A control method, device, storage medium and drone airport

Abstract

The present application proposes a control method, device, storage medium and drone airport of a UAV airport, wherein the UAV airport includes multiple independent cabins, each cabin maintains airflow, each cabin is provided with a temperature sensor, multiple temperature sensors obtain temperature information in their cabins and affect each other, when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors, the invalid temperature information is corrected according to the valid temperature information, and the drone airport is controlled according to the corrected temperature information; wherein the invalid temperature information is information with abnormal changes in the temperature information, and the valid temperature information is information with no abnormal changes in the temperature information. Without increasing the number of temperature sensors and without using expensive temperature sensors, the accuracy of temperature data is guaranteed, and the effect of reducing material costs is achieved.

Description

Technical Field

[0001] The present application relates to the field of temperature monitoring, and more specifically, to a control method, device, storage medium and unmanned aerial vehicle airport. Background Art

[0002] With the rapid development of the drone industry, the number of drones is increasing, and correspondingly, the number of drone airports is also increasing. Drone airports are used to park drones and replenish energy for drones. Drones will be parked inside drone airports for a long time. Therefore, it is necessary to monitor the status of drone airports, such as monitoring the internal temperature of drone airports, to avoid property losses caused by disasters in drone airports.

[0003] In the prior art, temperature sensors are usually used to monitor the temperature of drone airports. However, because temperature sensors may fail, the temperature information will be inaccurate, and even affect the mission execution of drone airports. In order to ensure the accuracy of temperature information, the number of sensors at a measurement point is usually increased or more expensive sensors are used to reduce the probability of failure. Both will lead to increased material costs.

[0004] Therefore, how to ensure the accuracy of temperature information while reducing material costs is a difficult problem that technicians in this field continue to pay attention to. Summary of the invention

[0005] The purpose of the present application is to provide a control method, device, storage medium and unmanned aerial vehicle airport, so as to at least partially improve the above-mentioned problems.

[0006] In order to achieve the above purpose, the technical solution adopted in the embodiment of the present application is as follows:

[0007] In a first aspect, an embodiment of the present application provides a control method for an unmanned aerial vehicle airport, which is applied to an unmanned aerial vehicle airport, wherein the unmanned aerial vehicle airport includes multiple independent cabins, each cabin maintains airflow, and each cabin is respectively provided with a temperature sensor, and the temperature information obtained by the multiple temperature sensors in the cabins affects each other. The method includes: when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors, the invalid temperature information is corrected according to the valid temperature information, and the unmanned aerial vehicle airport is controlled according to the corrected temperature information; wherein the invalid temperature information is information in which the temperature information changes abnormally, and the valid temperature information is information in which the temperature information changes normally.

[0008] In a second aspect, an embodiment of the present application provides a control device for an unmanned aerial vehicle airport applied to an unmanned aerial vehicle airport, wherein the unmanned aerial vehicle airport includes multiple independent cabins, each cabin maintains airflow, and each cabin is respectively provided with a temperature sensor, and the temperature information obtained by the multiple temperature sensors in the cabins influence each other, and the control device includes: a processing unit, which is used to correct the failed temperature information according to the valid temperature information when there is at least one failed temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors; a control unit, which is used to control the unmanned aerial vehicle airport according to the corrected temperature information; wherein the failed temperature information is information with abnormal changes in the temperature information, and the valid temperature information is information with no abnormal changes in the temperature information.

[0009] In a third aspect, an embodiment of the present application provides a storage medium on which a computer program is stored, and the computer program implements the above method when executed by a processor.

[0010] In a fourth aspect, an embodiment of the present application provides an unmanned aerial vehicle airport, comprising: a processor and a memory, wherein the memory is used to store one or more programs; when the one or more programs are executed by the processor, the above method is implemented.

[0011] Compared with the prior art, the control method, device, storage medium and drone airport provided by the embodiment of the present application include multiple independent cabins, each cabin maintains airflow, each cabin is provided with a temperature sensor, multiple temperature sensors obtain temperature information in the cabins and affect each other, when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors, the invalid temperature information is corrected according to the valid temperature information, and the drone airport is controlled according to the corrected temperature information; wherein the invalid temperature information is the information with abnormal changes in the temperature information, and the valid temperature information is the information with no abnormal changes in the temperature information. Without increasing the number of temperature sensors and without using expensive temperature sensors, the accuracy of temperature data is guaranteed, which has the effect of reducing material costs. And the continuity of the execution of the drone airport mission is guaranteed, avoiding the interruption of the drone airport mission execution process due to the lack of temperature data.

