Air conditioner adjusting method and device without external temperature sensor and hovercar

Abstract

The invention relates to the technical field of air conditioners of hovercars, and discloses an air conditioner adjusting method and device without an external temperature sensor and a hovercar. Comprising at least one of vehicle exterior temperature data collected by a land moving body, altitude difference of flying of the flying body and weather forecast information, determining a vehicle exterior temperature evaluation value corresponding to the flying body based on to-be-evaluated data, performing corresponding air conditioning based on the vehicle exterior temperature evaluation value, and controlling the air conditioning of the flying body under the condition that a flying body environment temperature sensor is canceled. The environment temperature can be estimated through an algorithm to achieve automatic control of an air conditioner, and weight reduction and cost reduction of a flying body are achieved.

Description

Technical Field

[0001] The present invention relates to the technical field of air conditioning for flying cars, and in particular to an air conditioning adjustment method and device without an external temperature sensor, and a flying car. Background Art

[0002] In traditional automobile air-conditioning systems, the outdoor temperature sensor is an important component for obtaining the external ambient temperature. The control of automatic air conditioning must be based on the ambient temperature, so traditional cars equipped with automatic air conditioning will be equipped with outdoor temperature sensors. However, for the special structure of flying cars, which are divided into two parts, the land body and the flying body, if an outdoor temperature sensor is installed separately for the flying body, it will not only increase the cost and weight, but may also cause sensor failure or inaccurate measurement due to the complex flight environment. Summary of the invention

[0003] In view of this, the present invention provides an air conditioning adjustment method, device and flying car without an outdoor temperature sensor, so as to solve the problem that installing an outdoor temperature sensor separately for a flying body not only increases the cost and weight, but also may cause sensor failure or inaccurate measurement due to the complex flight environment.

[0004] In a first aspect, the present invention provides an air conditioning adjustment method without an outdoor temperature sensor, which is applied to a flying body in a flying car, wherein the flying body establishes a communication connection with a land body in the flying car, and the method comprises: obtaining data to be evaluated for evaluating the outdoor temperature of the flying body, wherein the data to be evaluated comprises at least one of outdoor temperature data collected by the land body, an altitude difference of the flying body, and weather forecast information; based on the data to be evaluated, determining an outdoor temperature evaluation value corresponding to the flying body, and performing corresponding air conditioning adjustment based on the outdoor temperature evaluation value.

[0005] The air conditioning adjustment method without an outdoor temperature sensor provided by the present invention obtains data to be evaluated for the user to evaluate the outdoor temperature of the flying body, including at least one of the outdoor temperature data collected by the land body, the altitude difference of the flying body, and weather forecast information, and then determines the outdoor temperature evaluation value corresponding to the flying body based on the data to be evaluated, and performs corresponding air conditioning based on the outdoor temperature evaluation value. In the case of eliminating the ambient temperature sensor of the flying body, the ambient temperature can be estimated by an algorithm to realize automatic control of the air conditioning, thereby achieving weight reduction and cost reduction of the flying body.

[0006] In an optional embodiment, the weather forecast information includes at least the weather forecast temperature, and determining the outdoor temperature evaluation value corresponding to the flying body based on the data to be evaluated includes: determining the corresponding temperature values ​​to be evaluated based on the outdoor temperature data, the altitude difference of the flying body, and preset temperature coefficients corresponding to the weather forecast temperature; calculating the outdoor temperature evaluation value corresponding to the flying body based on the outdoor temperature data, the altitude difference of the flying body, and the temperature values ​​to be evaluated corresponding to the weather forecast temperature.

[0007] The present invention sets the corresponding temperature coefficient according to the influence of the outdoor temperature data, the altitude difference of the flying body and the weather forecast temperature waiting evaluation data on the outdoor temperature of the flying body, and then calculates the outdoor temperature evaluation value based on the temperature coefficient and the data to be evaluated, thereby improving the accuracy of the outdoor temperature evaluation.

[0008] In an optional embodiment, the preset temperature coefficients corresponding to the outdoor temperature data and the weather forecast temperature are the first temperature coefficient and the second temperature coefficient, respectively, and the first temperature coefficient and the second temperature coefficient are obtained by the following temperature coefficient determination steps: obtaining the length of time that the land body is in a power-off state after the land body and the flying body are separated; obtaining the positioning distance between the flying body and the land body; determining the first temperature coefficient based on the length of time that the land body is in the power-off state and the positioning distance between the flying body and the land body; determining the second temperature coefficient by subtracting the first temperature coefficient from the sum of the preset temperature coefficients, and the sum of the preset temperature coefficients is the sum of the first temperature coefficient and the second temperature coefficient.

[0009] The present invention determines the first temperature coefficient based on the length of time the land body is in the power-off state and the positioning distance between the flying body and the land body, thereby achieving the credibility of determining the land body temperature based on the real-time distance relationship between the land body and the flying body, and improving the accuracy of calculating the external temperature of the flying body.

