CN105355114A - Flight operation task and instrument monitor task simulation system based on flat computer gravity induction system and simulation method - Google Patents
Flight operation task and instrument monitor task simulation system based on flat computer gravity induction system and simulation method Download PDFInfo
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Abstract
The invention relates to the flight simulation field, more specifically a flight operation task and instrument monitor task simulation system based on a flat computer gravity induction system and a simulation method. The double task simulation system comprises a flight simulation operation unit based on the flat computer gravity system, a flight subject design unit of a computer server, a management unit of a flight simulation model usage environment for a participant, and a flight simulation monitor and data analysis unit. The gravity induction system of a general flat computer is used to simulate the flight operation. Compared with the products that use external operating lever equipment, the system has the advantages of low cost and convenient usage; the flight simulation effect is more lifelike by using a software system internal algorithm and a visual sense system operation system in combination; and a tester can feel smoother during flight simulation. Therefore, the system can be applied to flight training for professional flight students and flight staff or can be applied to flight detection in special situation.
Description
Technical field
The present invention relates to flight simulation field, be specifically related to based on the flight operation task of panel computer gravity sensing system and instrument monitoring task simulation system and analogy method.
Background technology
Flight occupation is a kind of special occupation, and flying activity carries out in special three-dimensional space environment condition.Aerial mission is complicated, and pilot often will bear the physical limit of high load capacity and large overload, and also will grasp scientific knowledge up-to-date in a large number fast, wherein two task cognitive ability is indispensable pith simultaneously.Therefore, set up the two TU task unit of flight simulation and be significant, all have great Research Significance and powerful application prospect in multiple fields such as pilot selection, flight training, fatigue detecting and antifatigue training.
The flight-simulation equipment that current application is more, all needs complicated hardware device, the such as external unit such as operating grip, control lever.Such as, Lufthansa Group, for the special instrument hardware equipment of the flight simulation task of selecting, lasts three hours, has checked and examined and many-sided psychological traits such as the closely-related functipnal capability of flight.Civil Aviation Flight College is also applied to the recruit-pilot work of CAAC flying cadet, but lower owing to testting efficiency, has a strong impact on choice process, is being promoted on a large scale.Although flight simulation software equipment to a certain degree simulate aerial mission, pilot selection and training in all played effect.But because it all needs special external unit; and must be connected with high performance desktop computer; therefore there is significant limitation; both the inconvenient a large amount of tests carrying out colony in the choice of recruiting pilot; also carry out flight simulation task in the inconvenient field limited in external environment or hardstand environment, therefore in application, all there is larger limitation.
Gravity sensor, also known as gravity sensor, novel genus sensor technology, it adopts elastic sensing element to make cantilevered shifter, with the energy-stored spring adopting elastic sensing element to make to drive electric contact, completes the conversion from Gravity changer to electric signal.Current most middle and high ends smart mobile phone and the built-in gravity sensor of panel computer.Gravity sensor screen when mobile phone anyhow can automatically turn, and can replace up and down playing games.Measure the acceleration because gravity causes by gravity sensor, equipment angle of inclination with respect to the horizontal plane can be calculated.
The present invention utilizes the gravity sensing system simulation of panel computer to fly.Civilian aviator is being carried out on the basis of job analysis, extract in its work and the cognitive index of most crucial operation is required, based on flight operation task and the instrument monitoring task simulation system of panel computer gravity sensing system to two task cognitive ability (flight operation task and instrument monitoring task).Take two task operating patterns of operation task and monitor task, task one is the control errors of flight operation instrument, and the sextuple space being driven in up, down, left, right, before and after in the air drives an airplane, and task two is the monitoring to multiple meter lamp state.In addition, test adopts panel computer to implement, and use the gravity sensing system simulation sextuple space of panel computer, sensitivity is similar to the driving experience of Boeing large aircraft, and undistorted, has again feature flexibly and fast.Being established as based on the checking and examining of flight simulation, training and research work provides basic means and basic platform of this system.
Summary of the invention
The object of the invention is with panel computer is carrier, utilizes the function of its gravity sensing system to carry out the foundation of flight operation task and instrument monitoring task simulation system, provides one based on the system and method for the two task of dull and stereotyped simulated flight.
According to the specific embodiment of the present invention, describedly comprise four parts based on the simulated flight operation task of flat gravity induction system and the system of instrument monitoring task, Part I is the flight simulation operating unit based on panel computer gravity system, Part II is the flight account design unit of computer server, Part III is the administrative unit of participant's flight simulation environment for use, and Part IV is monitoring and the data analysis unit of flight simulation.Specific as follows:
One, based on the flight simulation operating unit of panel computer gravity system, five modules are specifically comprised.
The flight operation module that 1-1, flat gravity induction system bring out
The real-time random variation of heads up display is represented in the display screen of panel computer, user carries out real time correction by the change to heads up display of the gravity sensing system using panel computer, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback in the change of heads up display, thus realizes the effect of flight operation simulation smoothly.
According to following formula, produce random disturbance, be presented at the instant random variation of flight operation panel board in computer screen, by using the function of dull and stereotyped gravity sensing system, at the operate tablet computer of three-dimensional perspective, produce the operation change of X-axis, Y-axis, Z axis, to correct the error that random disturbance produces.Tester is shown in the bidimensional change of flight operation panel board on computer screen by the operant response of gravity sensing system.The operation performance immediate feedback of tester on screen display, thus adjusts.