[0012] In order to make the above-mentioned objects, features and advantages of the present application more obvious and easy to understand, preferred embodiments are specifically cited below and described in detail with reference to the attached drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0014] Figure 1 A schematic diagram of the structure of a drone airport provided in an embodiment of the present application;

[0015] Figure 2 One of the structural schematic diagrams of the drone airport provided in the embodiment of the present application;

[0016] Figure 3 A schematic diagram of a flow chart of a method for controlling a drone airport provided in an embodiment of the present application;

[0017] Figure 4 One of the flow charts of the control method of the drone airport provided in the embodiment of the present application;

[0018] Figure 5 A schematic diagram of sub-steps of S102 provided in an embodiment of the present application;

[0019] Figure 6 One of the flow charts of the control method of the drone airport provided in the embodiment of the present application;

[0020] Figure 7 A schematic diagram of sub-steps of S104 provided in an embodiment of the present application;

[0021] Figure 8 One of the sub-step schematic diagrams of S104 provided in the embodiment of the present application;

[0022] Fig. 9 One of the structural schematic diagrams of the drone airport provided in the embodiment of the present application;

[0023] Fig.10 A unit schematic diagram of a control device for an unmanned aerial vehicle airport provided in an embodiment of the present application.

[0024] In the figure: 10 - processor; 11 - memory; 12 - bus; 13 - communication interface; 201 - processing unit; 202 - control unit. DETAILED DESCRIPTION

[0025] In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the technical solution in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various different configurations.

[0026] Therefore, the following detailed description of the embodiments of the present application provided in the accompanying drawings is not intended to limit the scope of the present application for which protection is sought, but merely represents selected embodiments of the present application. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in the field without creative work are within the scope of protection of the present application.

[0027] It should be noted that similar reference numerals and letters represent similar items in the following drawings, so once an item is defined in one drawing, it does not need to be further defined and explained in subsequent drawings. At the same time, in the description of this application, the terms "first", "second", etc. are only used to distinguish the description and cannot be understood as indicating or implying relative importance.

[0028] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0029] In the description of the present application, it should be noted that the terms "upper", "lower", "inside", "outside", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, or are the orientations or positional relationships in which the product of the application is usually placed when in use. They are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present application.

[0030] In the description of this application, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "disposed" and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two elements. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0031] In conjunction with the accompanying drawings, some embodiments of the present application are described in detail below. In the absence of conflict, the following embodiments and features in the embodiments can be combined with each other.

[0032] Temperature is an important detection index in the UAV field and is a necessary parameter to ensure the safe operation of UAVs. Figure 1 As shown, the drone airport includes multiple independent cabins, each cabin maintains airflow, and each cabin is respectively provided with a temperature sensor, and multiple temperature sensors obtain the temperature information in the cabins and influence each other. Optionally, the independent cabins are, for example, a first cabin (parking cabin), a second cabin (electrical cabin), and a third cabin (wiring cabin). The parking cabin, the electrical cabin, and the wiring cabin are all arranged in the drone airport. Multiple temperature sensors are, for example, a first temperature sensor T1, a second temperature sensor T2, and a third temperature sensor T3. The first temperature sensor T1 is used to collect the first temperature information of the parking cabin, the second temperature sensor T2 is used to collect the second temperature information of the electrical cabin, and the third temperature sensor T3 is used to collect the third temperature information of the wiring cabin.

[0033] The electrical compartment is used to install the main control panel, gateway, power supply and other electrical equipment of the drone airport. The parking compartment is used as the aircraft recovery parking position. The wiring compartment is used to install power cables and signal control and signal detection cables, various sensors connected to the main control panel and power cables of each compartment. Optionally, the drone airport also includes a high-voltage compartment where the 220V mains power is connected to place the air switch.

[0034] The temperature of the parking compartment, electrical compartment and wiring compartment needs to be measured inside the drone airport. In order to control the material cost of the temperature sensor, a temperature sensor is installed in each of the electrical compartment, the parking compartment and the wiring compartment, namely the first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3.

