CN103760780A - Universal simulation platform of cockpit display control system - Google Patents
Universal simulation platform of cockpit display control system Download PDFInfo
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- CN103760780A CN103760780A CN201410053394.7A CN201410053394A CN103760780A CN 103760780 A CN103760780 A CN 103760780A CN 201410053394 A CN201410053394 A CN 201410053394A CN 103760780 A CN103760780 A CN 103760780A
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Abstract
The invention discloses a universal simulation platform of a cockpit display control system. The universal simulation platform of the cockpit display control system comprises a cockpit mechanical structure subsystem, a display control unit, a control mechanism and half-entity interface subsystem, a management and monitoring system, a software system module, an audio system, and a computer network and optical fiber signal transmission system. Through combination of the above modules, the simulation platform of the cockpit display control system has the advantages of being capable of being reconstructed, simple in structure, high in universality, high in performance-price ratio and the like. Each part is designed according to the modularized design thought and each module is provided with an independent function and a good connection interface, so that strong combination ability is achieved. A functional hierarchical structure is adopted for the software system so that higher transportability, higher configurability, and higher extensibility can be achieved.
Description
[technical field]
The present invention relates to a kind of emulation platform, particularly the aobvious control of general passenger cabin system simulation platform.
[background technology]
Aircraft cockpit is the main activities place of pilot while carrying out aerial mission.Pilot must rely on sweep out of my cabin, the demonstration of cabin internal information and self proprioception etc. to obtain all kinds of flight informations, by each quasi-controller in passenger cabin, handles and control aircraft.In recent years, along with the develop rapidly of display device and display technique, passenger cabin aobvious control device layout and function realize larger change.At present, the development and research of aviation operating platform of new generation main with show that information requirement, information display format, passenger cabin software interface, pilot's context-aware, personnel's decision-making are auxiliary, the problem such as passenger cabin operation automation, fly guiding and control, command input device is relevant.
Traditionally, the development of new model, new product, all will first produce many model machines, makes a service test or takes a flight test, and this kind the mode test period is long, cost is large.Along with infotech, the particularly fast development of computer technology, computer networking technology, graph and image processing technology, the information processing technology etc., the beforehand research that makes people to carry out new projects by the method for modeling and simulation is developed, thereby greatly reduces cost, has improved work efficiency.Because general flight simulation platform can carry out engineering and operation use research, there is the features such as high-level efficiency, high benefit, be subject to the great attention of countries in the world always.
[summary of the invention]
The object of the present invention is to provide the aobvious control of a kind of general passenger cabin system simulation platform.
For achieving the above object, implement the aobvious control of general passenger cabin of the present invention system simulation platform and comprise passenger cabin mechanical framework subsystem, aobvious control unit, catanator and half interface subsystem in kind, management monitoring system, software system module, sound system and computer network and fiber-optic signal transmission system, wherein:
Passenger cabin mechanical framework subsystem, adopts open cockpit structure, and cockpit structure adopts modular form setting;
Aobvious control unit, comprises helmet-mounted display system, the man-machine interaction subsystem based on touch-screen and cockpit instrument emulation and display subsystem;
Catanator and half interface subsystem in kind, comprise a plurality of simulations, and obtain input signal by sensor, then be connected with interface computer by the interface on embedded data acquisition card;
Management monitoring system, provides management, setting, the monitoring interface of cockpit display research environment, realizes the operational management function of the detection of system equipment, the monitoring of the function setting of realistic model, system state and model parameter and whole system;
Software system module, comprises flight course simulation unit and what comes into a driver's unit;
Sound system, receives the real-time flight status data that comes from flight simulation computing machine, from voice data element corresponding to voice data library lookup, synthesizes the various sound that can hear in true aircraft cockpit;
Computer network and fiber-optic signal transmission system, whole interface between software and hardware and transfer function have been contained, by data acquisition equipment, parameter is inputed to interface computer, interface computer is distributed to other unit after the data of a plurality of equipment in kind are merged on timing node.
According to above-mentioned principal character, this passenger cabin mechanical framework subsystem comprises passenger cabin mechanical framework, what comes into a driver's supporting frame, the technique framework of supporting instrument to show front panel and both sides instrument panel.