Control lever task
The pitching of application dynamic menu simulated aircraft, roll attitude, participant's right hand single order controls the change of bidimensional:
Instant random variation is produced in X-axis, Y-axis by following formula, the coordinate in each moment is made all on the basis of a upper moment coordinate, to produce not expected change in displacement, it is the random disturbance that tester causes that this random change in displacement constitutes computing machine, it is made to produce deviation with balance reference position, require that tester awares the random variation of each moment position as early as possible, and the external unit accurately and fast produced by dull and stereotyped gravity sensing system is effectively adjusted, and makes to reduce with the deviation of benchmark equilibrium position as far as possible
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t.
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1).
Allow computing machine often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit.
This test adopts the adaptive mode of computing machine, and barre operation task sets different grade of difficulty, determines the grade of difficulty that tester can reach.
Dynamic similation forms the random disturbance of 60 grade of difficulty automatically, the change of grade of difficulty D, is reached by the value changing t.D=f (T), along with the reduction of chronomere T, grade of difficulty strengthens.Computing machine applies the random disturbance that can divide 60 grade of difficulty automatically to experimenter, destroys the equilibrium state of instrument.
The flight monitoring module that 1-2, dull and stereotyped visual presentation system are brought out
The real-time random variation of six flight simulation warning meter lamps is represented in the display screen of panel computer, user monitors in real time by using the change of the touch screen function of panel computer to multiple flight simulation warning meter lamp, and require according to different sections object the judgement reaction carrying out button, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, the judgement of immediate feedback meter lamp is corrected errors, thus realizes the effect that meter lamp monitors in real time.
Set each flight simulation warning meter lamp and all have green light, amber light and red light three kinds of states, according to the change of time dependent random function control instrument lamp, certain random times instrument panel lamp becomes amber light from green light, tester needs to be noted this warning instrument, amber light enters red light phase after changing for 3 seconds, and tester needs to remove warning by the on & off switch clicked on screen on relevant position as soon as possible, after tester's operation, red light returns to green light phase, enters next random rotation.There is multiple flight simulation warning meter lamp in screen, the rule that each instrument is all followed above carries out random variation simultaneously.Tester needs to pay close attention to all instrument, and carries out the instruction monitoring and remove alarm operation.
The two task modules jointly presented are monitored in 1-3, flight operation and flight
This module opens gravity sensing function and the touch-screen keypress function of panel computer simultaneously, represents the real-time random variation of heads up display and the real-time random variation of flight simulation warning meter lamp in the display screen of panel computer simultaneously.User by use panel computer gravity sensing system real-time correction is carried out to its change, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback in the change of heads up display, thus realizes the effect of flight operation simulation smoothly.Simultaneously, user monitors in real time by using the change of the touch screen function of panel computer to six flight simulation warning meter lamps and requires to carry out the judgement reaction of button according to different sections object, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, immediate feedback is corrected errors in the judgement of meter lamp, thus realizes the effect that meter lamp monitors in real time.
Control lever task
The pitching of application dynamic menu simulated aircraft, roll attitude, participant's right hand single order controls the change of bidimensional:
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t.
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1).
Allow computing machine often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit.
This test adopts the adaptive mode of computing machine, and barre operation task sets different grade of difficulty, determines the grade of difficulty that tester can reach.
Dynamic similation forms the random disturbance of 60 grade of difficulty automatically, the change of grade of difficulty D, is reached by the value changing t.D=f (T), along with the reduction of chronomere T, grade of difficulty strengthens.Computing machine applies the random disturbance that can divide 60 grade of difficulty automatically to experimenter, destroys the equilibrium state of instrument.
1-4, rest module.
This module presents clocking information with countdown, and related cognitive task, does not use as rest module.
Module is introduced in 1-5, test
This module playing video file, to explain and publicise to user for the use of the two task of flight simulation.
Two, the flight account design unit of computer server, specifically comprises three modules.
2-1 arranges the task definition of flight simulation and the module of parameter
The function of this module mainly occurs in administrator role, and can realize parameter and arranges the particular content of the module of three in Part I.Specifically arrange content to comprise: the selection of flight operation, flight monitoring, two task three kinds of modules; The selection of flight operation module difficulty adaptive mode and difficulty fixed form; The setting of flight operation module difficulty level; The setting of flight monitoring module meter lamp number; The setting of flight monitoring module meter lamp change frequency.
According to a particular embodiment of the invention, the test of Self-adaptive flight operation subject, flight simulation content and the parameter of setting are as follows: the module of selection comprises: introductory video module, flight operation module (using as exercise for first group), rest module, flight operation module (using as official testing for second group).
(1) the flight operation model choice of exercise part fixes difficulty level, the flight operation model choice difficulty adaptive mode of official testing part.
(2) difficulty of the flight operation module of exercise part is 30 grades, the initial difficulty of official testing part flight operation module is 30 grades, then according to the definition of adaptive testing, within every 1 minute, change a difficulty level according to the achievement of tester in this 1 minute.If achievement is lower than the error criterion of setting, then difficulty level reduces by 5 grades on the basis of this difficulty level; If achievement is lower than the error criterion of setting, then difficulty level promotes 5 grades on the basis of this difficulty level.
According to one more embodiment of the present invention, for bringing out tired flight operation and monitoring "Double-task Mode", flight simulation content and the parameter of setting are as follows: the module of selection comprises: introductory video module, flight operation module (using as exercise for first group), instrument monitoring module (using as exercise for first group), dual role module (using as exercise for first group), rest module, flight operation module (using as official testing for second group), instrument monitoring module second group is used as official testing), dual role module second group is used as official testing.
(1) no matter flight operation module, practise with or test use, all selects fixing difficulty level.The difficulty of the flight operation module of exercise part is 50 grades, and official testing part flight operation module installation is 65 grades.
