CN110979728A - Flight data processing method, flight data reading method, flight data processing device, electronic equipment and storage medium - Google Patents
Flight data processing method, flight data reading method, flight data processing device, electronic equipment and storage medium Download PDFInfo
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- CN110979728A CN110979728A CN201911111138.8A CN201911111138A CN110979728A CN 110979728 A CN110979728 A CN 110979728A CN 201911111138 A CN201911111138 A CN 201911111138A CN 110979728 A CN110979728 A CN 110979728A
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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Abstract
The application discloses a flight data processing method, a flight data reading device, electronic equipment and a storage medium. The flight data processing method comprises the following steps: the method comprises the steps of obtaining flight data of flights, compiling the flight data at the user-defined moment to obtain a parameter set corresponding to the user-defined moment, wherein the parameter set comprises a plurality of sub-parameters. According to the processing method of the flight data, the flight data of the flights included in the custom moment is determined by obtaining the flight data of the flights, so that the flight data of the custom moment is compiled to obtain the parameter set of the custom moment, related personnel can directly obtain the parameter set of the custom moment and the sub-parameters corresponding to the parameter set of the custom moment, and the efficiency is improved.
Description
Technical Field
The present disclosure relates to the field of flight technologies, and in particular, to a method and an apparatus for processing flight data, an electronic device, and a storage medium.
Background
In the related art, when whether a flight is in a certain state or not is judged, a plurality of related parameters need to be acquired according to flight data for comprehensive analysis, and related personnel need to independently program each related parameter, so that the operation is complex and the efficiency is low.
Disclosure of Invention
The embodiment of the application provides a flight data processing method, a flight data reading device, electronic equipment and a storage medium.
The flight data processing method of the embodiment of the application comprises the following steps:
acquiring flight data of flights; and
compiling the flight data at the user-defined time to obtain a parameter set corresponding to the user-defined time, wherein the parameter set comprises a plurality of sub-parameters.
In some embodiments, the custom time includes a plurality of times, and compiling the flight data at the custom time to obtain a parameter set corresponding to the custom time includes:
and analyzing the flight data to determine the custom moment.
In some embodiments, the compiling the flight data at the custom time to obtain a parameter set corresponding to the custom time, where the parameter set includes a plurality of sub-parameters includes:
and configuring a parameter set corresponding to the user-defined time according to the user-defined time.
In some embodiments, the processing method further comprises:
the flight data of the flight data is processed to obtain a measurement parameter.
The method for reading flight data comprises the following steps:
responding to the input user-defined time, and reading the parameter set corresponding to the user-defined time; and
and responding to the input sub-parameter name, and reading the sub-parameter corresponding to the sub-parameter name.
In some embodiments, the reading method further comprises:
and reading the measurement parameter corresponding to the name of the measurement parameter in response to the input name of the measurement parameter.
The flight data processing device according to the embodiment of the present application includes:
the acquisition module is used for acquiring original flight data of flights; and
the compiling module is used for compiling the flight data at the user-defined time to obtain a parameter set corresponding to the user-defined time, and the parameter set comprises a plurality of sub-parameters.
The electronic device of the embodiment of the application comprises a processor, and the processor is used for processing any flight data processing method and any flight data reading method.
The computer storage medium according to the embodiments of the present application stores a computer program that, when executed by a processor, implements the flight data processing method and the flight data reading method according to any of the embodiments described above.
According to the flight data processing method, the flight data reading device, the electronic equipment and the storage medium, flight data of flights corresponding to the custom moment are determined according to the acquired flight data, and therefore the custom moment is compiled to obtain the parameter set of the custom moment. Related personnel can directly obtain the parameter set at the user-defined moment and the sub-parameters of the parameter set at the user-defined moment, the operation is simple and convenient, and the efficiency is improved.
Additional aspects and advantages of the present application will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the present application.
Drawings
The above and/or additional aspects and advantages of the present application will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a schematic flow chart of a flight data processing method according to an embodiment of the present application.
Fig. 2 is a block diagram of a flight data processing device according to an embodiment of the present application.
Fig. 3 is another flow chart of a flight data processing method according to an embodiment of the present application.
Fig. 4 is another flow chart of a flight data processing method according to an embodiment of the present application.
Fig. 5 is a flowchart illustrating a method for reading flight data according to an embodiment of the present application.
Fig. 6 is a block diagram of a device for reading flight data according to an embodiment of the present application.