According to above-mentioned principal character, cockpit instrument emulation and the display subsystem emulation demonstration control instrument relevant to flight management of aobvious control unit, employing is by the instrument picture of computer software generating virtual, and use touch-screen to carry out man-machine interaction, and man-machine interaction subsystem based on touch-screen is by the employing high precision that is arranged on front panel and the both sides control panel of aircraft cockpit, the band touch screen LCD of high stable generates by concrete picture, all kinds of switches on it, button, the operation of knob etc. all realizes by touch-screen, analyze movement characteristic and the kinematic constraint of staff, set up corresponding motor pattern model, by to input data time sequential analysis, identify user's operational motion, in the operation response time, image frame changes cooperation, the aspects such as Tip Sound, accomplish organic coordination, helmet-mounted display system can be realized a kind of immersion interactive environment, by the object interaction effect in physical environment and virtual environment, influence each other, impression and the experience that is equal to true environment is come in generation personally.
According to above-mentioned principal character, catanator and half interface subsystem in kind comprise the simulations such as jociey stick, pedal, throttle control handle, and obtain input signal by related sensor, then by Ethernet interface on embedded data acquisition card, be connected with interface computer.
According to above-mentioned principal character, management monitoring system comprises that system management module, hardware operational management monitoring module, flight and environmental parameter arrange module, monitoring and additional information display module, wherein system management module detects and manages the state of simulated environment unit and subsystem, the main software and hardware running status of each unit is shown in patterned mode, can carry out power on, power-off, start, close, the operation such as communication; Hardware operational management monitoring module, to after unit startup normal operation, is set according to present mode of operation, flight and environmental parameter, and operation starts/freezes/continue/end; System is supported simulation run and two kinds of patterns of playback operation, and simulation run will access main analogue system and other specify Aerial Electronic Equipment, and playback operation is carried out system playback according to the data content of preserving; Under default setting, once operation in simulation run pattern starts data recording; Flight and environmental parameter arrange module in order under simulation run pattern, and the model parameter of this emulation is set, and mainly comprise aircraft self parameter, flight parameter, environmental parameter etc.; Software provides a default set of setting parameter while installing; Once setting, the starting condition of this emulation is determined accordingly; Monitoring and additional information display module, when simulation run, carry out implementing monitoring and check the setting of flight performance parameter and state of flight, flying condition etc., check various ways such as adopting data, curve, explanatory note, map.
According to above-mentioned principal character, the flight course simulation unit of software system module comprises main emulation module, helmet display module, instrument and aobvious control module, administration module, modules all can provide external data-interface and video interface, main emulation module is responsible for settling accounts flying simulation model, model clearing are according to current state of flight and setting, calculate next state of flight constantly, state of flight is distributed to the helmet to be shown, instrument and aobvious control and what comes into a driver's module, instrument adopts touch screen display mode with aobvious control module, in natural mode, carry out state setting, these set informations return to main emulation module, instrument can be edited and reconstruct according to aerial mission or user of service's demand with aobvious control module, to reset instrument and aobvious control interface.
Compared with prior art, implement restructural passenger cabin environment of the present invention and there is restructural, simple in structure, highly versatile, personality cost ratio high, each several part is all carried out design effort according to modular design philosophy, each module has independently function and good connecting interface, has stronger combination ability; Software systems adopt functional stratification structure, have higher portability, configurability and extendability.
[accompanying drawing explanation]
Fig. 1 forms modular structure figure for implementing the system of the aobvious control of general passenger cabin of the present invention system simulation platform.
[embodiment]
Refer to shown in Fig. 1, for implementing the system of the aobvious control of general passenger cabin of the present invention system simulation platform, form modular structure figure, implement the aobvious control of general passenger cabin of the present invention system simulation platform and comprise passenger cabin mechanical framework subsystem, aobvious control unit, catanator and half interface subsystem in kind, management monitoring system, software system module, sound system and computer network and fiber-optic signal transmission system, below the composition of each module and function are elaborated.