(2) no matter instrument monitoring module, practise with or test use, all selects the difficulty level of 6 instrument panel lamps.
(3) two task module, exercise part selects the difficulty level of 50 grades of flight operation difficulty levels and 6 instrument panel lamps, and official testing part selects the difficulty level of 65 grades of flight operation difficulty levels and 6 instrument panel lamps.
2-2, the duration that flight simulation is set and module sequentially
The function of this module mainly occurs in administrator role, can arrange the duration presenting order and each module of the module of three in Part I.Specifically arrange content to comprise: the setting of the duration of each flight operation chosen, flight monitoring, two task three kinds of modules; The setting of the duration of rest module; Introduce the setting of the order of module; The setting presenting ordinal position of multiple selection module.
According to a particular embodiment of the invention, the test of Self-adaptive flight operation subject, flight simulation duration and the order of setting are as follows: first introduce module, present with visual form, presentative time is 3 minutes.As the flight operation module of exercise, the duration is 5 minutes.Rest module, the duration is 1 minute.As the flight operation module of test, the duration is 10 minutes.
According to a specific embodiment more of the present invention, for bringing out tired flight operation and monitoring "Double-task Mode", flight simulation duration and the order of setting are as follows: introduce module, present with visual form, presentative time is 3 minutes.As flight operation module, instrument monitoring module, each one of two task module of exercise, each duration is 5 minutes.Rest module, the duration is 2 minutes.As flight operation module, instrument monitoring module, each 8 of two task module of the official testing part that fatigue is brought out, the duration is respectively 5 minutes.Rest module in test module 8, each 90 seconds.
2-3, the module of the programme of flight simulation is set
On the basis of " task definition of flight simulation and the module of parameter are set " and " duration of flight simulation and the module of order are set ", by affiliated " arranging the module of the programme of flight simulation " establishment, generation, preserve and editing program list.Affiliated program refers to be arranged in section sometime and carries out a certain specific activity, different program combination is produced the scheme of the two task operating of simulated flight of different demand.Programme is exactly " menu " that form the two task subject of different simulated flight and scheme.In setting in above-mentioned two modules of task and on parameter, duration and basis sequentially, form the scheme of a set of fixing flow process.And the program is named, setting that remarks illustrate, and then to preserve, be presented in programme in list, form fixing flight simulation subject, use for other research work.Meanwhile, new programme can be added at any time, also can edit existing programme.
Three, participant's flight simulation environment for use administrative unit, specifically comprises three modules:
The module of the environment for use of 3-1, construction experimenter flight simulation
The function of this module mainly occurs in research user role, builds the environment for use of experimenter and arranges.Comprise the foundation of experimenter and the typing of personal information, comprise the setting of test environment seat in the plane number and column locations.
The module of the seat in the plane of 3-2, distribution experimenter flight simulation
The function of this module mainly occurs in research user role, distributes the seat in the plane of carrying out test of experimenter and arranges.Comprise the selection of experimenter, the selection of seat in the plane, experimenter is mated with seat in the plane.
The module of the account of 3-3, management flight simulation researcher
The function of this module mainly occurs in senior manager role, manages the authority organizing flight simulation to implement on-the-spot research user.Its function comprises the mechanism of research user, mechanism is arranged with tabular form and manages and show, can increase and revise mechanism information, comprising organization names, sequence number; Arrange main examiner's management information, main examiner is movable organizer, is also responsible for safeguarding examination hall information, needs to arrange main examiner's name, institutional affiliation, login password, and record adds the time of main examiner.
Four, the monitoring of flight simulation and data analysis unit, specifically comprises three modules:
4-1, flight simulation implement the immediately monitoring module of state
The function of this module mainly occurs in research user role, while experimenter carries out the use of flight simulation subject, monitor in the using state of server end to its seat in the plane, can understand its whether take a seat, whether normally log in, whether normally carry out testing, test development situation, with the basic computer hardware information such as the connection status of server end.
The instant observation module of 1-1, flight simulation subject achievement
The function of this module mainly occurs in research user role and senior manager role, perform in two task operating process experimenter, its each performance is monitored and record, monitors when monitoring project comprises the monitoring of flight operation error, the monitoring of instrument operation accuracy, reaction.The monitoring of flight operation error is the error that monitoring experimenter operating lever operation produces particularly; The monitoring of instrument operation accuracy is the accuracy of monitoring experimenter instrument operation, wrong reaction number of times comprises advance operation, postpone operation and without operation; During reaction, reaction velocity when experimenter reddens to instrument warning lamp is monitored in monitoring.
1-2, flight simulation Report downloading and data analysis module
The function of this module mainly occurs in research user role and senior manager role, can real time inspection this examination combined data, i.e. monitor data of experimenter.Also can check and download current completing and the report data of all plays, and preserve in the machine with the form of compressed file, conveniently carry out deep data analysis work.