[0035] The first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3 are set in the air 3 cm away from the warehouse wall. The temperature data measured by the first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3 can be used to determine whether the drone is in an abnormal state when charging in the drone field, and whether it is the best temperature for drone battery storage. The drone field is controlled based on the obtained temperature information. The lack of any temperature data is an unsafe task execution. For example, if the temperature in the parking warehouse cannot be detected, it is impossible to determine whether it is the appropriate charging temperature and battery storage temperature during the charging process. Using the battery under inappropriate temperature conditions may bring great risks.

[0036] In one possible implementation, a smoke detection sensor can be added to the electrical compartment. A small weather station can be deployed outside the drone airport to measure the temperature, humidity, wind direction and wind speed around the drone airport. A small scheduling fan can be set at the air outlet at the bottom of the drone airport to blow air outward and generate a micro-motion airflow inside, so that airflow is maintained between the parking compartment, the electrical compartment and the wiring compartment. It should be noted that airflow is maintained between the parking compartment, the electrical compartment and the wiring compartment, so that there is a correlation between the temperatures of the three. The embodiment of the present application will use the correlation between the temperatures of the three to monitor the temperature information of the first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3, and correct it in time when failed data is found. Thereby, the possibility of data failure is reduced without increasing material costs, and the accuracy of the obtained temperature information is guaranteed.

[0037] Please refer to Figure 2 2 is a schematic diagram of the structure of another drone airport provided in an embodiment of the present application. Figure 2 As shown, the UAV airport includes a processor 10, a memory 11, and a bus 12. The processor 10 and the memory 11 are connected via the bus 12, and the processor 10 is used to execute executable modules stored in the memory 11, such as computer programs.

[0038] The processor 10 can be an integrated circuit chip with signal processing capabilities. In the implementation process, each step of the control method of the unmanned aerial vehicle airport can be completed by the hardware integrated logic circuit in the processor 10 or the instructions in the form of software. The above-mentioned processor 10 can be a general-purpose processor, including a central processing unit (CPU), a network processor (NP), etc.; it can also be a digital signal processor (DSP), an application specific integrated circuit (ASIC), a field programmable gate array (FPGA) or other programmable logic devices, discrete gates or transistor logic devices, discrete hardware components.

[0039] The memory 11 may include a high-speed random access memory (RAM), and may also include a non-volatile memory, such as at least one disk memory.

[0040] The bus 12 may be an ISA (Industry Standard Architecture) bus, a PCI (Peripheral Component Interconnect) bus, or an EISA (Extended Industry Standard Architecture) bus. Figure 2 Although only one bidirectional arrow is used in the diagram, it does not mean that there is only one bus 12 or only one type of bus 12 .

[0041] The memory 11 is used to store programs, such as programs corresponding to the control device of the drone airport. The control device of the drone airport includes at least one software function module that can be stored in the memory 11 in the form of software or firmware or fixed in the operating system (OS) of the drone airport. After receiving the execution instruction, the processor 10 executes the program to implement the control method of the drone airport.

[0042] Possibly, the drone airport provided in the embodiment of the present application further includes a communication interface 13. The communication interface 13 is connected to the processor 10 via a bus. The drone airport can communicate with other terminals, such as drones, via the communication interface 13.

[0043] In a possible implementation, the processor 10 is in communication connection with the first temperature sensor T1 , the second temperature sensor T2 , and the third temperature sensor T3 , and the processor 10 can obtain temperature information of the first temperature sensor T1 , the second temperature sensor T2 , and the third temperature sensor T3 .

[0044] It should be understood that Figure 1 and Figure 2 The structure shown is only a schematic diagram of the structure of a portion of the drone airport. The drone airport may also include Figure 1 and Figure 2 More or fewer components as shown, or with Figure 1 and Figure 2 Different configurations shown. Figure 1 and Figure 2 Each component shown in the figure can be implemented by hardware, software or a combination thereof.

[0045] The control method of the drone airport provided in the embodiment of the present application can be applied to but not limited to Figure 1 and Figure 2 For the specific process of the drone airport shown, please refer to Figure 3 , the control method of the UAV airport includes: S104 and S105, which are specifically described as follows.

[0046] S104: when there is at least one piece of failed temperature information and at least one piece of valid temperature information in the temperature information obtained by the plurality of temperature sensors, modify the failed temperature information according to the valid temperature information.