Passenger cabin mechanical framework subsystem comprises passenger cabin mechanical framework, what comes into a driver's supporting frame, the technique framework of supporting instrument to show front panel and both sides instrument panel.This subsystem adopts open cockpit structure, and cockpit structure adopts modular form, is easy to assembling and dismounting, has good maintainability.The representative advanced military cockpit of take is reference, take steel construction as core, and curve special partly adopts forming process of glass fiber reinforced plastics to complete, and has enough physical strengths, and body structure surface sophisticated technologies are attractive in appearance.
Aobvious control unit comprises helmet-mounted display system, the man-machine interaction subsystem based on touch-screen and cockpit instrument emulation and display subsystem, wherein cockpit instrument emulation and the display subsystem emulation demonstration control instrument relevant to flight management, employing is by the instrument picture of computer software generating virtual, and use touch-screen to carry out man-machine interaction, there is dirigibility, can again customize according to the requirement of concrete aircraft.And man-machine interaction subsystem based on touch-screen is by the employing high precision that is arranged on front panel and the both sides control panel of aircraft cockpit, the band touch screen LCD of high stable generates by concrete picture, all kinds of switches on it, button, the operation of knob etc. all realizes by touch-screen, analyze movement characteristic and the kinematic constraint of staff, set up corresponding motor pattern model, by to input data time sequential analysis, identify user's operational motion, in the operation response time, image frame changes cooperation, the aspects such as Tip Sound, accomplish organic coordination, make the response obtaining there is the enough sense of reality.Helmet-mounted display system can be realized a kind of immersion interactive environment, by the object interaction effect in physical environment and virtual environment, influence each other, thereby produce, comes to impression and the experience that is equal to true environment personally, and Helmet Mounted Display is selected the video perspective type helmet.
Catanator and half interface subsystem in kind comprise jociey stick (aileron and horizontal tail), pedal (yaw rudder), throttle control handle is simulation, and obtains input signal by related sensor, by Ethernet interface on embedded data acquisition card, be connected with interface computer again; Jociey stick adopts side lever form.
Management monitoring system is in order to provide advanced cockpit to show management, setting, the monitoring interface of research environment, realize the operational management function of the detection of system equipment, the monitoring of the function setting of realistic model, system state and model parameter and whole system, comprise that system management module, hardware operational management monitoring module, flight and environmental parameter arrange module, monitoring and additional information display module.Wherein system management module detects and manages the state of simulated environment unit and subsystem, the main software and hardware running status of each unit is shown in patterned mode, can carry out power on (for main hardware equipment), power-off (for main hardware equipment), start, close the operations such as communication.Hardware operational management monitoring module, to after unit startup normal operation, is set according to present mode of operation, flight and environmental parameter, and operation starts/freezes/continue/end; System is supported simulation run and two kinds of patterns of playback operation, and simulation run will access main analogue system and other specify Aerial Electronic Equipment, and playback operation is carried out system playback according to the data content of preserving; Under default setting, once operation in simulation run pattern starts data recording.Flight and environmental parameter arrange module in order under simulation run pattern, and the model parameter of this emulation is set, and mainly comprise aircraft self parameter, flight parameter, environmental parameter etc.; Software provides a default set of setting parameter while installing; Once setting, the starting condition of this emulation is determined accordingly.Monitoring and additional information display module, when simulation run, carry out implementing monitoring and check the setting of flight performance parameter and state of flight, flying condition etc., check various ways such as adopting data, curve, explanatory note, map.
Software system module comprises flight course simulation unit and what comes into a driver's unit.Wherein flight course simulation unit comprises main emulation module, helmet display module, instrument and aobvious control module, administration module, and modules all can provide external data-interface and video interface.Main emulation module is responsible for settling accounts flying simulation model, and model is settled accounts according to current state of flight and setting, calculates next state of flight constantly, and state of flight is distributed to helmet demonstration, instrument and aobvious control and what comes into a driver's module.Instrument adopts touch screen display mode with aobvious control module, in natural mode, carries out state setting, and these set informations return to main emulation module; Instrument can be edited and reconstruct according to aerial mission or user of service's demand with aobvious control module, to reset instrument and aobvious control interface.