Comprise the following steps based on the flight operation of flat gravity induction system and the two task simulation method of instrument monitoring:
One, flight simulation operation is carried out based on panel computer gravity system,
Comprise:
(1-1) the real-time random variation representing heads up display in the display screen of panel computer is realized, by using the function of dull and stereotyped gravity sensing system, at the operate tablet computer of three-dimensional perspective, produce the operation change of X-axis, Y-axis, Z axis, to correct the error that random disturbance produces, tester shows in the bidimensional change of flight operation panel board on computer screen by the operant response of gravity sensing system, thus adjusts, realize the effect of flight operation simulation smoothly
Instant random variation is produced in X-axis, Y-axis by following formula, the coordinate in each moment is made all on the basis of a upper moment coordinate, to produce not expected change in displacement, this random change in displacement constitutes the random disturbance for tester causes, and makes it produce deviation with balance reference position
Wherein,
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Make computing machine often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit;
(1-2) in the display screen of panel computer, represent the real-time random variation of flight simulation warning meter lamp, user monitors in real time by using the change of the touch screen function of panel computer to multiple flight simulation warning meter lamp, and require according to different sections object the judgement reaction carrying out button, the judgement of immediate feedback meter lamp is corrected errors, thus realizes the effect that meter lamp monitors in real time;
(1-3) open gravity sensing function and the touch-screen keypress function of panel computer simultaneously, in the display screen of panel computer, represent the real-time random variation of heads up display and the real-time random variation of flight simulation warning meter lamp simultaneously.User by use panel computer gravity sensing system real-time correction is carried out to its change, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback is in the change of heads up display, thus realize the effect of flight operation simulation smoothly, simultaneously, user monitors in real time by using the change of the touch screen function of panel computer to flight simulation warning meter lamp and requires to carry out the judgement reaction of button according to different sections object, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, immediate feedback is corrected errors in the judgement of meter lamp, thus realize the effect that meter lamp monitors in real time,
Control lever task
The pitching of application dynamic menu simulated aircraft, roll attitude, participant's right hand single order controls the change of bidimensional:
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit, often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit, by adaptive mode, barre operation task sets different grade of difficulty, dynamic similation forms the random disturbance of grade of difficulty automatically, the change of grade of difficulty D, reached by the value changing t, D=f (T), along with the reduction of chronomere T, grade of difficulty strengthens, realize the random disturbance of grade of difficulty, destroy the equilibrium state of instrument,
Two, design a calculating machine the flight subject of server
Comprise:
(2-1) task definition and the parameter of flight simulation are set,
The described content based on all modules of the flight simulation operating unit of panel computer gravity system and parameter are set,
(2-1) duration and the order of flight simulation are set
The duration presenting order and each module arranging the described all modules based on the flight simulation operating unit of panel computer gravity system is arranged;
Three, participant's flight simulation environment for use is managed
Comprise:
(3-1) environment for use of construction experimenter flight simulation,
(3-2) distribute the seat in the plane of experimenter's flight simulation, distribute and select the seat in the plane of carrying out test of experimenter,
(3-3) manage the account of flight simulation researcher, management organization flight simulation implements on-the-spot research user
Authority;
Four, flight simulation and data analysis is monitored
Comprise:
(4-1) immediately monitoring flight simulation implements state
When experimenter carries out the use of flight simulation subject, in the using state of server side to monitor experimenter,
(4-2) instant observation mould flight simulation subject achievement
Perform in two task operating process experimenter, its each performance monitored and record,
(4-3) flight simulation form and data analysis is downloaded, the monitor data of real time inspection experimenter
The present invention utilizes the gravity sensing system simulation flight operation of general panel computer, than the product using peripheral operation bar apparatus, cost is low, easy to use, combining to present and make flight simulation effect better true to nature by software systems internal algorithm and vision system operating system, the sensitivity of tester is more smooth.Therefore, among the flight that can be applied under technical flight student, the flight training of aircrew, specific situation detects.
Accompanying drawing explanation
Fig. 1 display is according to the flight operation based on flat gravity induction system of the specific embodiment of the present invention and the two task simulation system of instrument monitoring.
Embodiment
Embodiment 1: the self-adaptation subject that can be used for the flight operation simulation tested
One, the flight simulation operating unit based on panel computer gravity system is set up
The flight operation module that 1-1, flat gravity induction system bring out
This module realizes the real-time random variation representing heads up display in the display screen of panel computer, user carries out real-time correction by using the gravity sensing system of panel computer to its change, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback in the change of heads up display, thus realizes the effect of flight operation simulation smoothly.
Test introduces module, this module playing video file, to explain and publicise to user for the use of the two task of flight simulation, and rest module.
This module presents clocking information with countdown, and related cognitive task, does not use as rest module.
Two, the flight account design unit of computer server, specifically comprises three modules:
2-1, the task definition of flight simulation and the module of parameter are set.
The function of this module produces primarily of administrator role, and can realize parameter and arranges the particular content of above-mentioned flight operation module.In this example, specifically arrange content to comprise:
(1) module selected comprises: introductory video module, flight operation module (using as exercise for first group), rest module, flight operation module (using as official testing for second group).
(2) the flight operation model choice of exercise part fixes difficulty level, the flight operation model choice difficulty adaptive mode of official testing part.
(3) difficulty of the flight operation module of exercise part is 30 grades
(4) the initial difficulty of official testing part flight operation module is 30 grades, then according to the definition of adaptive testing, within every 1 minute, changes a difficulty level according to the achievement of tester in this 1 minute.If achievement is lower than the error criterion of setting, then difficulty level reduces by 5 grades on the basis of this difficulty level; If achievement is lower than the error criterion of setting, then difficulty level promotes 5 grades on the basis of this difficulty level.
2-2, the duration that flight simulation is set and module sequentially
The function of this module produces primarily of administrator role, but the duration presenting order and each module of each flight simulation module is arranged.In this example, specifically arrange content to comprise:
(1) first introduce module, present with visual form, presentative time is 3 minutes.
(2) as the flight operation module of exercise, the duration is 5 minutes.
(3) rest module, the duration is 1 minute.
(4); As the flight operation module of test, the duration is 10 minutes.