[0047] The invalid temperature information is the information in which the temperature information changes abnormally, and the valid temperature information is the information in which the temperature information changes normally.

[0048] It should be understood that when the temperature information obtained by multiple temperature sensors is all valid temperature information, no correction is required, and the UAV airport is directly controlled based on the valid temperature information. When the temperature information obtained by multiple temperature sensors is all invalid temperature information, the temperature information obtained by multiple temperature sensors cannot be used as reference information for correction, and S104 does not need to be executed at this time. When there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by multiple temperature sensors, for example, the first temperature information is invalid temperature information, and the second temperature information and the third temperature information are both valid temperature information, the invalid temperature information can be corrected based on the valid temperature information, that is, S104 is executed.

[0049] In a possible implementation, after long-term simulation of outdoor environment and simulation test of temperature box, the data of temperature sensors in each cabin inside the drone airport and the ambient temperature data are collected for data analysis, and a mathematical model of the relationship between the temperatures of each cabin can be established. The mathematical model of the relationship is used to fuse the temperature sensor data. Therefore, when one or two temperature sensors fail, resulting in one or two temperature information being invalid temperature information, corrections can be made based on the valid temperature information and the corresponding mathematical module of the relationship to obtain the corrected valid temperature information.

[0050] S105, controlling the UAV airport according to the corrected temperature information.

[0051] Optionally, the control content is, for example, charging the drones parked at the drone airport and adjusting the temperature in the drone airport to keep the temperature at an optimal temperature for preserving the batteries.

[0052] In summary, the embodiment of the present application provides a control method for an unmanned aerial vehicle airport, which is applied to an unmanned aerial vehicle airport. The unmanned aerial vehicle airport includes multiple independent cabins, each cabin maintains airflow, and each cabin is provided with a temperature sensor. The temperature information obtained by the multiple temperature sensors affects each other. When there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors, the invalid temperature information is corrected according to the valid temperature information, and the unmanned aerial vehicle airport is controlled according to the corrected temperature information; wherein the invalid temperature information is the information with abnormal changes in the temperature information, and the valid temperature information is the information with no abnormal changes in the temperature information. Without increasing the number of temperature sensors and without using expensive temperature sensors, the accuracy of the temperature data is guaranteed, which has the effect of reducing material costs. In addition, the continuity of the execution of the unmanned aerial vehicle airport tasks is guaranteed, and the interruption of the task execution process of the unmanned aerial vehicle airport due to the lack of temperature data is avoided.

[0053] exist Figure 3 Based on how to determine the failure temperature information and the effective temperature information, the embodiment of the present application also provides a possible implementation method, please refer to Figure 4 Before S104, the control method of the UAV airport also includes: S101 and S102, which are described in detail as follows.

[0054] S101, obtaining current change slopes corresponding to temperature information of multiple temperature sensors.

[0055] Continuing with the example that the three independent cabins in the drone airport are respectively equipped with the first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3, the first temperature sensor T1, the second temperature sensor T2 and the third temperature sensor T3 correspond to the first temperature information, the second temperature information and the third temperature information respectively. That is, the current change slope corresponding to the first temperature information, the second temperature information and the third temperature information is obtained.

[0056] The current change slope may be a change range of the temperature information detected by the temperature sensor within a unit time length.

[0057] S102, determining failure temperature information and valid temperature information according to current change slopes corresponding to temperature information of a plurality of temperature sensors.

[0058] The first temperature sensor T1, the second temperature sensor T2, and the third temperature sensor T3 in the embodiment of the present application can be conventional NTC temperature sensors with an effective measurement range of -30°C to 100°C. The resistance of the temperature measuring resistor in the temperature sensor has a one-to-one correspondence with its temperature. In the event of failure of the temperature measuring resistor, the detected value of the resistor may have a maximum or minimum value. During the service life cycle of the temperature sensor design, if the physical structure of the temperature sensor (such as the temperature measuring resistor therein) is destroyed, the detected value of the temperature measuring resistor may jump instantaneously, that is, the slope of its change is very large.

[0059] By using the above characteristics, the current change slopes corresponding to the first temperature information, the second temperature information and the third temperature information can be obtained, so as to determine whether the first temperature information, the second temperature information and the third temperature information are invalid temperature information.