Main emulation module comprises flight dynamics kinematics model, flight control model and fire control model.Aircraft dynamics kinematics module is the nucleus module of flight Simulation System model, for navigation part, Flight Control Section provide source data, and with these module composition closed loops, reach real simulation and take off, landing, the overall process of airflight.The Module Division of flight dynamics inside is Pneumatic module, equation of motion module, undercarriage wind tunnel, ground wind tunnel module, power system module, parameter setting module, malfunctioning module.
In simulated dynamics computation process, flight dynamics part is mainly to receive the operating surface position providing from flight control system module, throttle position, the wing flap that hydraulic system module provides and undercarriage position and folding and unfolding sign, the atmospheric environment of atmospheric engine output, the thrust output of engine, fuel oil, the structural parameters such as load, the various Aircraft Targets parameters that the output parameter of ground model and avionics control system and trainer set, aircraft instruction etc.
Fire control model is comprised of a plurality of modules: the module of taking off, course line module, flight module, search module, fistfight module, missile attack module, (water) face is attacked module, projectile weapon and attacked module, landing module, shooting and aim at correction angle calculating, radar simulation signal, dispersion probability, deviation computing module, favourable shooting checking module, hit condition and hit rate calculation procedure over the ground.
Helmet display module comprises that Camera obtains the fusion of reality scene, video detection, head movement tracking, man-machine interaction, virtual scene generation, actual situation scene and shows several parts.Camera obtains the fusion of reality scene, video detection, virtual scene generation, actual situation scene and shows that all a minute images of left and right eyes two-way carries out, finally the scene of left eye can be presented on the display screen that left eye is corresponding, right eye scene is presented on the display screen that right eye is corresponding, realizes 3 D stereo show with this.
Instrument, is not changing under the condition of hardware with patterned way simulation conventional instrument and maneuvering device with aobvious control module, can realize the rapid emulation of different existing type passenger cabin man-machine interfaces by easy configuration.Use the up-to-date interface instrument WPF of Microsoft company, make the control part of front top plate, rear top board and front electronic instrument panel.The design of aobvious control part adopts the up-to-date design concept of MVVM to control part and realizes.All panel controls are divided into input class and output class, and input class comprises electric switch, rotary switch, knob, test electric switch, digital input keyboard, button etc., and output class comprises dial plate, pilot lamp, electron display tube etc.In order to realize editor's recombination function, need possess following key element: fundamental element storehouse (character repertoire, icon library, display element, element descriptive model), display module editing machine (extract the element in basic display element database, form a display module), display layout's editing machine (is combined in some assemblies in cockpit display region, and the driving variable structure of each assembly is integrated, form aircraft and show data-interface, this data-interface can achieve a butt joint with realistic model).
What comes into a driver's unit is by data management on a large scale and loading, realization is to the paging management of data on a large scale, the real-time loading of data block with remove, to reach, utilize in maximum efficiency storage space, easily terrain data is searched, load rapidly and remove, make scene picture not only true to nature but also smooth.It can complete following function:
(1) real-time rendering: the terrain data, sea and the airport model that load are carried out to real-time rendering, combine terrain data partition, continuous level detail model (CLOD) technology, Morphing technology etc., large-scale terrain is carried out to real-time rendering, give people's sensation on the spot in person, strengthen feeling of immersion, guarantee certain frame rate simultaneously.
(2) lamp light specific effect generates: airfield light, city light at night, dynamic lighting light etc. are carried out to emulation, to reach display effect true to nature.Dissimilar according to lamp, sets up the light source of respective type, and writes shader program to accepting the material that light source irradiates, and realizes by pixel and calculates illumination; For the light in city and the runway lights on airport, adopt the method for point range to generate.
(3) time change effect: can complete different natural time sky colors, the position of the Sun and the Moon, CF, the concentration calculating of mist etc., can accurate Calculation natural time, and calculating environment attribute according to current time, conversion ambient condition, realizes round-the-clock emulation.
