CN117392898A - Flight view simulation training system based on HLA architecture - Google Patents

Flight view simulation training system based on HLA architecture Download PDF

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Publication number
CN117392898A
CN117392898A CN202311623355.1A CN202311623355A CN117392898A CN 117392898 A CN117392898 A CN 117392898A CN 202311623355 A CN202311623355 A CN 202311623355A CN 117392898 A CN117392898 A CN 117392898A
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flight
computer
software
hla
training
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徐晴晴
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Tianjin Jinhang Computing Technology Research Institute
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Tianjin Jinhang Computing Technology Research Institute
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Priority to CN202311623355.1A priority Critical patent/CN117392898A/en
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Abstract

The application provides a flight view simulation training system based on an HLA architecture, which comprises a master control device and a plurality of flight simulators, wherein each flight simulator comprises a hardware platform and a computer system, each hardware platform comprises a simulation seat assembly and a training helmet assembly, each simulation seat assembly is used for adapting to various types of aircrafts, and each training helmet assembly is used for simulating a flight training environment; the computer system is used for interacting with the training helmet assembly and the simulated seat assembly and cooperatively carrying out flight training; the master control device comprises an HLA architecture computer, HLA software is operated in the HLA architecture computer and used for enabling a plurality of flight simulators to perform information interaction; through the structure, the flight simulator adopts the universal simulation seat assembly, is suitable for various types of aircrafts, and has the advantages of small whole volume, low manufacturing cost and universality; meanwhile, HLA software is adopted to enable a plurality of flight simulators to perform multi-aircraft type air countermeasure.

Description

Flight view simulation training system based on HLA architecture
Technical Field
The application relates generally to the technical field of flight simulators, and in particular relates to a flight vision simulation training system based on an HLA architecture.
Background
The flight simulator mainly aims at training a pilot to achieve the purposes of testing the flight level of the pilot and keeping the pilot to the operation proficiency of the aircraft; the flight simulator is adopted for training, so that the running loss can be avoided, the training cost is greatly reduced, the time and space limitations are avoided, and the training efficiency is improved; in addition, the high-risk flight subject training can be performed, the safety is high, and the pilot is helped to establish flight confidence;
in the field of flight simulators, the mainstream flight simulators are mostly used for daytime training, and most of the mainstream flight simulators can only perform single-machine training and have certain limitations; the flight simulator mostly adopts an arc or spherical display screen and is additionally provided with an entity simulation cabin equal system, so that the whole volume of the flight simulator is huge and the manufacturing cost is high; moreover, as the entity cabin is adopted, a single flight simulator can only train aiming at one model, and certain limitation exists; in summary, the flight simulators in the prior art are limited to training for a fixed model in a visible light mode, so that a plurality of flight simulators cannot jointly perform multi-model air countermeasure.
Disclosure of Invention
In view of the foregoing drawbacks or shortcomings in the prior art, it is desirable to provide an HLA architecture-based flight view simulation training system that solves the foregoing technical problems.
The application provides a flight view simulation training system based on HLA framework, including: the master control device and the plurality of flight simulators;
the flight simulator comprises:
a hardware platform for simulating a cockpit of an aircraft, the hardware platform comprising a simulated seat assembly and a training helmet assembly; the simulated seat assembly is used for adapting to various types of aircrafts; the training helmet assembly is used for simulating a flight training environment;
the computer system is used for interacting with the training helmet assembly and the simulated seat assembly and performing flight training in a co-operation manner;
the master control device comprises an HLA architecture computer, HLA software is operated in the HLA architecture computer, and the HLA software is used for enabling a plurality of flight simulators to conduct information interaction.