Fig. 7 is a schematic view of a read page of flight data according to an embodiment of the present application.
Detailed Description
Reference will now be made in detail to embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the accompanying drawings are illustrative and are only for the purpose of explaining the present application and are not to be construed as limiting the present application.
Generally, the current flight data includes three types, namely, recorded parameters, calculated parameters and measured parameters. The recording parameters refer to raw data collected by a bus and raw data collected by a sensor, which are recorded by equipment, and the frequency range is 1/64Hz to 32 Hz. The recording parameters are binary data, which can be converted into decimal data by decoding.
Calculating a parameter refers to transforming and calculating one or more recording parameters to generate a value of a specified frequency.
The measured parameters refer to the summarized values obtained by processing and analyzing the recorded parameters or the calculated parameters by related personnel. For example, processing and analyzing recorded parameters or calculated parameters over a certain period of time or a certain range of heights results in maximum speed, maximum height, and the like.
In the related art, when a relevant person researches a flight state, since a measurement parameter is a summarized value obtained by recording or calculating the parameter, a conclusion is obtained by comprehensively analyzing and judging a plurality of measurement parameters related to the flight state. For each measurement parameter, the related personnel is required to individually develop the program for a specific measurement parameter. The operation is complicated and the efficiency is low.
Referring to fig. 1 and fig. 2, a method for processing flight data is provided in an embodiment of the first aspect of the present application. The processing method comprises the following steps:
s10, acquiring flight data of the flight; and
and S20, compiling the flight data at the custom moment to obtain a parameter set corresponding to the custom moment, wherein the parameter set comprises a plurality of sub-parameters.
The embodiment of the present application further provides a processing device 100 for flight data, where the processing device 100 includes an obtaining module 12 and a compiling module 14. S10 may be implemented by acquisition module 12 and S20 may be implemented by compilation module 14. That is, the acquisition module 12 may be used to acquire flight data for a flight. Compiling module 14 may be configured to compile the flight data at the custom time to obtain a parameter set corresponding to the custom time, where the parameter set includes a plurality of sub-parameters.
The embodiment of the application further provides electronic equipment, which comprises a processor, wherein the processor is used for acquiring flight data of a flight, compiling the flight data at the user-defined time to obtain a parameter set corresponding to the user-defined time, and the parameter set comprises a plurality of sub-parameters.
The electronic device may be a terminal or a device with data processing capability, such as a personal computer, a tablet computer, a mobile phone, or a personal digital assistant.
Specifically, a flight will record the flight data at each moment in time as it travels normally along the airline. When a relevant person researches a state of a user-defined time, the flight data of the user-defined time in the state is generally acquired and analyzed, so as to determine whether the state is abnormal. The self-defined time refers to a value which can be defined by related personnel according to the requirement at a certain time in the flight process. Different times can be set to obtain different custom times, for example, flight departure time, grounding time, maximum descent rate time below 1000 feet and the like are set as the custom times. In some embodiments, if the relevant personnel needs to acquire whether the flight state of the flight at the grounding time is abnormal, the airspeed of the flight at the grounding time, the ground speed at the grounding time, the flight overload at the grounding time, the descent rate at the grounding time, the weight at the grounding time, the flap configuration at the grounding time, the throttle at the grounding time, and the like need to be extracted, so as to comprehensively determine whether the flight state of the flight at the grounding time is abnormal. The grounding time is set as a custom time, and parameters of airspeed, grounding speed, flight overload, descending rate, weight, flap configuration, throttle and the like of the grounding time are parameters included in the custom time.
Further, the compiling module 14 analyzes the flight data of the flight to obtain a value of the custom time to determine the parameter recorded at the custom time, and compiles the parameter recorded at the custom time to obtain a parameter set corresponding to the custom time. So that each custom time includes a corresponding set of parameters.
Therefore, when the relevant personnel research the flight in a certain state, the required sub-parameters can be directly obtained from the corresponding parameter set at the user-defined time, and each parameter does not need to be developed and obtained by an independent program, so that the workload of the relevant personnel for developing the program is reduced, the operation is simple and convenient, and the efficiency for obtaining the parameters is improved.
Referring to fig. 3, in some embodiments, S20 includes:
and S22, analyzing the flight data to determine the custom moment.
In some embodiments, compiling module 14 includes processing unit 142, and S22 may be implemented by processing unit 142, or processing unit 142 may be configured to analyze flight data to determine a custom time.