[0060] exist Figure 4 Based on the content in S102, the present application embodiment also provides a possible implementation method, please refer to Figure 5 , S102 includes S102-1 to S102-4, which are described in detail as follows.

[0061] S102-1, determine whether the current change slope is greater than the first slope threshold. If yes, execute S102-2; if no, execute S102-4.

[0062] It should be understood that when the temperature sensor is working normally, the temperature information it detects changes continuously, and the change trend is relatively stable. If the temperature information detected by the temperature sensor rises or falls by more than 20°C from a time point in a relatively stable state to a time point in which a temperature maximum occurs, it means that the current change slope corresponding to the temperature sensor is greater than the first slope threshold. The temperature information detected by the temperature sensor may be invalid temperature information and requires further verification, that is, execute S102-2. On the contrary, when the current change slopes corresponding to the temperature information detected by multiple temperature sensors are less than or equal to the first slope threshold, it means that there is no abnormality in the change trend of the temperature information detected by multiple temperature sensors, and S102-4 can be executed to temporarily determine that all temperature information is valid temperature information.

[0063] S102-2, determine whether the current change slope is less than the second slope threshold. If yes, execute S102-3; if no, execute S102-4.

[0064] The second slope threshold is smaller than the first slope threshold.

[0065] In a possible implementation, for example, a disaster (fire) occurs, and the temperature information monitored by the temperature sensor may suddenly change, that is, the current change slope corresponding to the temperature information is greater than the first slope threshold. At this time, directly identifying the temperature information as invalid temperature information will not only fail to obtain accurate temperature information, but also lead to inaccurate identification results of the disaster, affect disaster relief, and cause unnecessary property losses.

[0066] In order to overcome the above problem, when the current change slope is greater than the first slope threshold, it is necessary to execute S102-2 to determine whether the current change slope is less than the second slope threshold.

[0067] Because there is airflow between the multiple cabins in the drone airport, the temperatures between the cabins are correlated. When a fire occurs in one cabin, causing the temperature inside to change dramatically, the temperatures in other cabins will also be affected and change. Of course, the temperature changes in other cabins may lag behind.

[0068] When there is no current change slope less than the second slope threshold, that is, the current change slopes of all temperature information are greater than the second slope threshold, it means that the temperatures in other warehouses are also changing, and the change amplitude is large. At this time, a disaster may have occurred rather than a temperature sensor failure, and S102-4 can be executed; when there is a current change slope less than the second slope threshold, it means that the temperature change trend in at least one warehouse is slow, for example, the change within a unit time length is less than 2°C, and no disaster has occurred. At this time, the temperature information corresponding to the current change slope greater than the first slope threshold can be determined as failed temperature information, and the temperature information corresponding to the current change slope less than the second slope threshold can be determined as valid temperature information, that is, S102-3 is executed.

[0069] S102-3, determining the temperature information corresponding to a current change slope greater than a first slope threshold as invalid temperature information, and determining the temperature information corresponding to a current change slope less than a second slope threshold as valid temperature information.

[0070] S102-4, temporarily determine that all temperature information is valid temperature information.

[0071] It should be understood that there is another possible situation, when the current change slope of all temperature information is greater than the first slope threshold, that is, when there is no temperature information whose current change slope is less than the second slope threshold, it may be that all temperature sensors are faulty and all temperature information is invalid temperature information. For how to identify this situation, the embodiment of the present application also provides a possible implementation method, please refer to Figure 6 The control method of the UAV airport also includes S103 and S106, which are described in detail as follows.

[0072] S103, determining whether the temperature information obtained by the multiple temperature sensors is all invalid temperature information. If yes, execute S106; if no, execute S104.

[0073] Optionally, after S102-2, when it is determined that there is no current change slope less than the second slope threshold, S102-4 is executed at this time. After S102-4, the validity of the temperature information is further verified. S103 is executed, for example, to determine whether the current smoke concentration information is greater than the concentration threshold. If so, it means that a fire may have occurred, and it is normal for the temperature to suddenly change at this time, then all temperature information is determined as valid temperature information. If not, it means that no fire has occurred, and it is abnormal for the temperature to suddenly change at this time, then all temperature information is determined as invalid temperature information.

[0074] It should be understood that the current change slopes of the multiple temperature information need to be obtained before S103. In a possible implementation, it is also possible to determine whether the current change slopes of the multiple temperature information are all invalid temperature information in combination with the current change slopes of the multiple temperature information and the external environment temperature.