According to the technical scheme that this application provided, training helmet assembly includes: helmet body, MR intelligent glasses, visible light camera, infrared camera, shimmer camera and headset, MR intelligent glasses are located the helmet body corresponds the position of human both eyes, MR intelligent glasses are used for showing virtual view and cabin; the visible light camera, the infrared camera and the low-light camera are all positioned at the positions of the helmet body corresponding to the forehead of the human body, the visible light camera is used for head tracking, the infrared camera is used for eye movement tracking, and the low-light camera is used for enhancing the positioning effect under low illumination aiming at night vision environment; the headset is used for communicating with other trained personnel.
According to the technical scheme provided by the application, the simulation seat assembly comprises: the device comprises a first platform, a seat, a steering column, an accelerator lever and pedals; the seat is arranged on the first platform, the steering column is located at one side armrest position of the seat along the first direction, the throttle lever is located at the other side armrest position of the seat along the first direction, and the foot pedal is located on the first platform and is located at one side far away from the seat back.
According to the technical scheme provided by the application, the computer system comprises: a visible light vision computer, a near infrared vision computer, a topography database computer, a cabin simulation computer, a instructor control computer, a flight and fire control simulation computer and a network switch; the visible light vision computer, the near infrared vision computer, the terrain database computer, the cabin simulation computer, the instructor control computer and the flight and fire control simulation computer are used for carrying out information interaction through the network switch.
According to the technical scheme provided by the application, the terrain database software is operated in the terrain database computer, and comprises the following components: various topography and topography data information.
According to the technical scheme provided by the application, the visible light view computer and the near infrared view computer operate view generation control software, the view generation and control software interacts with the terrain database software through the network switch, and the view generation and control software is used for calling the terrain data information to construct a virtual training scene, providing a visible light scene rendering mode and a near infrared scene rendering mode and simulating a real illumination environment.
According to the technical scheme provided by the application, the cabin simulation computer is operated with cabin display control software, and the cabin display control software is used for generating and controlling to switch simulated cabin environments of different models.
According to the technical scheme that this application provided, the operation has display processing software in the MR intelligent glasses, MR intelligent glasses with visible light camera, infrared camera, little light camera are connected, display processing software passes through the network switch with cabin display control software, vision generates and control software takes place information interaction, display processing software is used for showing and controlling virtual training scene and simulation cabin environment, and cooperates cabin display control tracks the hand action of discernment pilot.
According to the technical scheme provided by the application, the flight and fire control simulation computer runs flight and fire control simulation software, the flight and fire control simulation software interacts with the cabin display control software, the view generation and control software and the simulation seat assembly, and the flight and fire control simulation software is used for providing flight and fire control data for flight training.
According to the technical scheme provided by the application, the instructor control computer runs with instructor control software, the instructor control software and the display processing software, the view generation and control software, the cabin display control software and the flight and fire control simulation software are in information interaction, and the instructor control software is used for controlling and training management of the flight simulator by the instructor.
The beneficial effects of this application lie in:
the application provides a flight view simulation training system based on HLA framework, including: the flight simulator comprises a hardware platform and a computer system, wherein the hardware platform is used for simulating a cockpit of an aircraft, the hardware platform comprises a simulation seat assembly and a training helmet assembly, the simulation seat assembly is used for adapting to various aircraft types, and the training helmet assembly is used for simulating a flight training environment; the computer system is used for interacting with the training helmet assembly and the simulated seat assembly to perform flight training in a co-operation manner; the master control device comprises an HLA architecture computer, HLA software is operated in the HLA architecture computer and is used for enabling the flight simulators to conduct information interaction; through the structure, the flight simulator adopts the universal simulation seat assembly, is suitable for various types of aircrafts, and has the advantages of small whole volume, low manufacturing cost and universality; and meanwhile, the HLA software is adopted to enable a plurality of flight simulators to perform multi-aircraft type air countermeasure.
Drawings
Other features, objects and advantages of the present application will become more apparent upon reading of the detailed description of non-limiting embodiments, made with reference to the following drawings, in which:
FIG. 1 is a schematic diagram of an HLA architecture-based flight view simulation training system in the present application;
FIG. 2 is a schematic diagram of the computer system connections in the flight simulator of the present application;
FIG. 3 is a schematic view of a simulated seat assembly.