In certain embodiments, the processor is configured to analyze the flight data to determine a custom time.
Specifically, the processing unit 142 further analyzes the flight data recorded during a certain period of time or a certain distance in the flight process of the flight, so as to determine which time is the custom time, where the custom time includes the parameters recorded at the time, and compiles the parameters included in the custom time to obtain a parameter set of the custom time. And for different self-defined moments, the self-defined moments can be determined according to different flight data. For example, flight data may be confirmed from radio altitude greater than 0 to 0 or from non-compressed to compressed state of the landing gear at the time of grounding during flight landing. And when the flight is at the highest point, the maximum value of the standard air pressure altitude can be determined according to the analysis of the standard air pressure altitude recorded when the flight flies along the air route, and the time when the flight is at the maximum value of the standard air pressure altitude can be obtained.
In certain embodiments, S20 further comprises:
and S24, configuring a parameter set corresponding to the user-defined time according to the user-defined time.
In some embodiments, compiling module 14 further includes a configuration unit 144, and S24 may be implemented by configuration unit 144. That is, the configuration unit 144 is configured to configure a parameter set corresponding to the custom time according to the custom time.
In some embodiments, the processor is further configured to configure a set of parameters corresponding to the custom time according to the custom time.
Specifically, the user-defined time is defined as a user-defined time by a certain time according to needs of related personnel, so that the user-defined time can be multiple. Since the flight data at each time during the flight is recorded, all parameters of the time are recorded at each custom time. And determining a parameter value corresponding to the user-defined time, and configuring the parameter included in the user-defined time and the corresponding user-defined time. For example, the custom time may include a grounding time, a 1000 foot maximum descent rate time, and the like. Parameters configured for the flight grounding moment comprise airspeed of the grounding moment, ground speed of the grounding moment, flight overload of the grounding moment, descending rate of the grounding moment, weight of the grounding moment, flap configuration of the grounding moment, throttle of the grounding moment and the like. Parameters configured for the 1000 foot maximum descent rate time instant include: a maximum descent rate of 1000 feet or less, a longitude of a maximum descent rate time of 1000 feet or less, a latitude of a maximum descent rate time of 1000 feet or less, a pitch angle of a maximum descent rate time of 1000 feet or less, a field pressure altitude of a maximum descent rate time of 1000 feet or less, a thrust of a maximum descent rate time of 1000 feet or less, and the like.
Furthermore, the compiling module 14 further includes a storage unit. The storage unit includes a plurality of storage units, each of which stores a corresponding sub-parameter of the parameter set at the user-defined time, for example, the compiling module 14 includes a first storage unit and a second storage unit, the first storage unit stores a parameter at the grounding time, and the second storage unit stores a parameter at the takeoff time. Therefore, the storage structure of the data is changed by storing the parameter set at the user-defined moment through the storage unit, the storage space is effectively saved, and the reading efficiency can be improved.
Referring to fig. 4, in some embodiments, the processing method further includes:
and S30, processing the flight data of the flight data to obtain the measurement parameters.
In some embodiments, S30 may be implemented by processing module 16. That is, the processing module 16 may be used for flight data processing of the flight data to derive the measured parameter.
In certain embodiments, the processor is configured to process the flight data to obtain the measured parameter.
It will be appreciated that in some cases, when a relevant person is studying a certain state, in addition to obtaining a parameter of a customized time corresponding to the state, other parameters of a non-customized time may also be obtained. For example, the relevant personnel need to analyze whether the low-altitude 1000-foot flight enters a stable approaching state, and the parameters of the custom time needed to be used include a maximum descent rate below 1000 feet, a longitude of a maximum descent rate below 1000 feet, a latitude of a maximum descent rate below 1000 feet, a pitch angle of a maximum descent rate below 1000 feet, a field pressure altitude of a maximum descent rate below 1000 feet, and a thrust of a maximum descent rate below 1000 feet. In addition, parameters of the maximum descent rate time below 1000 feet to the ground point flying time length and the maximum descent rate time below 1000 feet to the ground point flying distance are needed, and the maximum descent rate time below 1000 feet to the ground point flying time length and the maximum descent rate time below 1000 feet to the ground point flying distance are measurement parameters obtained by the relevant personnel through flight data processing.
