CN115511010A - Method and system for classifying pilot driving style based on aircraft landing process - Google Patents

Method and system for classifying pilot driving style based on aircraft landing process Download PDF

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CN115511010A
CN115511010A CN202211451872.0A CN202211451872A CN115511010A CN 115511010 A CN115511010 A CN 115511010A CN 202211451872 A CN202211451872 A CN 202211451872A CN 115511010 A CN115511010 A CN 115511010A
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pilot
landing
altitude
clustering
flight data
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CN115511010B (en
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诸彤宇
曹文华
林新智
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Beihang University
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Abstract

The invention relates to a method and a system for classifying pilot driving style based on an aircraft landing process, wherein the method comprises the following steps: step S1: dividing the aircraft landing process into different altitude intervals according to the ground clearance of the aircraft, and clustering the flight data subsequences in each altitude interval to obtain landing semantic codes; step S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probability; and step S3: and clustering the pilot style vectors to obtain the pilot style category. The method provided by the invention can analyze the driving operation style of the pilot and classify the pilot so as to help civil aviation operation to improve the safety level and guide an airline company to improve the pilot culture scheme.

Description

Method and system for classifying pilot driving style based on aircraft landing process
Technical Field
The invention relates to the field of civil aviation flight safety, in particular to a method and a system for classifying pilot driving style based on an aircraft landing process.
Background
The guarantee of civil aviation flight safety is the premise of carrying out all specific civil aviation activities. Of all flight phases, the accident incidence and the accident mortality rate are significantly higher in the landing phase than in the other phases, being one of the most dangerous flight phases. The flight accident is caused by the combined action of the pilot, the environment and the airplane. Therefore, how to analyze the driving style of the pilot to help civil aviation operation to improve the safety level and instruct an airline company to improve the pilot culture scheme becomes an urgent problem to be solved.
Disclosure of Invention
In order to solve the technical problem, the invention provides a method and a system for classifying pilot driving style based on an aircraft landing process.
The technical solution of the invention is as follows: a method for classifying pilot driving style based on an aircraft landing process comprises the following steps:
step S1: dividing the aircraft landing process into different altitude intervals according to the ground clearance of the aircraft, and clustering the flight data subsequences in the altitude intervals to obtain landing semantic codes;
step S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probabilities;
and step S3: and clustering the pilot style vectors to obtain the pilot style category.
Compared with the prior art, the invention has the following advantages:
the invention discloses a method for classifying pilot driving style based on an aircraft landing process, which can calculate the preference degree of a pilot for controlling the state transition of an aircraft in different aircraft states in the aircraft landing process, is used for analyzing the driving operation style of the pilot and classifying the pilot, and helps civil aviation to improve the safety level and guide an airline company to improve the pilot culture scheme.
Drawings
FIG. 1 is a flowchart of a method for classifying the driving style of a pilot based on the landing process of an aircraft according to an embodiment of the present invention;
fig. 2 is a block diagram of a pilot driving style classification system based on an aircraft landing process according to an embodiment of the present invention.
Detailed Description
The invention provides a method for classifying pilot driving style based on an airplane landing process, which can analyze the driving operation style of a pilot and classify the pilot so as to help civil aviation operation to improve the safety level and guide an airline company to improve the pilot culture scheme.
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings.
Example one
As shown in fig. 1, a method for classifying a pilot driving style based on an aircraft landing process according to an embodiment of the present invention includes the following steps:
step S1: dividing the aircraft landing process into different altitude intervals according to the ground clearance of the aircraft, and clustering the flight data subsequences in each altitude interval to obtain landing semantic codes;
step S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probability;
and step S3: and clustering the pilot style vectors to obtain the pilot style category.
In one embodiment, the step S1: according to the ground clearance of the airplane, dividing the landing process of the airplane into different height intervals, clustering flight data subsequences in each height interval to obtain landing semantic codes, and specifically comprising the following steps:
step S11: acquiring a flight data set M, wherein the flight data set M comprises P pilots, and each pilot has flight data of F flights;
Figure 906444DEST_PATH_IMAGE001
wherein the content of the first and second substances,
Figure 605279DEST_PATH_IMAGE002
indicating the ith flightFlight data for the member's jth flight; order to
Figure 85939DEST_PATH_IMAGE003
Wherein, in the step (A),
Figure 112801DEST_PATH_IMAGE004
flight data, T, representing the 1 st second of the ith pilot's jth flight during landing ij Indicating the duration of the jth flight of the ith pilot in the landing stage; wherein the content of the first and second substances,
Figure 704319DEST_PATH_IMAGE005
,
Figure 398606DEST_PATH_IMAGE006
a value representing the nth flight data for the ith pilot for the jth flight during the 1 st second of landing;