[0010] In an optional embodiment, the first temperature coefficient is determined based on the duration that the terrestrial body is in the power-off state and the positioning distance between the flying body and the terrestrial body, including: dividing the duration that the terrestrial body is in the power-off state by a preset duration threshold to obtain a first ratio, and then subtracting the first ratio from a preset standard value to obtain a first coefficient; dividing the positioning distance between the flying body and the terrestrial body by a preset distance threshold to obtain a second ratio, and then subtracting the second ratio from the preset standard value to obtain a second coefficient; multiplying the first coefficient and the second coefficient to obtain the first temperature coefficient.

[0011] In an optional embodiment, the first temperature coefficient is determined based on the duration of time the terrestrial body is in the power-off state and the positioning distance between the flying body and the terrestrial body, comprising: when a preset condition is not met, the first temperature coefficient is determined based on the duration of time the terrestrial body is in the power-off state and the positioning distance between the flying body and the terrestrial body; the temperature coefficient determination step also includes: when the preset condition is met, determining zero or the sum of the preset temperature coefficients as the first temperature coefficient.

[0012] In an optional embodiment, when a preset condition is met, zero or a preset temperature coefficient and a preset temperature coefficient are determined as the first temperature coefficient, including: when the first preset condition is met, zero is determined as the first temperature coefficient, and the first preset condition is that the acquired outdoor temperature data is not within a preset first normal range, and / or, outdoor temperature sensor failure prompt information transmitted by the land vehicle is received.

[0013] When the present invention determines that the land vehicle ambient temperature sensor fails, the corresponding first temperature coefficient is set to zero, thereby preventing abnormal land vehicle external temperature data from affecting the accuracy of evaluating the flying vehicle external temperature.

[0014] In an optional embodiment, when a preset condition is met, determining the sum of zero or preset temperature coefficients as the first temperature coefficient includes: when a second preset condition is met, determining the sum of preset temperature coefficients as the first temperature coefficient, wherein the second preset condition is that the obtained weather temperature is not within a preset second normal temperature range or the weather forecast temperature is not obtained.

[0015] When the present invention determines that the weather forecast interface module fails, the corresponding second temperature coefficient is set to zero, which can prevent the abnormal weather forecast temperature from affecting the accuracy of evaluating the external temperature of the flying body.

[0016] In a second aspect, the present invention provides an air conditioning control device without an outdoor temperature sensor, which is applied to a flying body in a flying car, and the flying body establishes a communication connection with a land body in the flying car. The device includes: a data acquisition module, used to obtain data to be evaluated for evaluating the outdoor temperature of the flying body, and the data to be evaluated includes at least one of the outdoor temperature data collected by the land body, the altitude difference of the flying body, and weather forecast information; a temperature evaluation module, used to determine the outdoor temperature evaluation value corresponding to the flying body based on the data to be evaluated, and perform corresponding air conditioning adjustment based on the outdoor temperature evaluation value.

[0017] In a third aspect, the present invention provides a flying car, comprising a flying body and a land body, wherein the flying body establishes a communication connection with the land body, the flying body comprises a controller, the controller comprises a memory and a processor, the memory and the processor are communicatively connected with each other, computer instructions are stored in the memory, and the processor executes the air conditioning adjustment method without an outdoor temperature sensor according to the above-mentioned first aspect or any corresponding embodiment thereof by executing the computer instructions.

[0018] In a fourth aspect, the present invention provides a computer-readable storage medium having computer instructions stored thereon, the computer instructions being used to enable a computer to execute the air conditioning adjustment method without an outdoor temperature sensor of the above-mentioned first aspect or any corresponding embodiment thereof. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the specific implementation methods of the present invention or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0020] Figure 1 is a flow chart of an air conditioning adjustment method without an external temperature sensor according to an embodiment of the present invention;

[0021] Figure 2 is a flow chart of another air conditioning adjustment method without an external temperature sensor according to an embodiment of the present invention;

[0022] Figure 3 is a structural block diagram of a flying car according to an embodiment of the present invention;

[0023] Figure 4 is a structural block diagram of a flying body and a land body in a flying car according to an embodiment of the present invention;

[0024] Figure 5 is a structural block diagram of an air conditioning regulating device without an external temperature sensor according to an embodiment of the present invention;

[0025] Figure 6 It is a schematic diagram of the hardware structure of a computer device according to an embodiment of the present invention. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical solution and advantages of the embodiments of the present invention clearer, the technical solution in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative work are within the scope of protection of the present invention.

[0027] In traditional automobile air conditioning systems, the outside temperature sensor is an important component for obtaining the external ambient temperature. The control of automatic air conditioning must be based on the ambient temperature, so traditional cars equipped with automatic air conditioning will be equipped with an outside temperature sensor. However, in the special structure of the flying car, if an outside temperature sensor is installed separately for the flying body, it will not only increase the cost and weight, but may also cause sensor failure or inaccurate measurement due to the complex flight environment.