2-3, the module of the programme of flight simulation is set
On the basis of " arranging the task definition of flight simulation and the module of parameter " and " arranging the duration of flight simulation and the module of order ", the function of this module is establishment, generates, preserves and editing program list.Program refers to be arranged in section sometime and carries out a certain specific activity, different program combination is produced the scheme of the two task operating of simulated flight of different demand.Programme is exactly " menu " that form the two task subject of different simulated flight and scheme.In setting in above-mentioned two modules of task and on parameter, duration and basis sequentially, form the scheme of a set of fixing flow process.And the program is named, setting that remarks illustrate, and then to preserve, be presented in programme in list, form fixing flight simulation subject, use for other research work.The concrete setting of programme is in this example as following table 1:
Table 1
Three, participant's flight simulation environment for use administrative unit, specifically comprises two modules.
The module of the environment for use of 3-1, construction experimenter flight simulation test
This module, primarily of research user role operation, builds the environment for use of experimenter and arranges.
(1) personal information of typing experimenter, has three testers and participates in experiment in the present embodiment.
(2) setting of test environment seat in the plane number and column locations is set, in the present embodiment, is provided with the test classroom of 1 row 3 row, three testers can be allowed on different seats in the plane simultaneously to complete test.
The module of the seat in the plane of 3-2, distribution experimenter flight simulation.
This module, primarily of research user role operation, is distributed the seat in the plane of carrying out test of experimenter and arranges.
(1) three experimenter a are selected, b, c.
(2) three the seat in the plane X1 arranged are selected, X2, X3.
(3) by experimenter a, b, c distribute to three seat in the plane X1 respectively, X2, X3.
The testing process of experimenter.
(1) first experimenter takes one's seat according to the requirement of researcher, determines that personally identifiable information is errorless, starts test.
(2) viewing test is introduced, and understands content measurement and using method.
(3) carry out the exercise of flight operation simulation, be familiar with using method.
(4) one minute break, prepares official testing
(5) carry out the formal flight operation simulation test of 10 minutes, realize in the mode of self-adaptation difficulty level.
The monitoring of flight simulation, specifically comprises two modules:
1, flight simulation implements the immediately monitoring module of state
While experimenter carries out the use of flight simulation subject, researchist can monitor in the using state of server end to its seat in the plane.Comprise in this example:
Arrange three experimenter a, b, c distribute to three seat in the plane X1, X2, X3.Understand it whether to take a seat, whether normally log in.In test process, understand three experimenters and whether normally carry out testing, testing to proceed to which sequent modular.
2, the instant observation module of flight simulation subject achievement
Perform in flight operation simulation process experimenter, its each performance is monitored and record.Specifically comprise the monitoring of exercise flight operation analog module and test flight operation analog module in this example:
(2-1) the every Fixed Time Interval of exercise flight operation analog module, the error that experimenter's operating lever operation produces
(2-2) the every Fixed Time Interval of test flight operation analog module, the error that experimenter's operating lever operation produces
(2-3) flight operation module is used in exercise, changes in time, the curve map of operate miss change.
(2-4) flight operation module is used in test, changes in time, the curve map of difficulty level change.
Flight simulation Report downloading and data analysis
After test terminates, can check and download the current report data completed, in the present embodiment,
(1) can with the form of compressed file to three experimenter a, the excel file of each self-forming of data of b, b compresses, and with the name of test time, preserves in the machine.
(2) result of everyone flight operation error is depicted as time dependent error change chart in the form of a graph, and convenient reproduction is pasted.
(3) the flight operation error result in everyone stipulated time is presented under curve map in digital form, and by copying the form of stickup, can be replicated in newly-built blank excel form, carrying out data analysis.
Embodiment 2: can be used for the "Double-task Mode" bringing out tired flight operation and flight monitoring
One, the flight simulation operating unit based on panel computer gravity system is set up
The flight operation module that 1-1 plate gravity sensing system is brought out
In the display screen of panel computer, the real-time random variation of heads up display is represented by this module, user carries out real-time correction by using the gravity sensing system of panel computer to its change, the function of gravity sensing feeds back to the software systems of panel computer, by internal algorithm immediate feedback in the change of heads up display, thus realize the effect of flight operation simulation smoothly.In the present embodiment, keep flat at up, down, left, right, before and after sextuple space by operating rod control " aircraft " and fly state, tester uses the gravity sensing system of panel computer, all around tilt flat plate operates, the pitching of application dynamic menu simulated aircraft, roll attitude, upgrade once at interval of 50 milliseconds, system program produces just profound curve at random, change elevation angle and the left and right flip angle of aspect, experimenter requires to want reverse operating, allows the angles return initial point of aircraft as far as possible.The difficulty level of operation, affects the difficulty that program " is set a question ".Difficulty is higher, and the deviation that tester produces is larger.
The flight monitoring module that 1-2, dull and stereotyped visual presentation system are brought out
In the display screen of panel computer, the real-time random variation of six flight simulation warning meter lamps is represented by this module, user monitors in real time by using the change of touch screen function to six meter lamps of panel computer, and require according to different sections object the judgement reaction carrying out button, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, and feedback is corrected errors in the judgement of meter lamp, thus realize the effect that meter lamp monitors in real time.In the present embodiment, tester monitors the dynamic instrument table status of corresponding six positions by clicking six relevant positions, be that emergency condition requires accurately to make a response when certain instrument warning lamp reddens, be dangerous situation when certain meter lamp yellowing, need vigilance, but can not react.Namely the pointer of panel board arranges by current difficulty and turns clockwise, and when rotating to yellow area, pilot lamp becomes yellow, and when rotating to red area, pilot lamp becomes redness.When experimenter presses corresponding reset button, pointer resets back green area, and pilot lamp extinguishes.