Further, flight data related to the measured parameter is determined, and the flight data related to the measured parameter is processed to obtain the measured parameter. For example, when determining that the measurement parameter is the maximum descent rate time of 1000 feet or less and the distance to the ground point, it is necessary to process parameters such as the geographical position of the flight at the maximum descent rate of 1000 feet or less and the geographical position of the ground time. Therefore, related personnel can obtain the sub-parameters of the parameter set corresponding to the user-defined time and can also obtain the measurement parameters.
Referring to fig. 5 and 6, a second embodiment of the present application provides a method for reading flight data, which is used for reading the flight data processed by the first embodiment. The reading method of the flight data comprises the following steps:
s40, responding to the input custom time, reading a parameter set corresponding to the custom time; and
s50, in response to the input sub-parameter name, reading the sub-parameter corresponding to the sub-parameter name.
The embodiment of the present application further provides a device 200 for reading flight data, where the device 200 includes a first reading module 22 and a second reading module 24. S40 may be implemented by the first reading module 22 and S50 may be implemented by the second reading module 24. That is, the first reading module 22 may be configured to read a parameter set corresponding to a custom time in response to the input custom time. The second reading module 24 may be configured to read a sub-parameter corresponding to the sub-parameter name in response to the input sub-parameter name.
The processor provided by the embodiment of the application is further configured to read a parameter set corresponding to the user-defined time in response to the input user-defined time, and read a sub-parameter corresponding to the sub-parameter name in response to the input sub-parameter name.
The reading apparatus 200 may further include a first input module and a second input module, where the first input module is configured to input the customized time, and because there are many parameter sets corresponding to the customized time, related personnel configure different parameter sets according to different requirements, when the related personnel analyze a flight in a certain state, the first input module inputs the customized time corresponding to the state, and the parameter set corresponding to the customized time can be read. And if the sub-parameter names of the parameter sets corresponding to the user-defined time are input in the second input module, the second reading module responds to the input sub-parameter names and reads the sub-parameters corresponding to the sub-parameter names. For example, referring to fig. 7, in some examples, the custom time may include a grounding time, an off-field time, and a maximum descent rate time below 1000 feet, among others. The grounding time comprises airspeed of the grounding time, grounding speed of the grounding time, flight overload of the grounding time, descending rate of the grounding time, weight of the grounding time, flap configuration of the grounding time, an accelerator of the grounding time and the like, and a parameter set and sub-parameters of each custom time correspond to a mnemonic code. If the related personnel need to analyze the grounding time, the first reading module can read the parameter set of the grounding time only by inputting the name or mnemonic code of the grounding time in the first input module, namely inputting the grounding time in the name input box of the newly added parameter set or inputting the mnemonic code in the mnemonic code box. When the mnemonic code or the name of the sub-parameter of the parameter set corresponding to the grounding moment is input in the second input module, that is, the mnemonic code or the name of the sub-parameter is input in the search box in the configuration sub-parameter. For example, if "airspeed at the grounding time" and "ground speed at the grounding time" are input or the mnemonics "SAD", "ASDFASDGADSG" are input, the second reading module reads the airspeed value and the ground speed value at the grounding time corresponding to the airspeed value and the ground speed value at the grounding time.
Therefore, through the arrangement of the first input module and the second input module, related personnel can conveniently acquire the required parameter set at the user-defined moment and the sub-parameters corresponding to the parameter set, and the efficiency is improved.
In some embodiments, the reading method further comprises:
s60: and reading the measurement parameter corresponding to the name of the measurement parameter in response to the input name of the measurement parameter.
In certain embodiments, where the reading apparatus 200 includes the third reading module 26, S30 may be implemented by the third reading module 26. That is, the third reading module 26 may be configured to read the measurement parameter corresponding to the measurement parameter name in response to the input measurement parameter name.
In some embodiments, the processor is configured to read a measurement parameter corresponding to the measurement parameter name in response to the input measurement parameter name.