[0028] The related automobile air-conditioning technology that eliminates the outdoor temperature sensor is to build a base station every 1 to 2 square kilometers in each region in advance to collect the temperature and wirelessly transmit the temperature to the car. However, this method requires the construction of a large number of dense base stations, and the investment cost is huge.

[0029] According to an embodiment of the present invention, an embodiment of an air conditioning adjustment method without an outdoor temperature sensor is provided. It should be noted that the steps shown in the flowchart of the accompanying drawings can be executed in a computer system such as a set of computer executable instructions, and although a logical order is shown in the flowchart, in some cases, the steps shown or described can be executed in an order different from that shown here.

[0030] In this embodiment, an air conditioning adjustment method without an external temperature sensor is provided, which can be used for a flying body in a flying car, and the flying body establishes a communication connection with a land body in the flying car. The flying car targeted by the present invention has a unique structure, which is divided into two parts: a land body and a flying body. Figure 1 is a flow chart of an air conditioning adjustment method without an external temperature sensor according to an embodiment of the present invention. Figure 1 As shown, the process includes the following steps:

[0031] Step S101, obtaining data to be evaluated for evaluating the external temperature of the flying body, wherein the data to be evaluated includes at least one of external temperature data collected by the terrestrial body, the altitude difference of the flying body, and weather forecast information.

[0032] The flying body in the embodiment of the present invention can obtain the data to be evaluated for evaluating the outdoor temperature of the flying body through the land body and other methods. The data to be evaluated may include but is not limited to the outdoor temperature data T1 collected by the land body, and is transmitted to the flying body by wireless. The flying body obtains the real-time weather forecast information of the current area and at least one of the altitude difference of the flying body through the weather forecast interface module according to the GPS positioning and time. Among them, the corresponding data to be evaluated can be determined according to the actual acquisition result of the flying body. For example, the flying body can simultaneously perform the acquisition operations of the above three types of data to be evaluated to obtain three types of data to be evaluated, but the weather forecast interface module may fail, resulting in the inability to obtain weather forecast information, or the wireless communication with the land body may be disconnected or the ambient temperature sensor of the land body may fail, resulting in the inability to receive the outdoor temperature data collected by the land body. Therefore, the data actually obtained by the flying body can be used to evaluate the outdoor temperature of the flying body, just as an example.

[0033] Step S102: determining an external temperature evaluation value corresponding to the flying object based on the data to be evaluated, and performing corresponding air conditioning adjustment based on the external temperature evaluation value.

[0034] The weather forecast information obtained by the embodiment of the present invention may include but is not limited to the weather forecast temperature T2 and weather conditions. The weather conditions may affect the coefficient of temperature evaluation. The outdoor temperature evaluation value corresponding to the flying body may be determined based on the data to be evaluated obtained by the flying body. The method for determining the outdoor temperature evaluation value corresponding to the flying body is not limited. For example, the corresponding temperature coefficient is determined based on the altitude difference of the flying body, and then the determined temperature coefficient is multiplied with the weather forecast temperature and the outdoor temperature collected by the land body to obtain the outdoor temperature evaluation value corresponding to the flying body. If only the weather forecast temperature and the outdoor temperature collected by the land body are collected, the two can be averaged to obtain the outdoor temperature evaluation value corresponding to the flying body. If only the altitude difference of the flying body and any temperature are collected, the outdoor temperature evaluation value corresponding to the flying body can be determined according to the rule that the temperature decreases by 6°C for every 1 km increase in altitude. As an example only, the cooling or heating power, wind speed and other parameters of the air conditioner can be automatically adjusted according to the outdoor temperature evaluation value and the temperature set in the car.

[0035] The air conditioning adjustment method without an outdoor temperature sensor provided in the present embodiment obtains data to be evaluated for the user to evaluate the outdoor temperature of the flying body, including at least one of the outdoor temperature data collected by the land body, the altitude difference of the flying body, and weather forecast information, and then determines the outdoor temperature evaluation value corresponding to the flying body based on the data to be evaluated, and performs corresponding air conditioning based on the outdoor temperature evaluation value. In the case of eliminating the ambient temperature sensor of the flying body, the ambient temperature can be estimated by an algorithm to realize automatic air conditioning control, thereby achieving weight reduction and cost reduction of the flying body.

[0036] In this embodiment, an air conditioning adjustment method without an external temperature sensor is provided, which can be used for a flying body in a flying car. Figure 2 is a flow chart of an air conditioning adjustment method without an external temperature sensor according to an embodiment of the present invention. Figure 2 As shown, the process includes the following steps:

[0037] Step S201, obtaining data to be evaluated for evaluating the external temperature of the flying body, the data to be evaluated includes at least one of the external temperature data collected by the terrestrial body, the altitude difference of the flying body, and weather forecast information. Figure 1 Step S101 of the illustrated embodiment will not be described in detail here.