In the figure: 1. a flight simulator; 2. an HLA architecture computer; 3. a visible light view computer; 4. near infrared vision computer; 5. a terrain database computer; 6. a cockpit simulation computer; 7. a instructor control computer; 8. flight and fire control simulation computer; 9. MR intelligent glasses; 10. a network switch; 11. a first platform; 12. a seat; 13. a steering column; 14. and (5) pedaling.
Detailed Description
The present application is described in further detail below with reference to the drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be noted that, for convenience of description, only the portions related to the invention are shown in the drawings.
It should be noted that, in the case of no conflict, the embodiments and features in the embodiments may be combined with each other. The present application will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Example 1
Please refer to fig. 1 for a schematic diagram of a flight view simulation training system based on an HLA architecture provided in the present application, which includes: a master control device and a plurality of flight simulators 1;
the flight simulator 1 includes:
a hardware platform for simulating a cockpit of an aircraft, the hardware platform comprising a simulation seat 12 assembly and a training helmet assembly; the simulated seat 12 assembly is used to accommodate various models of aircraft; the training helmet assembly is used for simulating a flight training environment;
a computer system for interacting with the training helmet assembly and the simulated seat 12 assembly, together in coordination for flight training;
the master control device comprises an HLA architecture computer 2, HLA software is operated in the HLA architecture computer 2, and the HLA software is used for enabling a plurality of flight simulators 1 to conduct information interaction.
Specifically, the HLA software is used for simulating information interaction between the plurality of flight simulators 1 during formation training and countermeasure training; as shown in fig. 1, each flight simulator 1 is a federal member and added into federation to perform distributed simulation; supporting an RT I network through the HLA software to realize federal management service, statement management service, object management service and time management service; when a plurality of flight simulators 1 are trained in a combined mode, each federal member needs to initialize member data, and a federal data file is created, wherein the federal data file comprises simulation object simulation SOM and federal object model FOM, and the position and posture information of the flight simulators 1 needing interaction are covered; the federate members interact through the RT I, and after the members are connected to the RT I, the federate members are created and added; the federation member needs to publish/subscribe object class attribute to acquire other member information, register object instance, update object attribute when simulation is advanced, exit and cancel federation after simulation is finished;
working principle: the flight simulator 1 adopts a universal simulation seat 12 assembly, is suitable for various types of aircrafts, and has the advantages of small whole volume, low manufacturing cost and universality; and meanwhile, the HLA software is adopted to enable a plurality of flight simulators 1 to perform multi-aircraft type air countermeasure.
Further, the training helmet assembly includes: the helmet comprises a helmet body, MR intelligent glasses 9, a visible light camera, an infrared camera, a low-light camera and a headset, wherein the MR intelligent glasses 9 are positioned at positions of the helmet body corresponding to the eyes of a human body, and the MR intelligent glasses 9 are used for displaying virtual views and cabins; the visible light camera, the infrared camera and the low-light camera are all positioned at the positions of the helmet body corresponding to the forehead of the human body, the visible light camera is used for head tracking, the infrared camera is used for eye movement tracking, and the low-light camera is used for enhancing the positioning effect under low illumination aiming at night vision environment; the headset is used for communicating with other trained personnel.