[0075] S106, controlling the UAV airport to issue an abnormal alarm.

[0076] It should be understood that when the temperature sensors installed in multiple compartments in the drone airport all fail and the measured temperature information is invalid, it will affect the normal function execution of the drone airport and an abnormal alarm will be required to prompt the staff to maintain the equipment.

[0077] Please continue to refer to Figure 1 In a possible implementation, the independent cabin includes a first cabin, a second cabin and a third cabin, and the second cabin is arranged between the first cabin and the third cabin.

[0078] On this basis, when the temperature information obtained by the temperature sensor in the first compartment or the third compartment is failure temperature information, for the content in S104, the embodiment of the present application also provides a possible implementation method, please refer to Figure 7 , S104 includes S104-1 and S104-2, which are described in detail as follows.

[0079] S104-1, bringing the temperature information obtained by the temperature sensor in the second chamber into the first function to obtain first corrected temperature information.

[0080] S104-2, replacing the failure temperature information with the first corrected temperature information to complete the correction of the failure temperature information.

[0081] Optionally, the second compartment (electrical compartment) is arranged between the first compartment (shutdown compartment) and the third compartment (wiring compartment); based on the central principle, the temperature information collected by adjacent temperature sensors has a higher correlation, and when the temperature sensor arranged in the middle (the temperature sensor in the second compartment) is valid temperature information, the temperature information of the temperature sensor in the second compartment is selected to correct the failure temperature.

[0082] When the temperature sensor in the middle (the temperature sensor in the second compartment) has invalid temperature information, the temperature information of the temperature sensor in the second compartment is selected to correct the invalid temperature. Then any valid temperature information is selected to correct the temperature information of the temperature sensor in the second compartment.

[0083] When only one of the temperature information obtained by the temperature sensors in the first compartment, the second compartment, and the third compartment is valid temperature information, the present application embodiment further provides a possible implementation method for the content in S104, please refer to Figure 8 , S104 includes S104-3 to S104-7, which are described in detail as follows.

[0084] S104-3, determine whether the effective temperature information is less than the first temperature threshold. If yes, execute S104-6; if no, execute S104-4.

[0085] It should be understood that when the temperature values ​​of the cabins corresponding to the effective temperature information are different, the temperature impacts on the adjacent cabins are different. When the temperature is higher, the temperature impact on the adjacent cabins is greater. Therefore, it is necessary to determine whether the effective temperature information is less than the first temperature threshold. Optionally, the value of the first temperature threshold can be 40 degrees.

[0086] S104-4, when the effective temperature information is greater than or equal to the first temperature threshold, the effective temperature information is brought into the second function and the third function to obtain second corrected temperature information and third corrected temperature information.

[0087] S104-5, replacing the two pieces of failure temperature information with the second corrected temperature information and the third corrected temperature information, to complete the correction of the failure temperature information.

[0088] S104-6, when the effective temperature information is less than the first temperature threshold, the effective temperature information is brought into the fourth function and the fifth function to obtain the fourth corrected temperature information and the fifth corrected temperature information. S104-7, the two invalid temperature information are replaced with the fourth corrected temperature information and the fifth corrected temperature information to complete the correction of the invalid temperature information.

[0089] Optionally, the second function and the fourth function are used to correct the temperature information of the same faulty temperature sensor, and the third function and the fifth function are used to correct the temperature information of the same faulty temperature sensor.

[0090] The first parameter in the second function is greater than the first parameter in the fourth function, the second parameter in the second function is greater than the second parameter in the fourth function, the first parameter in the third function is greater than the first parameter in the fifth function, and the second parameter in the third function is greater than the second parameter in the fifth function.

[0091] Optionally, the expressions of the first to fifth functions in the embodiment of the present application are as follows:

[0092] Tempout = a*Temp-b;

[0093] Among them, Tempout represents the corrected temperature information, Temp represents the effective temperature information, a is a preset first parameter, b is a preset second parameter, and the values ​​of a and b in different functions are not exactly the same.

[0094] In one possible implementation, when the ambient temperature is greater than 50 degrees Celsius, when the current change slope of the temperature information is greater than the first slope threshold, that is, the upward trend is abnormal, data correction is not required and disaster judgment and environmental monitoring can be performed directly based on the corresponding temperature information.