Sound system receives the real-time flight status data that comes from flight simulation computing machine, from voice data element corresponding to voice data library lookup, synthesizes the various sound that can hear in true aircraft cockpit, the following a few class sound of main simulation:
A) engine noise: for the noise of (engine noise that takes off/normal cruise, aircraft landing engine reverse thrust system noise, engine failure noise etc.) aircraft engine under various conditions of work is carried out to emulation and output.
B) aerodynamic noise: under various conditions of work, the noise that in aircraft flight, air effect produces carries out emulation and output.
C) undercarriage action noise: for the noise of (gear up, gear down, undercarriage fault etc.) undercarriage under various conditions of work is carried out to emulation and output.
D) ground roll-out noise: under various conditions of work, in takeoff and landing process, the effect noise of wheel and ground runway carries out emulation and output.
E) thunderstorm neighbourhood noise: under various conditions of work, in the aircraft course of work, the noise of various weather, meteorological condition carries out emulation and output.
Computer network and fiber-optic signal transmission system have contained whole interface between software and hardware and transfer function (having non-relay).Equipment in kind inputs to interface computer by data acquisition equipment by parameter, and interface computer is distributed to other unit after the data of a plurality of equipment in kind are merged on timing node, and sound equipment and what comes into a driver's data guarantee that by fiber plant long-distance nondestructive transmits.
Compared with prior art, the present invention introduces advanced cockpit man-machine interface reconfiguration technique concept and open cockpit design theory first, cockpit display controlling equipment layout and screen display content are adopted to graphical symbol configuration mode flexibly, and use the man-machine interactive system based on touch-screen, reach and realize restructural convenience, highly versatile, object that configuration efficiency is high.Avionics interface editing and reconfiguration technique are mainly reflected in patterned way simulation conventional instrument and maneuvering device, are not changing under the condition of hardware, can realize the rapid emulation of different existing type passenger cabin man-machine interfaces by easy configuration.By the research to advanced cockpit man-machine interface reconfiguration technique, developed avionics interface editing and reconstructor, realized the configuration of graphical symbol flexibly to cockpit display controlling equipment layout and screen display content; By the graphic elements such as instrument, character, switch, button are configured, online editing to attributes such as display layout, form, tone, sizes, can again customize according to the requirement of concrete aircraft, arbitrary disposition, thereby meet the development mission requirements of Multiple Type operational aircraft.
And, the present invention introduces augmented reality virtual cockpit mentality of designing, adopts the see-through Helmet Mounted Display based on video, realizes the fusion of reality scene and virtual information, and present to user with 3 D stereo form, this mode has good virtual display effect and feeling of immersion.Augmented reality virtual technology and man-machine interface reconfiguration technique mutually combine, and can realize accurate aligning and the fusion of actual situation image.The virtual display technique of augmented reality based on the helmet is mainly obtained the fusion of reality scene, video detection, head movement tracking, man-machine interaction, virtual scene generation, actual situation scene and is shown several parts by Camera.According to the motion of user's head, come the position of viewpoint and the direction of sight line in real time altering virtual scene, realize dummy object and mate with the correct of real scene picture.Integrated Helmet Display System has been realized immersion interactive environment, the object interaction effect in physical environment and virtual environment, influences each other, thereby produce, comes to impression and the experience that is equal to true environment personally.
Be understandable that, for those of ordinary skills, can be equal to replacement or change according to technical scheme of the present invention and inventive concept thereof, and all these changes or replacement all should belong to the protection domain of the appended claim of the present invention.
Claims (6)
1. general passenger cabin shows a control system simulation platform, comprising:
Passenger cabin mechanical framework subsystem, adopts open cockpit structure, and cockpit structure adopts modular form setting;
Aobvious control unit, comprises helmet-mounted display system, the man-machine interaction subsystem based on touch-screen and cockpit instrument emulation and display subsystem;
Catanator and half interface subsystem in kind, comprise a plurality of simulations, and obtain input signal by sensor, then be connected with interface computer by the interface on embedded data acquisition card;
Management monitoring system, provides management, setting, the monitoring interface of cockpit display research environment, realizes the operational management function of the detection of system equipment, the monitoring of the function setting of realistic model, system state and model parameter and whole system;
Software system module, comprises flight course simulation unit and what comes into a driver's unit;
Sound system, receives the real-time flight status data that comes from flight simulation computing machine, from voice data element corresponding to voice data library lookup, synthesizes the various sound that can hear in true aircraft cockpit;
Computer network and fiber-optic signal transmission system, whole interface between software and hardware and transfer function have been contained, by data acquisition equipment, parameter is inputed to interface computer, interface computer is distributed to other unit after the data of a plurality of equipment in kind are merged on timing node.