Specifically, the training personnel comprises: a pilot and a trainer, the headset for communication between the pilot and the trainer;
specifically, the training helmet assembly includes: the helmet comprises a helmet body, MR intelligent glasses 9, a visible light camera, an infrared camera, a low-light camera and a headset, wherein the MR intelligent glasses 9 are free-form surface MR intelligent glasses 9 and are positioned at positions of the helmet body corresponding to eyes of a human body, and the MR intelligent glasses 9 are used for displaying virtual views and cabins; the visible light camera, the infrared camera and the low-light camera are all positioned at the position of the helmet body corresponding to the forehead of the human body, the visible light camera is used for head tracking, the infrared camera is used for eye movement tracking, and the low-light camera is used for enhancing the positioning effect under low illumination aiming at night vision environment; the MR intelligent glasses 9 are carried, the traditional giant curved surface screen and the traditional spherical screen are replaced, and the cabin is integrated in the virtual picture, so that the flight simulator is light in trend; meanwhile, the micro-light camera is added on the helmet body to help to sense and position in a dark environment, night vision training can be performed by combining near infrared vision pictures, and training types are enriched.
Further, the simulated seat 12 assembly includes: a first platform 11, a seat 12, a steering column 13, an accelerator lever and a foot pedal 14; the seat 12 is arranged on the first platform 11, the steering column 13 is positioned at one side armrest position of the seat 12 along the first direction, the throttle lever is positioned at the other side armrest position of the seat 12 along the first direction, and the foot pedal 14 is positioned on the first platform 11 and is positioned at one side far away from the backrest of the seat 12.
Specifically, as shown in FIG. 3, the simulated seat 12 assembly includes: the seat 12 is arranged on the first platform 11, the steering column 13 is positioned at one side armrest position of the seat 12 along the first direction, the throttle rod is positioned at the other side armrest position of the seat 12 along the first direction, in the embodiment, the steering column 13 is positioned at the right side of a human body, and the throttle rod is positioned at the left side of the human body; the foot rest 14 is positioned on the first platform 11 and is positioned on the side far away from the backrest of the seat 12; therefore, the cabin entity is simplified, and the use cost is reduced; and allows versatility to the simulated seat 12 assembly.
Further, the computer system includes: a visible light vision computer 3, a near infrared vision computer 4, a terrain database computer 5, a cabin simulation computer 6, an instructor control computer 7, a flight and fire control simulation computer 8 and a network switch 10; the visible light vision computer 3, the near infrared vision computer 4, the terrain database computer 5, the cabin simulation computer 6, the instructor control computer 7 and the flight and fire control simulation computer 8 are in information interaction through the network switch 10.
Specifically, as shown in fig. 2, the computer system includes: a visible light vision computer 3, a near infrared vision computer 4, a terrain database computer 5, a cabin simulation computer 6, an instructor control computer 7, a flight and fire control simulation computer 8 and a network switch 10; the visible light vision computer 3, the near infrared vision computer 4, the terrain database computer 5, the cabin simulation computer 6, the instructor control computer 7 and the flight and fire control simulation computer 8 are subjected to information interaction through the network switch 10; therefore, the cabin digital virtualization method and the cabin digital virtualization system realize the switching of various types of cabins by carrying out information interaction through software on the basis of the same set of hardware, improve reusability of the flight simulator 1 and enable training to be more diversified.
Further, the terrain database computer 5 is internally provided with terrain database software, and the terrain database software comprises: various topography and topography data information.
Specifically, the topographic database computer 5 is internally provided with topographic database software, and the topographic database software comprises various topographic data signals, and the topographic data information comprises three-dimensional terrains such as mountains, oceans, rivers, forests, grasslands, lakes and the like, and three-dimensional ground objects such as airports, villages, roads, bridges and the like; the construction of the terrain and the ground object comprises physical material information, and night vision simulation is supported.
Further, the visible light view computer 3 and the near infrared view computer 4 run view generation control software, the view generation and control software interacts with the terrain database software through the network switch 10, and the view generation and control software is used for calling the terrain data information to construct a virtual training scene, providing a visible light scene rendering mode and a near infrared scene rendering mode, and simulating a real illumination environment.