step S12: respectively calculating mean value mean of single flight data of all flights in M n And standard deviation ofstd n
Figure 784588DEST_PATH_IMAGE007
Figure 688958DEST_PATH_IMAGE008
Using mean n Andstd n for flight data
Figure 818588DEST_PATH_IMAGE009
Standardized processing is carried out to obtain standardized flight data
Figure 367382DEST_PATH_IMAGE010
(ii) a Wherein the content of the first and second substances,
Figure 189844DEST_PATH_IMAGE011
partitioning M into two subdata sets M 1 And M 2 Wherein, in the process,M 1 and M 2 All contain all pilots in M, and each pilot contains the same amount of flight data;
step S13: dividing the landing process of the airplane into K altitude intervals according to the ground clearance of the airplane: { (H) i-1 ,H i ) I =1,2,3 \8230K }, wherein H i Is a division value of the height interval; flight data that standardizes primary flights
Figure 456877DEST_PATH_IMAGE012
Is shown as
Figure 390198DEST_PATH_IMAGE013
Wherein, in the step (A),
Figure 652552DEST_PATH_IMAGE014
flight data representing the flight in the first altitude interval is represented as
Figure 911495DEST_PATH_IMAGE015
Wherein, in the step (A),
Figure 400245DEST_PATH_IMAGE016
a radio altitude representing the u-th second recorded in the flight data;
step S14: using a Dynamic Time Warping (DTW) -based k-means + + time sequence clustering method to M 1 Clustering the flight data of all flights in different height intervals, and adjusting the number of each clustering center and initializing each clustering center initial value to make the clustering outline coefficient as small as possible to obtain the landing semantic code number of the airplane in the kth height intervalτ k Then the set of all landing semantic codes for the kth altitude interval is represented as
Figure 137257DEST_PATH_IMAGE017
Thus, flight data for the j-th flight of the i pilots can be normalized
Figure 395063DEST_PATH_IMAGE018
Is shown as
Figure 824908DEST_PATH_IMAGE019
Wherein, in the process,
Figure 535375DEST_PATH_IMAGE020
in one embodiment, the above S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probability, wherein the method specifically comprises the following steps:
step S21: calculating M 1 The conditional probability of occurrence of any two landing semantic codes of each pilot in all adjacent altitude intervals;
Figure 76077DEST_PATH_IMAGE021
wherein, the first and the second end of the pipe are connected with each other,
Figure 578603DEST_PATH_IMAGE022
expressing that the ith pilot semantically codes the ith code for the ith altitude interval in the kth altitude interval
Figure 913769DEST_PATH_IMAGE023
Under the condition (1), the landing semantic code of the (k + 1) th altitude interval is the r-th code of the altitude interval
Figure 377112DEST_PATH_IMAGE024
The probability of (d);card{ } is the operation of calculating the number of collection elements;
step S22: each height interval hasN i The landing semantic code is used for constructing the ith pilot
Figure 455926DEST_PATH_IMAGE025
Driving style vector of dimension
Figure 688324DEST_PATH_IMAGE026
Wherein, in the step (A),
Figure 194392DEST_PATH_IMAGE027
the probability matrix representing all landing semantic code transitions of the ith pilot from the kth altitude interval to the (k + 1) th altitude interval is represented as
Figure 145031DEST_PATH_IMAGE028
In one embodiment, the step S3: clustering the pilot style vectors to obtain the pilot style categories, which specifically comprises the following steps:
step S31: using KMeans clustering method to determine driving style vectorV 1 ,V 2 ,V 3V P ]Clustering to obtain the class of pilot's driving styleS 1 ,S 2 ,S 3S P ]Wherein, in the process,S i a driving style category for the ith pilot;
step S32: to M is aligned with 2 Repeating the steps S2 to S3 to obtain all the pilot style categories
Figure 27536DEST_PATH_IMAGE029
(ii) a Order to
Figure 239074DEST_PATH_IMAGE030
And then, the L is minimized by adjusting the initial clustering centers and the number of the clustering centers of the Kmeans clustering method in the S3, and finally all the pilot style categories are obtained.
The flight data of different batches of pilots with longer flight time can be classified by the classification method provided by the embodiment of the invention, so that the difference of the classification results is minimum. In addition, the clustered categories can be labeled by flight instructors or experienced pilots, and finally, the label of each category is obtained.
The invention discloses a method for classifying pilot driving style based on an airplane landing process, which can calculate the preference degree of a pilot for controlling airplane state transition in different airplane states in the airplane landing process, is used for analyzing the driving operation style of the pilot and classifying the pilot, and helps civil aviation operation to improve the safety level and guides an airline company to improve the pilot culture scheme.
Example two
As shown in fig. 2, an embodiment of the present invention provides a system for classifying a pilot's driving style based on an aircraft landing process, which includes the following modules:
the obtaining landing semantic code module 41 is configured to divide the aircraft landing process into different altitude intervals according to the altitude of the aircraft from the ground, and cluster the flight data subsequences in each altitude interval to obtain a landing semantic code;
a pilot driving style vector construction module 42, configured to calculate conditional probabilities of any two landing semantic codes of each pilot in all adjacent altitude sections, respectively, and construct a pilot driving style vector based on the conditional probabilities;
and the pilot style category obtaining module 43 is configured to cluster the pilot style vectors to obtain the pilot style categories.
The above examples are provided for the purpose of describing the present invention only and are not intended to limit the scope of the present invention. The scope of the invention is defined by the appended claims. Various equivalent substitutions and modifications can be made without departing from the spirit and principles of the invention, and are intended to be within the scope of the invention.

