移动终端基于飞行器的型号、性能确定其存在的相关飞行参数，然后基于确定出的参数来查询或者从全部气象信息中筛选出所需的气象信息。
所述飞行受限指示信息也可以是基于受限飞行参数以及对应的气候信息，发出的飞行控制指令。如上述，在基于雾霾等级确定出能见度信息后，可以产生限高和限远的飞行控制指令作为飞行受限指示，以便于飞行器在目标飞行区域飞行时，限制飞行高度、飞行距离等，确定飞行安全。
还可以进一步地对应显示警告等级，对于一些非常危险的气象情况，例如强风环境，发出红色报警等。并且，在本发明实施例中，对于条件良好的气象情况，即没有确定出飞行受限指示，则可以发出适宜飞行的提示信息。
具体的，所述获取模块1可以包括：
区域确定单元，用于将飞行器当前所在区域或用户指定区域作为目标飞行区域；
网络单元，用于根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
在其他实施例中，所述获取模块1可以基于终端或飞行器自带的气象监测功能，例如自带简单的风速、风向、气温、气压等气象信息的监测机构，来实现气象信息的监测。
所述确定模块2具体可以通过查表或者模拟器的形式来确定受限参数，具体可选地，所述确定模块2可以包括：
查找单元，用于根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；
对象确定单元，用于将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
其中，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；
所述查找单元，具体用于分析确定出获取的气象信息的气象等级；基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。
进一步可选地，所述确定模块2，具体用于根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
进一步可选地，在确定了受限飞行参数对象后，本发明实施例的所述装置可以自动地进行飞行任务的更新修改，本发明实施例的所述装置具体还可以包括：
飞行处理模块4，用于判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
进一步可选地，所述指示模块3在用于发出飞行受限指示时，具体可以用于显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
进一步可选地，所述指示模块3在用于发出飞行受限指示时，具体还可以用于将所述受限飞行参数对象提供给用户选择；根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；发出所述飞行受限指示以控制所述飞行器受限飞行。
需要说明的是，本发明实施例的所述装置中的各个模块、单元的具体实现可对应地参考上述方法项实施例的描述。
本发明实施例可基于获取的目标飞行区域的气象信息来确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户或者直接控制无人机较为安全的执行在所述目标飞行区域的飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
再请参见图6，是本发明实施例的一种飞行器的结构示意图，本发明实施例的所述飞行器包括现有的实现飞行的相关结构，具体包括飞行器主体、供电电源、动力组件，以及一些附属的拍摄装置、云台装置等，还包括用于存储飞行指示应用程序的存储器，具体的，在本发明实施例中，所述飞行器包括：通信装置100和处理器200，其中，所述处理器200，调用所述存储器中的相关应用程序，用于通过所述通信装置100获取目标飞行区域的气象信息；根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；基于确定出的受限飞行参数对象发出飞行受限指示。
所述处理器200通过所述通信装置100连接到网络搜索目标飞行区域的气象信息，并可以通过所述通信装置100将受限飞行对象作为飞行受限指示发送给指定的用户终端。
进一步具体的，所述处理器200调用存储器中的应用程序，还可以用于判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
进一步可选地，所述处理器200在用于获取目标飞行区域的气象信息时，具体用于将飞行器当前所在区域或用户指定区域作为目标飞行区域；根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
进一步可选地，所述处理器200在用于根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，具体用于根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
进一步可选地，所述处理器200在用于根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，具体用于根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
进一步可选地，所述处理器200在用于基于确定出的受限飞行参数对象发出飞行受限指示时，具体用于显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
进一步可选地，所述处理器200在用于基于确定出的受限飞行参数对象发出飞行受限指示时，具体用于将所述受限飞行参数对象提供给用户选择；根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；发出所述飞行受限指示以控制所述飞行器受限飞行。
需要说明的是，本发明实施例中所述飞行器的所述处理器200的具体实现可对应地参考上述方法及装置相关内容的描述。
本发明实施例可基于获取的目标飞行区域的气象信息来确定受限飞行参数，以此作出飞行受限的指示，可以预先提醒用户或者直接控制无人机较为安全的执行在所述目标飞行区域的飞行任务，较好地保证了飞行器的飞行安全，且满足了飞行器用户对于气象信息的自动化、智能化的需求。
在本发明所提供的几个实施例中，应该理解到，所揭露的相关装置和方法，可以通过其它的方式实现。例如，以上所描述的装置实施例仅仅是示意性的，例如，所述模块或单元的划分，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，例如多个单元或组件可以结合或者可以集成到另一个***，或一些特征可以忽略，或不执行。另一点，所显示或讨论的相互之间的耦合或直接耦合或通信连接可以是通过一些接口，装置或单元的间接耦合或通信连接，可以是电性，机械或其它的形式。
所述作为分离部件说明的单元可以是或者也可以不是物理上分开的，作为单元显示的部件可以是或者也可以不是物理单元，即可以位于一个地方，或者也可以分布到多个网络单元上。可以根据实际的需要选择其中的部分或者全部单元来实现本实施例方案的目的。
另外，在本发明各个实施例中的各功能单元可以集成在一个处理单元中，也可以是各个单元单独物理存在，也可以两个或两个以上单元集成在一个单元中。上述集成的单元既可以采用硬件的形式实现，也可以采用软件功能单元的形式实现。