Specifically, the visible light view computer 3 and the near infrared view computer 4 run view generation control software, the view generation and control software transmits information interaction with the terrain database software through the network exchange stage, and the terrain database software mainly provides data support for the view generation and control software; the view generation and control software is used for calling the topographic and geomorphic data information, constructing a virtual training scene, providing a visible light scene rendering mode and a near infrared scene rendering mode, and simulating a real illumination environment; meanwhile, special effect simulation can be performed, including but not limited to smoke, flame and the like; the visible light vision computer 3 can simulate and output training scenes under all-weather various meteorological conditions; the near infrared vision computer 4 can simulate and output a scene picture observed at night through the night vision goggles; the pilot wears the MR intelligent glasses 9 to observe the simulation picture of the visible light vision computer 3, and also can switch and display the simulation picture of the near infrared vision computer 4, so as to train the night vision flight fight capability of the pilot.
Further, the cabin simulation computer 6 is operated with cabin display control software for generating and controlling switching of simulated cabin environments of different models.
Specifically, the cabin simulation computer 6 runs cabin display control software, and the cabin display control software performs information interaction with the view generation and control software; the cabin display control software can generate and control the switching of the simulated cabin environments of different types, establish and output three-dimensional cabin models of different types, render the real cabin environment and periodically update pictures according to actual conditions; therefore, the cabin is digitally virtualized, the switching of various types of cabins can be realized through software on the basis of the same set of hardware, reusability of the simulator is improved, and training is more diversified;
specifically, the cabin display control software performs information interaction with the instructor control software, the flight and fire control simulation software 13 and the display processing software, and the cabin display control software receives and processes the flight and fire control simulation software data information and displays corresponding flight data and symbols on a virtual cabin instrument, wherein the virtual cabin instrument comprises but is not limited to a head-up display, a multifunctional display, an instrument and a warning lamp; and meanwhile, the cockpit display control software receives and processes the display processing software data information and makes corresponding picture feedback according to pilot operation actions.
Further, display processing software is operated in the MR intelligent glasses 9, the MR intelligent glasses 9 are connected with the visible light camera, the infrared camera and the micro-light camera, the display processing software is in information interaction with the cockpit display control software and the view generation and control software through the network switch 10, and the display processing software is used for displaying and controlling the virtual training scene and simulating the cockpit environment and tracking and identifying the hand actions of a pilot by matching with the cockpit display control software.
Specifically, display processing software is run in the processor of MR intelligent glasses 9, MR intelligent glasses 9 with visible light camera, infrared camera, little light camera are connected, display processing software passes through network switch 10 with cabin display control software, vision generation and control software take place information interaction, display processing software is used for showing and controlling virtual training scene and simulation cabin environment to carry out data fusion to the information that the camera gathered and realize spatial location, in addition carry out manual tracking, eye movement tracking and gesture recognition when pilot and virtual cabin take place the interaction.
Further, the flight and fire control simulation computer 8 runs flight and fire control simulation software that interacts with the cockpit display control software, view generation and control software, and simulation seat 12 components, the flight and fire control simulation software being used to provide flight and fire control data for the flight training.
Specifically, the flight and fire control simulation computer 8 runs flight and fire control simulation software, and the flight and fire control simulation software interacts with the cabin display control software, the view generation and control software and the simulated seat 12 component; the flight and fire control simulation software provides flight and fire control data for flight simulation training, including but not limited to basic takeoff, aerial maneuver and landing simulation support, and makes corresponding roll, yaw, pitch and pitch responses for the operation of the pilot through the steering column 13, the throttle lever and the foot pedal 14; resolving aircraft flight waypoints, gestures, speeds and related fire control algorithms, including but not limited to continuously calculating a hit line ccil and continuously calculating a hit point CCIP; meanwhile, the flight and fire control simulation computer 8 transmits flight and fire control simulation data information to the cabin display software, and corresponding flight data and symbols are displayed on cabin instruments including, but not limited to, head up displays, multifunction displays, instruments, warning lamps, etc.