[0038] Step S202: determining an external temperature evaluation value corresponding to the flying object based on the data to be evaluated, and performing corresponding air conditioning adjustment based on the external temperature evaluation value.

[0039] Specifically, the weather forecast information at least includes the above step S202 including:

[0040] Step S2021, based on the preset temperature coefficients corresponding to the vehicle external temperature data, the altitude difference of the flying body, and the weather forecast temperature, determine the temperature values ​​to be evaluated respectively.

[0041] Step S2022, based on the temperature data outside the vehicle, the altitude difference of the flying body, and the temperature to be evaluated values ​​corresponding to the weather forecast temperature, the evaluation value of the temperature outside the vehicle corresponding to the flying body is calculated.

[0042] In an embodiment of the present invention, corresponding temperature coefficients can be set for the outdoor temperature data, the altitude difference of the flying body, and the weather forecast temperature, respectively. The basis and method for setting the temperature coefficients are not limited. The temperature coefficients can be set based on actual human professional experience or multiple experiments to determine the influence of each data to be evaluated on the evaluation of the outdoor temperature of the flying body. The corresponding relationship between different flight environments and the above three temperature coefficients can also be obtained based on multiple experiments. During the driving process of the flying body, the corresponding temperature coefficient can be determined according to the current flight environment. The temperature coefficient can represent the credibility coefficient for evaluating the outdoor temperature of the flying body. Generally, the first temperature coefficient a corresponding to the outdoor temperature data can be set between 0 and 1, and the second temperature coefficient b=1-a corresponding to the weather forecast temperature. The altitude of the flying body can be set to a default coefficient value of 6 based on experience, which is only used as an example.

[0043] In an embodiment of the present invention, the data to be evaluated is actually obtained based on the flying body, and the data is multiplied by the corresponding preset temperature coefficient to determine the temperature value to be evaluated corresponding to the data to be evaluated. Then, the calculated temperature values ​​to be evaluated corresponding to the data to be evaluated can be added together to obtain the external temperature evaluation value corresponding to the flying body, which is only taken as an example.

[0044] In a specific embodiment, when the above three types of data to be evaluated are obtained, the product of the vehicle outside temperature data and the first temperature coefficient can be calculated to obtain the first temperature value to be evaluated, the product of the weather forecast temperature and the second temperature coefficient can be calculated to obtain the second temperature value to be evaluated, and then the product of the altitude difference between the flying body and the land body and the third temperature coefficient can be calculated to obtain the third temperature value to be evaluated. The sum of the first temperature value to be evaluated and the second temperature value to be evaluated can be calculated, and then the sum can be subtracted from the third temperature value to be evaluated to obtain the vehicle outside temperature evaluation value corresponding to the flying body, that is, the vehicle outside temperature evaluation value T can be calculated by the following formula:

[0045] T=a*T1+b*T2-c*(H-H0)

[0046] Wherein, T represents the evaluation value of the outside temperature; a represents the first temperature coefficient; T1 represents the outside temperature data collected by the land body; b represents the second temperature coefficient; T2 represents the weather forecast temperature; H represents the current altitude of the flying body, and H0 represents the altitude before the flying body leaves the ground.

[0047] The present invention sets the corresponding temperature coefficient according to the influence of the outdoor temperature data, the altitude difference of the flying body and the weather forecast temperature waiting evaluation data on the outdoor temperature of the flying body, and then calculates the outdoor temperature evaluation value based on the temperature coefficient and the data to be evaluated, thereby improving the accuracy of the outdoor temperature evaluation.

[0048] Specifically, the length of time that the terrestrial body is in a power-off state after the terrestrial body and the flying body are separated is obtained; the positioning distance between the flying body and the terrestrial body is obtained; based on the length of time that the terrestrial body is in a power-off state and the positioning distance between the flying body and the terrestrial body, a first temperature coefficient is determined; and the second temperature coefficient is determined by subtracting the first temperature coefficient from the sum of the preset temperature coefficients.

[0049] The preset temperature coefficient sum is the sum of the first temperature coefficient and the second temperature coefficient.

[0050] In an optional embodiment, a first temperature coefficient is determined based on a duration in which the terrestrial body is in a power-off state and a positioning distance between the flying body and the terrestrial body, including: when a preset condition is not met, the first temperature coefficient is determined based on a duration in which the terrestrial body is in a power-off state and a positioning distance between the flying body and the terrestrial body; the temperature coefficient determination step also includes: when the preset condition is met, determining zero or the sum of the preset temperature coefficients as the first temperature coefficient.