Claims (5)

1. A method for classifying pilot driving style based on an aircraft landing process is characterized by comprising the following steps:
step S1: dividing the aircraft landing process into different altitude intervals according to the ground clearance of the aircraft, and clustering the flight data subsequences in the altitude intervals to obtain landing semantic codes;
step S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probabilities;
and step S3: and clustering the pilot style vectors to obtain the pilot style category.
2. The method for classifying pilot' S driving style based on aircraft landing procedure according to claim 1, wherein the step S1: dividing the aircraft landing process into different altitude intervals according to the ground clearance of the aircraft, clustering the flight data subsequences in the altitude intervals to obtain landing semantic codes, and specifically comprising the following steps:
step S11: acquiring a flight data set M, wherein the flight data set M comprises P pilots, and each pilot has flight data of F flights;
Figure 901974DEST_PATH_IMAGE001
wherein, the first and the second end of the pipe are connected with each other,
Figure 147010DEST_PATH_IMAGE002
flight data representing the ith pilot's jth flight; order to
Figure 192327DEST_PATH_IMAGE003
Wherein, in the step (A),
Figure 587536DEST_PATH_IMAGE004
flight data, T, representing the 1 st second of the ith pilot's jth flight during landing ij Indicating the duration of the jth flight of the ith pilot in the landing stage; wherein the content of the first and second substances,
Figure 605171DEST_PATH_IMAGE005
,
Figure 427633DEST_PATH_IMAGE006
a value representing the nth flight data for the ith pilot for the jth flight during the 1 st second of landing;
step S12: respectively calculating mean value mean of single flight data of all flights in M n And standard ofDifference betweenstd n
Figure 960246DEST_PATH_IMAGE007
Figure 159146DEST_PATH_IMAGE009
Using mean n Andstd n for flight data
Figure 155921DEST_PATH_IMAGE010
Standardized processing is carried out to obtain standardized flight data
Figure 149284DEST_PATH_IMAGE011
(ii) a Wherein, the first and the second end of the pipe are connected with each other,
Figure 169193DEST_PATH_IMAGE012
partitioning M into two subdata sets M 1 And M 2 Wherein M is 1 And M 2 All contain all pilots in M, and each pilot contains the same amount of flight data;
step S13: dividing the landing process of the airplane into K altitude intervals according to the ground clearance of the airplane: { (H) i-1 ,H i ) I =1,2,3 \ 8230k }, wherein H i Is a division value of the height interval; normalizing flight data for a flight
Figure 906205DEST_PATH_IMAGE013
Is shown as
Figure 632852DEST_PATH_IMAGE014
Wherein, in the step (A),
Figure 62697DEST_PATH_IMAGE015
flight data representing the flight in the first altitude interval, denoted as
Figure 569902DEST_PATH_IMAGE016
Wherein, in the process,
Figure 845025DEST_PATH_IMAGE017
represents the radio altitude of the u second recorded in the flight data;
step S14: using a k-means + + time sequence clustering method based on dynamic time warping to M 1 Clustering the flight data of all flights in different height intervals, and adjusting the number of each clustering center and initializing each clustering center initial value to make the clustering outline coefficient as small as possible to obtain the landing semantic code number of the airplane in the kth height intervalτ k Then the set of all landing semantic codes for the kth altitude interval is represented as
Figure 816392DEST_PATH_IMAGE018
Thus, flight data for the j-th flight of the i pilots can be normalized
Figure 417138DEST_PATH_IMAGE019
Is shown as
Figure 146059DEST_PATH_IMAGE020
Wherein, in the step (A),
Figure 428136DEST_PATH_IMAGE021
3. the method for classifying pilot' S driving style based on aircraft landing procedure according to claim 2, wherein the step S2: respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals, and constructing a pilot driving style vector based on the conditional probabilities, wherein the method specifically comprises the following steps:
step S21: calculating M 1 In all adjacent altitude areas for each pilotThe conditional probability of any two landing semantic codes in between;
Figure 926114DEST_PATH_IMAGE023
wherein the content of the first and second substances,
Figure 963340DEST_PATH_IMAGE024
expressing that the ith pilot semantically codes the ith code for the ith altitude interval in the kth altitude interval
Figure 913978DEST_PATH_IMAGE025
Under the condition (1), the landing semantic code of the (k + 1) th altitude interval is the r-th code of the altitude interval
Figure 124380DEST_PATH_IMAGE026
The probability of (d);card{ } is an operation to count the number of collection elements;
step S22: each height interval hasN i Landing semantic code is adopted to construct the model of the ith pilot
Figure 476864DEST_PATH_IMAGE027
Driving style vector of dimension
Figure 684991DEST_PATH_IMAGE028
Wherein, in the process,
Figure 122926DEST_PATH_IMAGE029
the probability matrix representing all landing semantic code transitions of the ith pilot from the kth altitude interval to the (k + 1) th altitude interval is represented as
Figure 746805DEST_PATH_IMAGE030
4. The method for classifying pilot' S driving style based on aircraft landing procedure according to claim 3, wherein the step S3: clustering the pilot style vectors to obtain pilot style categories, specifically comprising:
step S31: the driving style vector [ 2 ] using KMeans clustering methodV 1 ,V 2 ,V 3V P ]Clustering to obtain the class of pilot's driving styleS 1 ,S 2 ,S 3S P ]Wherein, in the step (A),S i a driving style category for the ith pilot;
step S32: to M 2 Repeating the steps S2 to S3 to obtain all the pilot style categories
Figure DEST_PATH_IMAGE031
(ii) a Order to
Figure 484954DEST_PATH_IMAGE032
And then, the L is minimized by adjusting the initial clustering centers and the number of the clustering centers of the Kmeans clustering method in the S3, and finally all the pilot style categories are obtained.
5. A pilot driving style classification system based on an airplane landing process is characterized by comprising the following modules:
the system comprises an obtaining landing semantic coding module, a classifying module and a classifying module, wherein the obtaining landing semantic coding module is used for dividing the landing process of the airplane into different altitude intervals according to the ground clearance of the airplane, and clustering flight data subsequences in the altitude intervals to obtain landing semantic codes;
the pilot driving style vector building module is used for respectively calculating the conditional probability of any two landing semantic codes of each pilot in all adjacent altitude intervals and building a pilot driving style vector based on the conditional probability;
and the pilot style category acquisition module is used for clustering the pilot style vectors to obtain the pilot style categories.
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Citations (5)