The two task modules jointly presented are monitored in 1-3, flight operation and flight
This module opens gravity sensing function and the touch-screen keypress function of panel computer simultaneously, represents the real-time random variation of heads up display and the real-time random variation of six flight simulation warning meter lamps in the display screen of panel computer simultaneously.User carries out real-time correction by using the gravity sensing system of panel computer to its change, and by the feedback function of gravity sensing, immediate feedback in the change of heads up display, thus realizes the effect of flight operation simulation smoothly.Simultaneously, user monitors in real time by using the change of the touch screen function of panel computer to six instrument flight simulation warning meter lamps and requires to carry out the judgement reaction of button according to different sections object, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, immediate feedback is corrected errors in the judgement of meter lamp, thus realizes the effect that meter lamp monitors in real time.
1-4, rest module
This module presents clocking information with countdown, and related cognitive task, does not use as rest module.
Module is introduced in 1-5, test
This module playing video file, to explain and publicise to user for the use of the two task of flight simulation.
This module presents clocking information with countdown, and related cognitive task, does not use as rest module.
Two, the flight account design unit of computer server, specifically comprises three modules:
2-1, the task definition of flight simulation and the module of parameter are set
The function of this module produces primarily of administrator role, and can realize parameter and arranges the particular content of above-mentioned flight operation module.In this example, specifically arrange content to comprise:
(1) module selected comprises: introductory video module, flight operation module (using as exercise for first group), instrument monitoring module (using as exercise for first group), dual role module (using as exercise for first group), rest module, flight operation module (using as official testing for second group), instrument monitoring module second group is used as official testing), dual role module second group is used as official testing).
(2) no matter flight operation module, practise with or test use, all selects fixing difficulty level.
(3) difficulty of the flight operation module of exercise part is 50 grades, and official testing part flight operation module installation is 65 grades.
(4) no matter instrument monitoring module, practise with or test use, all selects the difficulty level of 6 instrument panel lamps.
(5) two task module, exercise part selects the difficulty level of 50 grades of flight operation difficulty levels and 6 instrument panel lamps, and official testing part selects the difficulty level of 65 grades of flight operation difficulty levels and 6 instrument panel lamps.
2-2, the duration that flight simulation is set and module sequentially
The function of this module produces primarily of administrator role, but the duration presenting order and each module of each flight simulation module is arranged.In the present embodiment, specifically arrange content to comprise:
(1) introduce module, present with visual form, presentative time is 3 minutes.
(2) as flight operation module, instrument monitoring module, each one of two task module of exercise, each duration is 5 minutes.
(3) rest module, the duration is 2 minutes.
(4) flight operation module, instrument monitoring module, each 8 of two task module of the official testing part of bringing out as fatigue, the duration is respectively 5 minutes.
(5) the rest module in test module 8, each 90 seconds.
2-3, the module of the programme of flight simulation is set
On the basis of " arranging the task definition of flight simulation and the module of parameter " and " arranging the duration of flight simulation and the module of order ", the function of this module is establishment, generates, preserves and editing program list.Program refers to be arranged in section sometime and carries out a certain specific activity, different program combination is produced the scheme of the two task operating of simulated flight of different demand.Programme is exactly " menu " that form the two task subject of different simulated flight and scheme.In setting in above-mentioned two modules of task and on parameter, duration and basis sequentially, form the scheme of a set of fixing flow process.And the program is named, setting that remarks illustrate, and then to preserve, be presented in programme in list, form fixing flight simulation subject, use for other research work.The concrete setting of the programme in the present embodiment example is as following table 2:
Table 2
Three, participant's flight simulation environment for use administrative unit, specifically comprises two modules:
The module of the environment for use of 3-1, construction experimenter flight simulation test
This module, primarily of research user role operation, builds the environment for use of experimenter and arranges.
(1-1) personal information of typing experimenter, has 6 testers and participates in experiment in this example.
(1-2) setting of test environment seat in the plane number and column locations is set, in this example, is provided with the test classroom of 2 row 3 row, six testers can be allowed on different seats in the plane simultaneously to complete test.
The module of the seat in the plane of 3-2, distribution experimenter flight simulation
This module, primarily of research user role operation, is distributed the seat in the plane of carrying out test of experimenter and arranges.
(1-1) three experimenter a are selected, b, c, d, e, f
(1-2) three the seat in the plane X1 arranged are selected, X2, X3, Y1, Y2, Y3
(1-3) by experimenter a, b, c, d, e, f distribute to three seat in the plane X1 respectively, X2, X3, Y1, Y2, Y3.
The testing process of experimenter:
(1) first experimenter takes one's seat according to the requirement of researcher, determines that personally identifiable information is errorless, starts test.
(2) viewing test is introduced, and understands content measurement and using method.
(3) carry out the exercise of flight operation module, instrument monitoring module, two task module, be familiar with using method.
(4) have a rest 2 minutes, prepare official testing
(5) official testing of 8 groups of flight operation modules of carrying out lasting 2 hours, instrument monitoring module, two task module, brings out for carrying out fatigue.
(6) test in every 15 minutes, have a rest 90 seconds.
Fatigue brings out the monitoring of process, specifically comprises two modules.
1, flight simulation implements the immediately monitoring module of state
While experimenter carries out the use of flight simulation subject, researchist can monitor in the using state of server end to its seat in the plane.Comprise in this example: arrange three experimenter a, b, c, d, e, f distribute to three seat in the plane X1, X2, X3, Y1, Y2, Y3.Understand it whether to take a seat, whether normally log in.In test process, understand six experimenters and whether normally carry out testing, testing to proceed to which sequent modular.