[0051] The embodiments of the present invention do not limit the preset conditions, and can be set according to the actual flight scene. For example, the flying body can calculate the duration t that the terrestrial body is in the power-off state through the time module, and then obtain the positions of the flying body and the terrestrial body through the GPS positioning module, and calculate the real-time positioning distance d between the two. It can be determined whether the positioning distance d is less than the preset distance threshold D, and whether the duration t in the power-off state is less than the preset duration threshold tc, where D and tc are calibrable coefficients, indicating that under the power-off duration or the distance, the reliability of the vehicle outside temperature data collected by the terrestrial body is zero, corresponding to The first temperature coefficient is zero, that is, the corresponding preset condition is: positioning distance d ≥ preset distance threshold D, and / or the duration of time that the land-based body is in the power-off state t ≥ tc. When the preset conditions are met, the first temperature coefficient is set to zero, and the corresponding second temperature coefficient can be set to b = 1-a, where 1 is the preset temperature coefficient and is only used as an example; if the preset conditions are not met, that is, the positioning distance d < preset distance threshold D, and the duration of time that the land-based body is in the power-off state t < tc, the first temperature coefficient can be set based on the flight environment of the current flying body, and then the second temperature coefficient can be set accordingly.

[0052] The present invention determines the first temperature coefficient based on the length of time the land body is in the power-off state and the positioning distance between the flying body and the land body, thereby achieving the credibility of determining the land body temperature based on the real-time distance relationship between the land body and the flying body, and improving the accuracy of calculating the external temperature of the flying body.

[0053] Specifically, the length of time that the land body is in the power-off state is divided by a preset length threshold to obtain a first ratio, and the first ratio is subtracted from a preset standard value to obtain a first coefficient; the positioning distance between the flying body and the land body is divided by a preset distance threshold to obtain a second ratio, and the second ratio is subtracted from the preset standard value to obtain a second coefficient; the first coefficient and the second coefficient are multiplied to obtain a first temperature coefficient.

[0054] In the present invention, when it is determined that the positioning distance d is less than the preset distance threshold D, and the duration t that the land vehicle is in the power-off state is less than tc, the first temperature coefficient can be calculated by the following formula, wherein the preset standard value is generally 1, which is only used as an example:

[0055] a=(1-d / D)(1-t / tc)

[0056] Then, based on the calculated first temperature coefficient, the second temperature coefficient is determined.

[0057] In an optional implementation, when the first preset condition is met, zero is determined as the first temperature coefficient.

[0058] Among them, the first preset condition is that the acquired vehicle exterior temperature data is not within a preset first normal range, and / or that failure prompt information of the vehicle exterior temperature sensor transmitted by the land vehicle is received.

[0059] The embodiment of the present invention can determine whether the outdoor temperature data is within a preset first normal temperature range after obtaining the outdoor temperature data, wherein the first normal temperature range can be set according to the current season weather, etc. The first preset condition may be that the outdoor temperature data is not within the first normal range, and / or the outdoor temperature sensor failure prompt information transmitted by the land vehicle is received, such as information such as unstable or too low voltage or current, or directly reporting an error code. When the first preset condition is met, it indicates that the ambient temperature sensor of the land vehicle has failed, and it can be determined that the credibility of the outdoor temperature data collected by the land vehicle is zero, and it can be determined that the first temperature coefficient is zero, and the corresponding second temperature coefficient is 1, which is only for example.

[0060] When the present invention determines that the land vehicle ambient temperature sensor fails, the corresponding first temperature coefficient is set to zero, thereby preventing abnormal land vehicle external temperature data from affecting the accuracy of evaluating the flying vehicle external temperature.

[0061] In an optional embodiment, when a preset condition is met, zero or a preset temperature coefficient and a sum are determined as the first temperature coefficient, including: when a second preset condition is met, a preset temperature coefficient and a sum are determined as the first temperature coefficient, wherein the second preset condition is that the obtained weather temperature is not within a preset second normal temperature range or the weather forecast temperature is not obtained.

[0062] The embodiment of the present invention obtains real-time weather forecast temperature through the weather forecast interface module. After receiving the weather forecast temperature, it can be determined whether the weather forecast temperature is within a preset second normal range. The set second preset condition can be to determine that the weather forecast temperature is not within the preset second normal range, or the weather forecast temperature is not obtained through the weather forecast module. When the second preset condition is met, it can be indicated that the weather forecast interface module fails, and the credibility of the weather forecast temperature is determined to be zero. Then the first temperature coefficient can be set to 1, and the corresponding second temperature coefficient can be set to zero.

[0063] When the present invention determines that the weather forecast interface module fails, the corresponding second temperature coefficient is set to zero, which can prevent the abnormal weather forecast temperature from affecting the accuracy of evaluating the external temperature of the flying body.

[0064] In this embodiment, a flying car is also provided. Figure 3 As shown, the flying car includes a flying body and a land body, the flying body and the land body are connected, and the controller in the flying body is used to execute the above-mentioned air conditioning adjustment method without an external temperature sensor.