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CN106548294A (en) * 2016-11-11 2017-03-29 中国民航大学 A kind of landing maneuver Performance Evaluation Methods and device based on flying quality
CN107909106A (en) * 2017-11-14 2018-04-13 北京航空航天大学 A kind of detection method of aircraft flight environment
CN111340388A (en) * 2020-03-13 2020-06-26 中国民航大学 Pilot operation quality evaluation method based on flight QAR data
CN114004292A (en) * 2021-10-29 2022-02-01 重庆大学 Pilot flat-floating ejector rod behavior analysis method based on flight parameter data unsupervised clustering

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2436164C1 (en) * 2010-10-01 2011-12-10 Федеральное государственное образовательное учреждение высшего профессионального образования "Военный авиационный инженерный университет" (г. Воронеж) Министерства обороны Российской Федерации Method of assessing quality of piloting aeroplane by pilot during landing phase based on data from standard on-board recording device
CN106548294A (en) * 2016-11-11 2017-03-29 中国民航大学 A kind of landing maneuver Performance Evaluation Methods and device based on flying quality
CN107909106A (en) * 2017-11-14 2018-04-13 北京航空航天大学 A kind of detection method of aircraft flight environment
CN111340388A (en) * 2020-03-13 2020-06-26 中国民航大学 Pilot operation quality evaluation method based on flight QAR data
CN114004292A (en) * 2021-10-29 2022-02-01 重庆大学 Pilot flat-floating ejector rod behavior analysis method based on flight parameter data unsupervised clustering

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