2, the instant observation module of flight simulation subject achievement
Perform in flight operation simulation process experimenter, its each performance is monitored and record.Specifically comprise the monitoring of exercise flight operation analog module and test flight operation analog module in this example:
(2-1) the every Fixed Time Interval of modules flight operation task, the error that experimenter's operating lever operation produces
(2-2) modules flight operation task, changes in time, the curve map of operate miss change.
(2-3) modules instrument monitoring task, in Fixed Time Interval, during average correct response.
(2-4) modules instrument monitoring task, changes in time, curve map during average correct response.
(2-5) modules instrument monitoring task, in Fixed Time Interval, correct key number.
(2-6) modules instrument monitoring task, changes in time, the curve map of correct key number.
Flight simulation Report downloading and data analysis
After test terminates, can check and download the current report data completed, in the present embodiment,
(1) can with the form of compressed file to six experimenter a, the excel file of each self-forming of data of b, b compresses, and with the name of test time, preserves in the machine.
(2) result of everyone flight operation error is depicted as time dependent error change chart in the form of a graph, and convenient reproduction is pasted.
(3) the flight operation error result in everyone stipulated time is presented under curve map in digital form, and by copying the form of stickup, can be replicated in newly-built blank excel form, carrying out data analysis.
(4) change chart when result is depicted as time dependent average response in the form of a graph during everyone instrument monitoring correct average response, convenient reproduction is pasted.
(5) during the correct response of the instrument monitoring in everyone stipulated time, result is presented under curve map in digital form, and by copying the form of stickup, can be replicated in newly-built blank excel form, carrying out data analysis.
(6) the correct key number of everyone instrument monitoring is depicted as the change chart of time dependent correct number in the form of a graph, and convenient reproduction is pasted.
(7) result of the correct key number of the instrument monitoring in everyone stipulated time is presented under curve map in digital form, and by copying the form of stickup, can be replicated in newly-built blank excel form, carrying out data analysis.
Claims (4)
1., based on flight operation and the two task simulation system of instrument monitoring of flat gravity induction system, it is characterized in that, described pair of task simulation system comprises:
One, based on the flight simulation operating unit of panel computer gravity system,
Described flight simulation operating unit comprises:
(1-1) the flat gravity induction system flight operation module of bringing out
The real-time random variation representing heads up display in the display screen of panel computer is realized by this module, by using the function of dull and stereotyped gravity sensing system, at the operate tablet computer of three-dimensional perspective, produce the operation change of X-axis, Y-axis, Z axis, to correct the error that random disturbance produces, tester shows in the bidimensional change of flight operation panel board on computer screen by the operant response of gravity sensing system, thus adjusts, realize the effect of flight operation simulation smoothly
Instant random variation is produced in X-axis, Y-axis by following formula, the coordinate in each moment is made all on the basis of a upper moment coordinate, to produce not expected change in displacement, this random change in displacement constitutes the random disturbance for tester causes, and makes it produce deviation with balance reference position
Wherein,
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Make computing machine often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit;
(1-2) the flight monitoring module that brings out of dull and stereotyped visual presentation system
The real-time random variation of flight simulation warning meter lamp is represented in the display screen of panel computer, user monitors in real time by using the change of the touch screen function of panel computer to multiple flight simulation warning meter lamp, and require according to different sections object the judgement reaction carrying out button, the judgement of immediate feedback meter lamp is corrected errors, thus realizes the effect that meter lamp monitors in real time;
(1-3) the two task modules jointly presented are monitored in flight operation and flight
This module opens gravity sensing function and the touch-screen keypress function of panel computer simultaneously, represent the real-time random variation of heads up display and the real-time random variation of flight simulation warning meter lamp in the display screen of panel computer simultaneously, by using the gravity sensing system of panel computer, real-time correction is carried out to its change, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback is in the change of heads up display, thus realize the effect of flight operation simulation smoothly, simultaneously, monitor in real time by using the change of the touch screen function of panel computer to flight simulation warning meter lamp, and require according to different sections object the judgement reaction carrying out button, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, immediate feedback is corrected errors in the judgement of meter lamp, thus realize the effect that meter lamp monitors in real time,
Control lever task
The pitching of application dynamic menu simulated aircraft, roll attitude, participant's right hand single order controls the change of bidimensional:
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit, by adaptive mode, barre operation task sets different grade of difficulty, dynamic similation forms the random disturbance of grade of difficulty automatically, the change of grade of difficulty D, is reached by the value changing t, D=f (T), along with the reduction of chronomere T, grade of difficulty strengthens, and realizes the random disturbance of grade of difficulty, destroys the equilibrium state of instrument;
Two, the flight account design unit of computer server
Comprise:
2-1 arranges the task definition of flight simulation and the module of parameter
For arranging the described content based on all modules of the flight simulation operating unit of panel computer gravity system and parameter;
2-2, the duration that flight simulation is set and module sequentially
The duration presenting order and each module for arranging the described all modules based on the flight simulation operating unit of panel computer gravity system is arranged;
Three, participant's flight simulation environment for use administrative unit
Comprise:
The module of the environment for use of 3-1, construction experimenter flight simulation
For building and arrange the environment for use of experimenter,
The module of the seat in the plane of 3-2, distribution experimenter flight simulation
For distributing and select the seat in the plane of carrying out test of experimenter,
The module of the account of 3-3, management flight simulation researcher
The authority of on-the-spot research user is implemented for management organization flight simulation;
Four, the monitoring of flight simulation and data analysis unit
Comprise:
4-1, flight simulation implement the immediately monitoring module of state
During for carrying out the use of flight simulation subject experimenter, in the using state of server side to monitor experimenter,
The instant observation module of 4-2, flight simulation subject achievement
Perform in two task operating process experimenter, its each performance monitored and record,
4-3, flight simulation Report downloading and data analysis module
For the monitor data of real time inspection experimenter.