[0065] In a specific embodiment, Figure 4As shown, the land body includes an external temperature acquisition module for obtaining the external temperature data T1 of the land body through the ambient temperature sensor, a GPS positioning module for obtaining the position of the land body and a time module for obtaining the power-off time of the land body. The land body transmits the obtained data to the flying body wirelessly through the data transmission module. The flying body receives the position of the land body through the data receiving module, and then determines the position of the flying body through the GPS positioning module, and calculates the positioning distance d between the land body and the flying body; receives the power-off time t0 of the land body through the data receiving module, and then obtains the current time t1 of the flying body through the time module, and calculates the power-off time t=t1-t0 of the land body; judges the relationship between d and D, t and tc, when d<D and t<tc, a=(1-d / D)(1-t / tc); when d≥D or t≥tc, set a=0, corresponding to the second temperature coefficient b=1-a.

[0066] The flying body obtains the outside temperature T1 of the land body through the data receiving module, and obtains the weather forecast temperature T2 through the weather forecast interface module. Then, the altitude H0 before the flying body takes off and the current altitude H are obtained through the altitude detection module. The outside temperature evaluation value of the flying body is calculated by the following formula:

[0067] T=a*T1+b*T2-c*(H-H0)

[0068] Where c is a calibrable coefficient representing the temperature drop per unit altitude.

[0069] The air conditioning control module in the flying body automatically adjusts the cooling or heating power, wind speed and other parameters of the air conditioning according to the determined outdoor temperature evaluation value and the set temperature inside the vehicle. For detailed description, please refer to the above embodiment and will not be repeated here.

[0070] In this embodiment, an air conditioning control device without an outside temperature sensor is also provided, which is used to implement the above-mentioned embodiments and preferred implementation modes, and the descriptions that have been made will not be repeated. As used below, the term "module" can be a combination of software and / or hardware that implements a predetermined function. Although the devices described in the following embodiments are preferably implemented in software, the implementation of hardware, or a combination of software and hardware, is also possible and conceivable.

[0071] This embodiment provides an air conditioning control device without an external temperature sensor, which is applied to a flying body in a flying car. The flying body establishes a communication connection with a land body in the flying car, such as Figure 5As shown, it includes: a data acquisition module 501, which is used to obtain data to be evaluated for evaluating the outdoor temperature of the flying body, and the data to be evaluated includes at least one of the outdoor temperature data collected by the land body, the altitude difference of the flying body, and weather forecast information; a temperature evaluation module 502, which is used to determine the outdoor temperature evaluation value corresponding to the flying body based on the data to be evaluated, and perform corresponding air conditioning adjustment based on the outdoor temperature evaluation value.

[0072] In some optional embodiments, the weather forecast information includes at least the weather forecast temperature, and the temperature evaluation module 502 includes: a temperature to-be-evaluated value determination unit, used to determine the temperature to-be-evaluated values ​​corresponding to the vehicle outside temperature data, the altitude difference of the flying body, and the preset temperature coefficients corresponding to the weather forecast temperature; a temperature evaluation value calculation unit, used to calculate the vehicle outside temperature evaluation value corresponding to the flying body based on the vehicle outside temperature data, the altitude difference of the flying body, and the temperature to-be-evaluated values ​​corresponding to the weather forecast temperature.

[0073] In some optional embodiments, the preset temperature coefficients corresponding to the outdoor temperature data and the weather forecast temperature are respectively the first temperature coefficient and the second temperature coefficient, and the first temperature coefficient and the second temperature coefficient are obtained by the following temperature coefficient determination steps: obtaining the length of time that the land body is in the power-off state after the land body and the flying body are separated; obtaining the positioning distance between the flying body and the land body; determining the first temperature coefficient based on the length of time that the land body is in the power-off state and the positioning distance between the flying body and the land body; determining the second temperature coefficient by subtracting the first temperature coefficient from the sum of the preset temperature coefficients, and the sum of the preset temperature coefficients is the sum of the first temperature coefficient and the second temperature coefficient.

[0074] In some optional embodiments, a first temperature coefficient is determined based on the duration that the terrestrial body is in the power-off state and the positioning distance between the flying body and the terrestrial body, including: dividing the duration that the terrestrial body is in the power-off state by a preset duration threshold to obtain a first ratio, and then subtracting the first ratio from a preset standard value to obtain a first coefficient; dividing the positioning distance between the flying body and the terrestrial body by a preset distance threshold to obtain a second ratio, and then subtracting the second ratio from the preset standard value to obtain a second coefficient; multiplying the first coefficient by the second coefficient to obtain the first temperature coefficient.

[0075] In some optional embodiments, a first temperature coefficient is determined based on a duration in which the terrestrial body is in a power-off state and a positioning distance between the flying body and the terrestrial body, including: when a preset condition is not met, the first temperature coefficient is determined based on a duration in which the terrestrial body is in a power-off state and a positioning distance between the flying body and the terrestrial body; the temperature coefficient determination step also includes: when the preset condition is met, determining zero or the sum of the preset temperature coefficients as the first temperature coefficient.

[0076] In some optional embodiments, when a preset condition is met, zero or a preset temperature coefficient and is determined as a first temperature coefficient, including: when the first preset condition is met, zero is determined as the first temperature coefficient, the first preset condition is that the acquired outdoor temperature data is not within a preset first normal range, and / or, outdoor temperature sensor failure prompt information transmitted by the land vehicle is received.