所述集成的单元如果以软件功能单元的形式实现并作为独立的产品销售或使用时，可以存储在一个计算机可读取存储介质中。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或者该技术方案的全部或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中，包括若干指令用以使得计算机处理器（processor）执行本发明各个实施例所述方法的全部或部分步骤。而前述的存储介质包括：U盘、移动硬盘、只读存储器（ROM，Read-Only Memory）、随机存取存储器（RAM，Random Access Memory）、磁碟或者光盘等各种可以存储程序代码的介质。
以上所述仅为本发明的实施例，并非因此限制本发明的专利范围，凡是利用本发明说明书及附图内容所作的等效结构或等效流程变换，或直接或间接运用在其他相关的技术领域，均同理包括在本发明的专利保护范围内。

Claims (18)

  1. 一种飞行指示方法，其特征在于，包括：
    获取目标飞行区域的气象信息；
    根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；
    基于确定出的受限飞行参数对象发出飞行受限指示。
  2. 如权利要求1所述的方法，其特征在于，所述获取目标飞行区域的气象信息，包括：
    将飞行器当前所在区域或用户指定区域作为目标飞行区域；
    根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；
    所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
  3. 如权利要求1所述的方法，其特征在于，所述根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，包括：
    根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；
    将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
  4. 如权利要求3所述的方法，其特征在于，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；
    所述根据预置的气象与飞行参数映射关系，查找与获取的气象信息关联的飞行参数，包括：
    分析确定出获取的气象信息的气象等级；
    基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。
  5. 如权利要求1所述的方法，其特征在于，所述根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象，包括：
    根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
  6. 如权利要求1所述的方法，其特征在于，还包括：
    判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；
    若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
  7. 如权利要求1所述的方法，其特征在于，所述基于确定出的受限飞行参数对象发出飞行受限指示，包括：
    显示所述确定出的受限飞行参数对象；或
    根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
  8. 如权利要求1所述的方法，其特征在于，所述基于确定出的受限飞行参数对象发出飞行受限指示，包括：
    将所述受限飞行参数对象提供给用户选择；
    根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；
    发出所述飞行受限指示以控制所述飞行器受限飞行。
  9. 如权利要求1所述的方法，其特征在于，所述确定出的受限飞行参数对象包括：飞行速度参数对象、飞行高度参数对象、飞行距离范围参数对象中的任一种或多种的组合。
  10. 一种飞行指示装置，其特征在于，包括：
    获取模块，用于获取目标飞行区域的气象信息；
    确定模块，用于根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；
    指示模块，用于基于确定出的受限飞行参数对象发出飞行受限指示。
  11. 如权利要求10所述的装置，其特征在于，所述获取模块包括：
    区域确定单元，用于将飞行器当前所在区域或用户指定区域作为目标飞行区域；
    网络单元，用于根据所述飞行器的气象参考信息，接入到网络中并搜索所述目标飞行区域的由所述气象参考信息所指示的气象信息；所述气象参考信息包括：指定的气象参考信息、或者基于飞行器的类型生成的气象参考信息。
  12. 如权利要求10所述的装置，其特征在于，所述确定模块包括：
    查找单元，用于根据预置的气象信息与飞行参数映射关系，查找与获取的气象信息关联的飞行参数；
    对象确定单元，用于将查找到的飞行参数确定为飞行器在所述目标飞行区域的受限飞行参数对象。
  13. 如权利要求12所述的装置，其特征在于，预置的气象信息与飞行参数映射关系中，包括气象及其等级信息与飞行参数映射关系；
    所述查找单元，具体用于分析确定出获取的气象信息的气象等级；基于气象信息及其等级在预置的气象与飞行参数映射关系中，查找关联的飞行参数。
  14. 如权利要求10所述的装置，其特征在于，
    所述确定模块，具体用于根据获取的各个气象信息作为模拟气象输入参数运行预置的模拟器，以确定出各个气候信息产生的模拟气象环境对模拟飞行器的飞行影响，进而确定出飞行器在所述目标飞行区域的受限飞行参数对象。
  15. 如权利要求10所述的装置，其特征在于，还包括：
    飞行处理模块，用于判断所述飞行器的飞行任务中，是否包括在所述目标飞行区域的飞行路径；若是，则根据所述气象信息对所述确定出的受限飞行参数对象进行修改更新，以使所述飞行器正常飞行。
  16. 如权利要求10所述的装置，其特征在于，
    所述指示模块，具体用于显示所述确定出的受限飞行参数对象；或根据所述确定出的受限飞行参数生成用于控制所述飞行器受限飞行的飞行受限指示，并发出所述飞行受限指示以控制所述飞行器受限飞行。
  17. 如权利要求10所述的装置，其特征在于，
    所述指示模块，具体用于将所述受限飞行参数对象提供给用户选择；根据对提供的所述受限飞行参数对象的选择操作，生成用于控制所述飞行器受限飞行的飞行受限指示；发出所述飞行受限指示以控制所述飞行器受限飞行。
  18. 一种飞行器，其特征在于，包括：通信装置和处理器，其中，所述处理器，用于通过所述通信装置获取目标飞行区域的气象信息；根据获取的气象信息确定出飞行器在所述目标飞行区域的受限飞行参数对象；基于确定出的受限飞行参数对象发出飞行受限指示。
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