2. the flight operation based on flat gravity induction system according to claim 1 and the two task simulation unit of instrument monitoring, it is characterized in that, the flight simulation operating unit based on panel computer gravity system also comprises: module is introduced in rest module and/or test.
3. the flight operation based on flat gravity induction system according to claim 1 and the two task simulation system of instrument monitoring, it is characterized in that, the flight account design unit of described computer server also comprises the module of the programme arranging flight simulation,
Wherein, described program refers to that being arranged in section sometime carries out a certain specific activity, different program combination is produced the scheme of the two task operating of simulated flight of different demand.
4., based on flight operation and the two task simulation method of instrument monitoring of flat gravity induction system, it is characterized in that, said method comprising the steps of:
One, flight simulation operation is carried out based on panel computer gravity system,
Comprise:
(1-1) the real-time random variation representing heads up display in the display screen of panel computer is realized, by using the function of dull and stereotyped gravity sensing system, at the operate tablet computer of three-dimensional perspective, produce the operation change of X-axis, Y-axis, Z axis, to correct the error that random disturbance produces, tester shows in the bidimensional change of flight operation panel board on computer screen by the operant response of gravity sensing system, thus adjusts, realize the effect of flight operation simulation smoothly
Instant random variation is produced in X-axis, Y-axis by following formula, the coordinate in each moment is made all on the basis of a upper moment coordinate, to produce not expected change in displacement, this random change in displacement constitutes the random disturbance for tester causes, and makes it produce deviation with balance reference position
Wherein,
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Make computing machine often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit;
(1-2) in the display screen of panel computer, represent the real-time random variation of flight simulation warning meter lamp, user monitors in real time by using the change of the touch screen function of panel computer to multiple flight simulation warning meter lamp, and require according to different sections object the judgement reaction carrying out button, the judgement of immediate feedback meter lamp is corrected errors, thus realizes the effect that meter lamp monitors in real time;
(1-3) open gravity sensing function and the touch-screen keypress function of panel computer simultaneously, in the display screen of panel computer, represent the real-time random variation of heads up display and the real-time random variation of flight simulation warning meter lamp simultaneously.User by use panel computer gravity sensing system real-time correction is carried out to its change, the function of gravity sensing feeds back to the software systems of panel computer, immediate feedback is in the change of heads up display, thus realize the effect of flight operation simulation smoothly, simultaneously, user monitors in real time by using the change of the touch screen function of panel computer to flight simulation warning meter lamp and requires to carry out the judgement reaction of button according to different sections object, the inducing function of touch-screen is by the software systems feeding back to panel computer of user, immediate feedback is corrected errors in the judgement of meter lamp, thus realize the effect that meter lamp monitors in real time,
Control lever task
The pitching of application dynamic menu simulated aircraft, roll attitude, participant's right hand single order controls the change of bidimensional:
The compensatory tracking input equation of Y-axis is:
Y (t+1)=y (t)+Δ y (t+1)+r (t+1), wherein, the ordinate position of target when y (t) represents time t, the increment that when Δ y (t) represents time t, target obtains in the vertical direction, the random delta of r (t) for obtaining during t
The compensatory tracking input equation of the swing of X-axis and surface level is:
θ (t+1)=θ (t)+sign (t+1) × (Δ θ (t+1)+r (t+1) × 9), wherein sign (t+1) equals 1 or-1, the angle that θ (t) is target position during time t and horizontal direction; Increment when Δ θ (t) represents time t, angle obtained, the random delta of r (t) for obtaining during t, changes between (0,1),
Often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit, often through the T moment just in Y direction, and the angle direction of X-axis and level produces a stochastic variable in certain limit, by adaptive mode, barre operation task sets different grade of difficulty, dynamic similation forms the random disturbance of grade of difficulty automatically, the change of grade of difficulty D, reached by the value changing t, D=f (T), along with the reduction of chronomere T, grade of difficulty strengthens, realize the random disturbance of grade of difficulty, destroy the equilibrium state of instrument,
Two, design a calculating machine the flight subject of server
Comprise:
(2-1) task definition and the parameter of flight simulation are set,
The described content based on all modules of the flight simulation operating unit of panel computer gravity system and parameter are set,
(2-1) duration and the order of flight simulation are set
The duration presenting order and each module arranging the described all modules based on the flight simulation operating unit of panel computer gravity system is arranged;
Three, participant's flight simulation environment for use is managed
Comprise:
(3-1) environment for use of construction experimenter flight simulation,
(3-2) distribute the seat in the plane of experimenter's flight simulation, distribute and select the seat in the plane of carrying out test of experimenter,
(3-3) manage the account of flight simulation researcher, management organization flight simulation implements on-the-spot research user
Authority;
Four, flight simulation and data analysis is monitored
Comprise:
(4-1) immediately monitoring flight simulation implements state
When experimenter carries out the use of flight simulation subject, in the using state of server side to monitor experimenter,
(4-2) instant observation mould flight simulation subject achievement
Perform in two task operating process experimenter, its each performance monitored and record,
(4-3) flight simulation form and data analysis is downloaded, the monitor data of real time inspection experimenter.
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