Furthermore, the instructor control computer 7 is operated with instructor control software, which interacts with the display processing software, the view generation and control software, the cockpit display control software and the flight and fire control simulation software, and the instructor control software is used for controlling and training the flight simulator by the instructor.
Specifically, the instructor control computer 7 runs instructor control software, and the instructor control software performs information interaction with the display processing software, the view generation and control software, the cabin display control software and the flight and fire control simulation software; the instructor control software is used for controlling and training and managing a single flight simulator 1 when running on the instructor control computer 7, and monitoring the hardware power-on and software running conditions of the flight simulator 1, wherein the training mode is single-machine training, and single-machine training subjects are loaded and configured;
specifically, the instructor control software may also run on the HLA architecture computer 2, and may perform status monitoring and management on the flight simulator 1 during the training mode, which may be a multi-machine formation training or a multi-machine countermeasure mode; the process control can be carried out on training subjects through the instructor control software, and the fault of the airplane and the training playback are set; process control content includes, but is not limited to, modifying training weather conditions, visible light, near infrared scene mode switching, scene freezing and thawing.
To facilitate understanding by those skilled in the art, the specific workflow is as follows:
the use environment of the training system can be set as a darkroom;
when the single machine training is carried out, firstly, the instructor control software on the instructor control computer 7 is started to carry out system power-up, then the model of the training aircraft is selected and the system is initialized, and after the system initialization is completed and in an operating state, the training subjects corresponding to the model are selected to start training; at this time, the MR intelligent glasses 9 display corresponding visual images and virtual cabins of training subjects, the pilot can operate the steering column 13, the throttle lever and the pedals 14 to perform flight training, and meanwhile, the pilot can also operate the virtual cabins and click keys or toggle switches, and the virtual cabins can give corresponding image feedback; during the training process, the instructor can change training time and meteorological conditions, and can also freeze the system, namely the system is in a pause state, and at the moment, the helmet display picture is frozen; in addition, the instructor can set different fault states of the carrier through instructor control software, and train the emergency processing capability of the pilot when facing the emergency; the instructor can synchronize the helmet display picture of the instructor to the console display of the instructor through the instructor control software, so that the instructor can conveniently control the whole training process; after training is finally completed, the training process can be played back, so that a series of flight operations are duplicated, and the pilot operation level is improved;
when multi-machine training is carried out, the instructor control software on the HLA architecture computer 2 is started to carry out system power-on all the flight simulators 1 connected to the network, then the machine type of each flight simulator 1 is designated and the system is initialized, the starting and the initialization of each flight simulator 1 are as described above, and after all the flight simulators 1 enter a normal running state, the HLA software is used for enabling each trained flight simulator 1 to enter federal to realize information interaction; the instructor control software on the HLA architecture computer 2 can control a plurality of flight simulators 1 to carry out formation flight training or countermeasure training, and control the addition or the withdrawal of federal members; a pilot can observe a formation member plane or an enemy plane in the visual field through the MR intelligent glasses 9; other training process control functions are consistent with those of stand-alone training.
The foregoing description is only of the preferred embodiments of the present application and is presented as a description of the principles of the technology being utilized. It will be appreciated by persons skilled in the art that the scope of the invention referred to in this application is not limited to the specific combinations of features described above, but it is intended to cover other embodiments in which any combination of features described above or equivalents thereof is possible without departing from the spirit of the invention. Such as the above-described features and technical features having similar functions (but not limited to) disclosed in the present application are replaced with each other.

Claims (10)

1. Flight view simulation training system based on HLA framework, characterized by comprising: a master control device and a plurality of flight simulators (1);
the flight simulator (1) comprises:
a hardware platform for simulating a cockpit of an aircraft, the hardware platform comprising a simulated seat assembly and a training helmet assembly; the simulated seat assembly is used for adapting to various types of aircrafts; the training helmet assembly is used for simulating a flight training environment;
the computer system is used for interacting with the training helmet assembly and the simulated seat assembly and performing flight training in a co-operation manner;
the master control device comprises an HLA architecture computer (2), HLA software is operated in the HLA architecture computer (2), and the HLA software is used for enabling a plurality of flight simulators (1) to conduct information interaction.