In particular, the reading device may further comprise a third input module for inputting a name of the measurement parameter. If the name of the measurement parameter is input into the third input module, the third reading module 26 reads the corresponding measurement parameter according to the input name of the measurement parameter. For example, referring further to fig. 7, in some examples, the relevant personnel need to analyze whether the low-altitude 1000-foot flight enters a stable approach state, and the parameters of the custom time needed to be used include a maximum descent rate below 1000 feet, a longitude below 1000 feet, a latitude below 1000 feet, a pitch below 1000 feet, a field pressure below 1000 feet, and a thrust below 1000 feet. Further, parameters of the maximum descent rate time of 1000 feet or less to the ground point flying length and the maximum descent rate time of 1000 feet or less to the ground point flying distance are also required. The flying time from the maximum descent rate moment below 1000 feet to the grounding point and the flying distance from the maximum descent rate moment below 1000 feet to the grounding point are measurement parameters, and each measurement parameter comprises a corresponding mnemonic code. The first input module and the second input module may obtain parameters included at times of maximum descent rate below 1000 feet. The third input module inputs "the time from the maximum descent rate time below 1000 feet to the ground point flying time", "the time from the maximum descent rate time below 1000 feet to the ground point flying distance" or inputs the corresponding mnemonic code in the search box configured with the measurement parameters, and the third reading module 26 reads the values from the time from the maximum descent rate time below 1000 feet to the ground point flying time and from the time from the maximum descent rate time below 1000 feet to the ground point flying distance.
Therefore, related personnel can obtain the parameters at the user-defined moment and can conveniently obtain the required measurement parameters.
A computer storage medium according to an embodiment of the present application stores a computer program that, when executed by a processor, implements the instructions for the flight data processing method according to any one of the above-described embodiments and the instructions for the flight data reading method according to any one of the above-described embodiments.
In the description of the present specification, reference to the description of the terms "one embodiment", "some embodiments", "an illustrative embodiment", "an example", "a specific example", or "some examples", etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
It will be understood by those skilled in the art that all or part of the steps carried out to implement the above-described implementation method can be implemented by a program that can be executed by associated hardware and can be stored in a computer-readable storage medium, and the program, when executed, includes one or a combination of the steps of the implementation method.
In addition, functional units in the embodiments of the present application may be integrated into one processing module, or each unit may exist alone physically, or two or more units are integrated into one module. The integrated module can be realized in a hardware mode, and can also be realized in a software functional module mode. The integrated module, if implemented in the form of a software functional module and sold or used as a stand-alone product, may also be stored in a computer readable storage medium. The storage medium mentioned above may be a read-only memory, a magnetic or optical disk, etc.
While embodiments of the present application have been shown and described, it will be understood by those of ordinary skill in the art that: numerous changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the application, the scope of which is defined by the claims and their equivalents.
Claims (10)
1. A method of processing flight data, the method comprising:
acquiring flight data of flights; and
compiling the flight data at the user-defined time to obtain a parameter set corresponding to the user-defined time, wherein the parameter set comprises a plurality of sub-parameters.
2. The processing method of claim 1, wherein the custom time includes a plurality of times, and the compiling the flight data at the custom time to obtain the parameter set corresponding to the custom time includes:
and analyzing the flight data to determine the custom moment.
3. The processing method of claim 1, wherein the compiling the flight data at a custom time to obtain a parameter set corresponding to the custom time, the parameter set comprising a plurality of sub-parameters comprises:
and configuring a parameter set corresponding to the user-defined time according to the user-defined time.
4. The processing method according to claim 1, characterized in that it further comprises:
the flight data of the flight data is processed to obtain a measurement parameter.
5. A reading method for reading flight data processed by the processing method of any one of claims 1 to 4, the reading method comprising:
responding to the input user-defined time, and reading the parameter set corresponding to the user-defined time; and
and responding to the input sub-parameter name, and reading the sub-parameter corresponding to the sub-parameter name.
6. The reading method according to claim 5, further comprising:
and reading the measurement parameter corresponding to the name of the measurement parameter in response to the input name of the measurement parameter.
7. A flight data processing apparatus, comprising:
the acquisition module is used for acquiring original flight data of flights; and
the compiling module is used for compiling the flight data at the user-defined time to obtain a parameter set corresponding to the user-defined time, and the parameter set comprises a plurality of sub-parameters.
8. A device for reading flight data, the device comprising:
the first reading module is used for responding to an input user-defined time and reading the parameter set corresponding to the user-defined time;
and the second reading module is used for responding to the input sub-parameter name and reading the sub-parameter corresponding to the sub-parameter name.
9. An electronic device, characterized in that it comprises a processor for processing the processing method of flight data according to any one of claims 1 to 4 and the reading method of flight data according to any one of claims 5 to 6.
10. A computer storage medium, characterized in that it stores a computer program that, when executed by a processor, implements the instructions of a flight data processing method according to claims 1-4 and the instructions of a flight data reading method according to claims 5-6.
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Application publication date: 20200410 |