[0095] Regarding the distribution of parking bays, electrical bays, and wiring bays in the drone airport, the present application embodiment also provides a possible implementation method, please refer to Fig. 9 For example, vents are provided between the bins to facilitate air flow.

[0096] See also Fig.10 , Fig.10 A control device for an unmanned aerial vehicle airport is provided in an embodiment of the present application. Optionally, the control device for an unmanned aerial vehicle airport is applied to the unmanned aerial vehicle airport described above.

[0097] The control device of the drone airport includes: a processing unit 201 and a control unit 202 .

[0098] The processing unit 201 is configured to correct the invalid temperature information according to the valid temperature information when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the multiple temperature sensors;

[0099] A control unit 202, configured to control the UAV airport according to the corrected temperature information;

[0100] The invalid temperature information is the information in which the temperature information changes abnormally, and the valid temperature information is the information in which the temperature information changes normally.

[0101] Optionally, the processing unit 201 may execute the above-mentioned S101 to S104 and S106, and the control unit 202 may execute the above-mentioned S105.

[0102] It should be noted that the control device for the drone airport provided in this embodiment can execute the method flow shown in the above method flow embodiment to achieve the corresponding technical effect. For the sake of brief description, for parts not mentioned in this embodiment, please refer to the corresponding content in the above embodiment.

[0103] The present application also provides a storage medium storing computer instructions and programs, which, when read and executed, execute the control method of the drone airport in the above embodiment. The storage medium may include memory, flash memory, register, or a combination thereof.

[0104] The following provides a drone field, a drone field such as Figure 1 and Figure 2 As shown, the control method of the drone airport described above can be implemented; specifically, the drone airport includes: a processor 10, a memory 11, and a bus 12. The processor 10 can be a CPU. The memory 11 is used to store one or more programs. When the one or more programs are executed by the processor 10, the control method of the drone airport described above is executed.

[0105] In the embodiments provided in the present application, it should be understood that the disclosed devices and methods can also be implemented in other ways. The device embodiments described above are merely schematic. For example, the flowcharts and block diagrams in the accompanying drawings show the possible architecture, functions and operations of the devices, methods and computer program products according to the multiple embodiments of the present application. In this regard, each box in the flowchart or block diagram can represent a module, a program segment or a part of a code, and the module, a program segment or a part of a code contains one or more executable instructions for implementing the specified logical function. It should also be noted that in some alternative implementations, the functions marked in the box can also occur in a different order from the order marked in the accompanying drawings. For example, two consecutive boxes can actually be executed substantially in parallel, and they can sometimes be executed in the opposite order, depending on the functions involved. It should also be noted that each box in the block diagram and / or the flowchart, and the combination of boxes in the block diagram and / or the flowchart can be implemented with a dedicated hardware-based system that performs a specified function or action, or can be implemented with a combination of dedicated hardware and computer instructions.

[0106] In addition, the functional modules in the various embodiments of the present application may be integrated together to form an independent part, or each module may exist separately, or two or more modules may be integrated to form an independent part.

[0107] If the functions are implemented in the form of software function modules and sold or used as independent products, they can be stored in a computer-readable storage medium. Based on this understanding, the technical solution of the present application can be essentially or partly embodied in the form of a software product that contributes to the prior art. The computer software product is stored in a storage medium, including several instructions to enable a computer device (which can be a personal computer, a server, or a network device, etc.) to perform all or part of the steps of the methods described in each embodiment of the present application. The aforementioned storage medium includes: various media that can store program codes, such as a USB flash drive, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk or an optical disk.

[0108] The above description is only the preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

[0109] It will be apparent to those skilled in the art that the present application is not limited to the details of the exemplary embodiments described above, and that the present application can be implemented in other specific forms without departing from the spirit or essential features of the present application. Therefore, the embodiments should be considered exemplary and non-limiting in all respects, and the scope of the present application is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present application. Any reference numeral in a claim should not be considered as limiting the claim to which it relates.