[0077] In some optional embodiments, when a preset condition is met, zero or a preset temperature coefficient and a sum are determined as the first temperature coefficient, including: when a second preset condition is met, a preset temperature coefficient and a sum are determined as the first temperature coefficient, wherein the second preset condition is that the obtained weather temperature is not within a preset second normal temperature range or the weather forecast temperature is not obtained.

[0078] The further functional description of each of the above modules and units is the same as that of the above corresponding embodiments and will not be repeated here.

[0079] The air conditioning control device without an outdoor temperature sensor in this embodiment is presented in the form of a functional unit, where the unit refers to an ASIC (Application Specific Integrated Circuit) circuit, a processor and memory that executes one or more software or fixed programs, and / or other devices that can provide the above functions.

[0080] The embodiment of the present invention also provides a computer device having the above Figure 5 Air conditioning system shown without outside temperature sensor.

[0081] See also Figure 6 , Figure 6 is a schematic diagram of the structure of a computer device provided by an optional embodiment of the present invention, such as Figure 6 As shown, the computer device includes: one or more processors 10, a memory 20, and interfaces for connecting various components, including high-speed interfaces and low-speed interfaces. Various components are connected to each other using different buses for communication, and can be installed on a common mainboard or installed in other ways as needed. The processor can process the instructions executed in the computer device, including instructions stored in or on the memory to display the graphical information of the GUI on an external input / output device (such as, a display device coupled to the interface). In some optional embodiments, if necessary, multiple processors and / or multiple buses can be used together with multiple memories and multiple memories. Similarly, multiple computer devices can be connected, and each device provides some necessary operations (for example, as a server array, a group of blade servers, or a multi-processor system). Figure 6 A processor 10 is taken as an example.

[0082] The processor 10 may be a central processing unit, a network processor or a combination thereof. The processor 10 may further include a hardware chip. The hardware chip may be a dedicated integrated circuit, a programmable logic device or a combination thereof. The programmable logic device may be a complex programmable logic device, a field programmable gate array, a general purpose array logic or any combination thereof.

[0083] The memory 20 stores instructions executable by at least one processor 10, so that at least one processor 10 executes the method shown in the above embodiment.

[0084] The memory 20 may include a program storage area and a data storage area, wherein the program storage area may store an operating system, an application required for at least one function; the data storage area may store data created according to the use of the computer device, etc. In addition, the memory 20 may include a high-speed random access memory, and may also include a non-transient memory, such as at least one disk storage device, a flash memory device, or other non-transient solid-state storage device. In some optional embodiments, the memory 20 may optionally include a memory remotely arranged relative to the processor 10, and these remote memories may be connected to the computer device via a network. Examples of the above-mentioned network include, but are not limited to, the Internet, an intranet, a local area network, a mobile communication network, and combinations thereof.

[0085] The memory 20 may include a volatile memory, such as a random access memory; the memory may also include a non-volatile memory, such as a flash memory, a hard disk or a solid state drive; the memory 20 may also include a combination of the above types of memory.

[0086] The computer device also includes an input device 30 and an output device 40. The processor 10, the memory 20, the input device 30 and the output device 40 may be connected via a bus or other means. Figure 6 The example of connecting through bus is taken in the following.

[0087] The input device 30 can receive input digital or character information, and generate key signal input related to the user settings and function control of the computer device, such as a touch screen, a keypad, a mouse, a track pad, a touch pad, an indicator bar, one or more mouse buttons, a trackball, a joystick, etc. The output device 40 may include a display device, an auxiliary lighting device (e.g., an LED) and a tactile feedback device (e.g., a vibration motor), etc. The above-mentioned display device includes but is not limited to a liquid crystal display, a light emitting diode, a display and a plasma display. In some optional embodiments, the display device can be a touch screen.

[0088] The embodiment of the present invention also provides a computer-readable storage medium. The method according to the embodiment of the present invention can be implemented in hardware, firmware, or can be implemented as a computer code that can be recorded in a storage medium, or can be implemented as a computer code that is originally stored in a remote storage medium or a non-temporary machine-readable storage medium and will be stored in a local storage medium through a network download, so that the method described herein can be stored in such software processing on a storage medium using a general-purpose computer, a dedicated processor, or programmable or dedicated hardware. Among them, the storage medium can be a magnetic disk, an optical disk, a read-only storage memory, a random access memory, a flash memory, a hard disk or a solid-state hard disk, etc.; further, the storage medium can also include a combination of the above types of memories. It can be understood that a computer, a processor, a microprocessor controller, or programmable hardware includes a storage component that can store or receive software or computer code. When the software or computer code is accessed and executed by a computer, a processor, or hardware, the method shown in the above embodiment is implemented.

[0089] Although the embodiments of the present invention have been described in conjunction with the accompanying drawings, those skilled in the art may make various modifications and variations without departing from the spirit and scope of the present invention, and such modifications and variations are all within the scope defined by the appended claims.