2. the aobvious control of general passenger cabin as claimed in claim 1 system simulation platform, is characterized in that: this passenger cabin mechanical framework subsystem comprises passenger cabin mechanical framework, what comes into a driver's supporting frame, the technique framework of supporting instrument to show front panel and both sides instrument panel.
3. general passenger cabin as claimed in claim 1 shows control system simulation platform, it is characterized in that: cockpit instrument emulation and the display subsystem emulation demonstration control instrument relevant to flight management of aobvious control unit, employing is by the instrument picture of computer software generating virtual, and use touch-screen to carry out man-machine interaction, and man-machine interaction subsystem based on touch-screen is by the employing high precision that is arranged on front panel and the both sides control panel of aircraft cockpit, the band touch screen LCD of high stable generates by concrete picture, all kinds of switches on it, button, the operation of knob etc. all realizes by touch-screen, analyze movement characteristic and the kinematic constraint of staff, set up corresponding motor pattern model, by to input data time sequential analysis, identify user's operational motion, in the operation response time, image frame changes cooperation, the aspects such as Tip Sound, accomplish organic coordination, helmet-mounted display system can be realized a kind of immersion interactive environment, by the object interaction effect in physical environment and virtual environment, influence each other, impression and the experience that is equal to true environment is come in generation personally.
4. general passenger cabin as claimed in claim 1 shows control system simulation platform, it is characterized in that: catanator and half interface subsystem in kind comprise the simulations such as jociey stick, pedal, throttle control handle, and obtain input signal by related sensor, by Ethernet interface on embedded data acquisition card, be connected with interface computer again.
5. general passenger cabin as claimed in claim 1 shows control system simulation platform, it is characterized in that: management monitoring system comprises that system management module, hardware operational management monitoring module, flight and environmental parameter arrange module, monitoring and additional information display module, wherein system management module detects and manages the state of simulated environment unit and subsystem, the main software and hardware running status of each unit is shown in patterned mode, can carry out power on, power-off, start, close, the operation such as communication; Hardware operational management monitoring module, to after unit startup normal operation, is set according to present mode of operation, flight and environmental parameter, and operation starts/freezes/continue/end; System is supported simulation run and two kinds of patterns of playback operation, and simulation run will access main analogue system and other specify Aerial Electronic Equipment, and playback operation is carried out system playback according to the data content of preserving; Under default setting, once operation in simulation run pattern starts data recording; Flight and environmental parameter arrange module in order under simulation run pattern, and the model parameter of this emulation is set, and mainly comprise aircraft self parameter, flight parameter, environmental parameter etc.; Software provides a default set of setting parameter while installing; Once setting, the starting condition of this emulation is determined accordingly; Monitoring and additional information display module, when simulation run, carry out implementing monitoring and check the setting of flight performance parameter and state of flight, flying condition etc., check various ways such as adopting data, curve, explanatory note, map.
6. general passenger cabin as claimed in claim 1 shows control system simulation platform, it is characterized in that: the flight course simulation unit of software system module comprises main emulation module, helmet display module, instrument and aobvious control module, administration module, modules all can provide external data-interface and video interface, main emulation module is responsible for settling accounts flying simulation model, model clearing are according to current state of flight and setting, calculate next state of flight constantly, state of flight is distributed to the helmet to be shown, instrument and aobvious control and what comes into a driver's module, instrument adopts touch screen display mode with aobvious control module, in natural mode, carry out state setting, these set informations return to main emulation module, instrument can be edited and reconstruct according to aerial mission or user of service's demand with aobvious control module, to reset instrument and aobvious control interface.
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