Claims

1. A method for controlling a drone airport, characterized in that: Applied to a drone airport, the drone airport includes multiple independent cabins, each cabin maintains airflow, each cabin is respectively provided with a temperature sensor, and multiple temperature sensors obtain temperature information in their cabins and affect each other. The method includes: Acquire current change slopes corresponding to the temperature information of the plurality of temperature sensors; Determine whether there is a current change slope greater than a first slope threshold; If there is a current change slope greater than the first slope threshold, determine whether there is a current change slope less than the second slope threshold, wherein the second slope threshold is less than the first slope threshold; If there is a current change slope that is less than the second slope threshold, the temperature information corresponding to the current change slope being greater than the first slope threshold is determined as invalid temperature information, and the temperature information corresponding to the current change slope being less than the second slope threshold is determined as valid temperature information; When there is no current change slope greater than the first slope threshold, or when there is no current change slope less than the second slope threshold, all temperature information is temporarily determined to be valid temperature information; When there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the plurality of temperature sensors, the invalid temperature information is corrected according to the valid temperature information, and the UAV airport is controlled according to the corrected temperature information; The invalid temperature information is the information of abnormal change in the temperature information, and the valid temperature information is the information of normal change in the temperature information.

2. The control method of the drone airport according to claim 1, characterized in that: Before correcting the failure temperature information according to the effective temperature information, the method further includes: Determining whether the temperature information obtained by the plurality of temperature sensors is all failure temperature information; If yes, the drone airport is controlled to issue an abnormal alarm; If not, when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the plurality of temperature sensors, the invalid temperature information is corrected according to the valid temperature information.

3. The control method of the drone airport according to claim 2, characterized in that: The independent cabins include a first cabin, a second cabin and a third cabin, and the second cabin is arranged between the first cabin and the third cabin.

4. The control method of the UAV airport as claimed in claim 3, characterized in that: When the temperature information obtained by the temperature sensor in the first compartment or the third compartment is invalid temperature information, the step of correcting the invalid temperature information according to the valid temperature information comprises: Substituting the temperature information obtained by the temperature sensor in the second chamber into the first function to obtain first corrected temperature information; The failure temperature information is replaced with the first corrected temperature information to complete the correction of the failure temperature information.

5. The method for controlling a drone airport according to claim 3, characterized in that: When only one of the temperature information obtained by the temperature sensors in the first compartment, the second compartment, and the third compartment is valid temperature information, the step of correcting the invalid temperature information according to the valid temperature information comprises: When the effective temperature information is greater than or equal to the first temperature threshold, the effective temperature information is brought into the second function and the third function to obtain the second corrected temperature information and the third corrected temperature information; replacing two pieces of failure temperature information with the second corrected temperature information and the third corrected temperature information, respectively, to complete the correction of the failure temperature information; When the effective temperature information is less than the first temperature threshold, the effective temperature information is substituted into the fourth function and the fifth function to obtain fourth corrected temperature information and fifth corrected temperature information; The two failure temperature information are replaced by the fourth corrected temperature information and the fifth corrected temperature information to complete the correction of the failure temperature information.

6. A control device for a drone airport, characterized in that: Applied to a drone airport, the drone airport includes multiple independent cabins, each cabin maintains airflow, each cabin is respectively provided with a temperature sensor, and multiple temperature sensors obtain temperature information in the cabins and affect each other. The control device includes: A processing unit, used to obtain current change slopes corresponding to the temperature information of the plurality of temperature sensors; determine whether there is a current change slope greater than a first slope threshold; if there is a current change slope greater than the first slope threshold, determine whether there is a current change slope less than a second slope threshold, wherein the second slope threshold is less than the first slope threshold; if there is a current change slope less than the second slope threshold, determine the temperature information corresponding to the current change slope greater than the first slope threshold as invalid temperature information, and determine the temperature information corresponding to the current change slope less than the second slope threshold as valid temperature information; when there is no current change slope greater than the first slope threshold, or when there is no current change slope less than the second slope threshold, provisionally determine that all temperature information is valid temperature information; when there is at least one invalid temperature information and at least one valid temperature information in the temperature information obtained by the plurality of temperature sensors, modify the invalid temperature information according to the valid temperature information; A control unit, used for controlling the UAV airport according to the corrected temperature information; The invalid temperature information is the information of abnormal change in the temperature information, and the valid temperature information is the information of normal change in the temperature information.

7. A computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, the method according to any one of claims 1 to 5 is implemented.

8. A drone airport, characterized in that: include: A processor and a memory, the memory being used to store one or more programs; When the one or more programs are executed by the processor, the method according to any one of claims 1 to 5 is implemented.

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