Claims

1. An air conditioning adjustment method without an external temperature sensor, characterized in that: A flying body in a flying car is applied to establish a communication connection with a land body in the flying car, and the method includes: Acquire data to be evaluated for evaluating the external temperature of the flying body, wherein the data to be evaluated includes at least one of external temperature data collected by the terrestrial body, an altitude difference of the flying body, and weather forecast information; Based on the data to be evaluated, an evaluation value of the vehicle's outside temperature corresponding to the flying object is determined, and corresponding air conditioning adjustment is performed based on the evaluation value of the vehicle's outside temperature.

2. The method according to claim 1, characterized in that The weather forecast information at least includes a weather forecast temperature, and the step of determining an external temperature evaluation value corresponding to the flying object based on the data to be evaluated includes: Determine the temperature values ​​to be evaluated corresponding to the vehicle exterior temperature data, the altitude difference of the flying body, and the preset temperature coefficients corresponding to the weather forecast temperature; Based on the outside temperature data, the altitude difference of the flying body, and the temperature to be evaluated corresponding to the weather forecast temperature, the outside temperature evaluation value corresponding to the flying body is calculated.

3. The method according to claim 2, characterized in that The preset temperature coefficients corresponding to the vehicle exterior temperature data and the weather forecast temperature are the first temperature coefficient and the second temperature coefficient, respectively. The first temperature coefficient and the second temperature coefficient are obtained by the following temperature coefficient determination steps: Get the duration of the land body being in the power-off state after the land body and the flying body are separated; Get the positioning distance between the flying object and the terrestrial object; Determining a first temperature coefficient based on a duration during which the terrestrial body is in a power-off state and a positioning distance between the flying body and the terrestrial body; The second temperature coefficient is determined by subtracting the first temperature coefficient from a preset temperature coefficient sum, where the preset temperature coefficient sum is the sum of the first temperature coefficient and the second temperature coefficient.

4. The method according to claim 3, characterized in that The determining of the first temperature coefficient based on the duration of the terrestrial body being in the power-off state and the positioning distance between the flying body and the terrestrial body comprises: Dividing the duration of the land vehicle being in the power-off state by a preset duration threshold to obtain a first ratio, and subtracting the first ratio from a preset standard value to obtain a first coefficient; Dividing the positioning distance between the flying object and the terrestrial object by a preset distance threshold to obtain a second ratio, and subtracting the second ratio from a preset standard value to obtain a second coefficient; The first coefficient and the second coefficient are multiplied to obtain a first temperature coefficient.

5. The method according to claim 3 or 4, characterized in that: The determining of the first temperature coefficient based on the duration of the terrestrial body being in the power-off state and the positioning distance between the flying body and the terrestrial body comprises: When the preset condition is not met, determining a first temperature coefficient based on the duration of the power-off state of the terrestrial body and the positioning distance between the flying body and the terrestrial body; The temperature coefficient determination step also includes: When a preset condition is met, zero or a preset temperature coefficient sum is determined as the first temperature coefficient.

6. The method according to claim 5, characterized in that The step of determining zero or a sum of preset temperature coefficients as the first temperature coefficient when a preset condition is met includes: When a first preset condition is met, zero is determined as the first temperature coefficient. The first preset condition is that the acquired outside temperature data is not within a preset first normal range, and / or that an outside temperature sensor failure prompt information transmitted by the land vehicle is received.

7. The method according to claim 5, characterized in that The step of determining zero or a sum of preset temperature coefficients as the first temperature coefficient when a preset condition is met includes: When the second preset condition is met, the preset temperature coefficient and is determined as the first temperature coefficient, wherein the second preset condition is that the acquired weather temperature is not within the preset second normal temperature range or the weather forecast temperature is not acquired.

8. An air conditioning device without an external temperature sensor, characterized in that: The flying body in the flying car is used to establish a communication connection with the land body in the flying car. The device includes: A data acquisition module, used to acquire data to be evaluated for evaluating the external temperature of the flying body, wherein the data to be evaluated includes at least one of the external temperature data collected by the terrestrial body, the altitude difference of the flying body, and weather forecast information; The temperature evaluation module is used to determine the vehicle exterior temperature evaluation value corresponding to the flying object based on the data to be evaluated, and to perform corresponding air conditioning adjustment based on the vehicle exterior temperature evaluation value.

9. A flying car, characterized in that: The flying car includes a flying body and a land body, the flying body establishes a communication connection with the land body, the flying body includes a controller, the controller includes a memory and a processor, the memory and the processor are communicatively connected to each other, the memory stores computer instructions, and the processor executes the air conditioning adjustment method without an outdoor temperature sensor according to any one of claims 1 to 7 by executing the computer instructions.

10. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores computer instructions, and the computer instructions are used to enable a computer to execute the air conditioning adjustment method without an external temperature sensor according to any one of claims 1 to 7.

Images