2. The HLA-architecture based flight view simulation training system of claim 1, wherein the training helmet assembly comprises: helmet body, MR intelligence glasses (9), visible light camera, infrared camera, shimmer camera and headset, MR intelligence glasses (9) are located the helmet body corresponds the position of human eyes, MR intelligence glasses (9) are used for showing virtual view and cabin; the visible light camera, the infrared camera and the low-light camera are all positioned at the positions of the helmet body corresponding to the forehead of the human body, the visible light camera is used for head tracking, the infrared camera is used for eye movement tracking, and the low-light camera is used for enhancing the positioning effect under low illumination aiming at night vision environment; the headset is used for communicating with other trained personnel.
3. The HLA-architecture based flight view simulation training system of claim 2, wherein the simulated seat assembly comprises: the device comprises a first platform (11), a seat (12), a steering column (13), an accelerator lever and a pedal (14); the seat (12) is arranged on the first platform (11), the steering column (13) is located at one side armrest position of the seat (12) along the first direction, the throttle lever is located at the other side armrest position of the seat (12) along the first direction, and the foot pedal (14) is located on the first platform (11) and is located at one side far away from the backrest of the seat (12).
4. A flight view simulation training system based on an HLA architecture of claim 3, wherein the computer system comprises: a visible light vision computer (3), a near infrared vision computer (4), a terrain database computer (5), a cabin simulation computer (6), an instructor control computer (7), a flight and fire control simulation computer (8) and a network switch (10); the visual light vision computer (3), the near infrared vision computer (4), the terrain database computer (5), the cabin simulation computer (6), the instructor control computer (7) and the flight and fire control simulation computer (8) are subjected to information interaction through the network switch (10).
5. The HLA architecture-based flight view simulation training system of claim 4, wherein a terrain database software is run in the terrain database computer (5), the terrain database software comprising: various topography and topography data information.
6. The flight view simulation training system based on the HLA architecture according to claim 5, wherein the visible light view computer (3) and the near infrared view computer (4) run view generation control software, the view generation and control software interacts with the terrain database software through the network switch (10), and the view generation and control software is used for calling the terrain data information, constructing a virtual training scene, providing a visible light scene rendering mode and a near infrared scene rendering mode, and simulating a real illumination environment.
7. The flight view simulation training system based on the HLA architecture as claimed in claim 6, wherein the cabin simulation computer (6) is operated with cabin display control software for generating and controlling switching of different model simulated cabin environments.
8. The flight view simulation training system based on the HLA architecture according to claim 7, wherein display processing software is operated in the MR intelligent glasses (9), the MR intelligent glasses (9) are connected with the visible light camera, the infrared camera and the micro-light camera, the display processing software is in information interaction with the cockpit display control software and the view generation and control software through the network switch (10), and the display processing software is used for displaying and controlling the virtual training scene and simulating cockpit environment and tracking and identifying hand actions of pilots in cooperation with the cockpit display control software.
9. The HLA architecture-based flight and vision simulation training system of claim 8, wherein the flight and fire simulation computer (8) is running flight and fire simulation software that interacts with the cabin display control software, vision generation and control software, and simulated seat components, the flight and fire simulation software being configured to provide flight and fire control data for the flight training.
10. The HLA architecture-based flight view simulation training system of claim 9, wherein the instructor control computer (7) is configured to run instructor control software, the instructor control software being in information interaction with the display processing software, the view generation and control software, the cockpit display control software, and the flight and fire control simulation software, the instructor control software being configured to provide an instructor with control and training management of the flight simulator.
CN202311623355.1A 2023-11-30 2023-11-30 Flight view simulation training system based on HLA architecture Pending CN117392898A (en)

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