CN115479499A - Airborne missile shooter training simulator - Google Patents
Airborne missile shooter training simulator Download PDFInfo
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- CN115479499A CN115479499A CN202211202403.5A CN202211202403A CN115479499A CN 115479499 A CN115479499 A CN 115479499A CN 202211202403 A CN202211202403 A CN 202211202403A CN 115479499 A CN115479499 A CN 115479499A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A33/00—Adaptations for training; Gun simulators
Abstract
The invention discloses an airborne missile shooter training simulator, belongs to the technical field of airborne missile weapon system training devices, and solves the technical problems of single function and insufficient training items of the existing airborne missile training simulator, and the specific technical scheme is as follows: the simulated carrying launching training cabin is basically the same as the plane missile launching cabin, the simulated carrying launching training cabin is fixed on the attitude six-axis control platform, the master console controls the attitude of the attitude six-axis control platform, the attitude six-axis control platform simulates a pilot to change the attitude of the plane, and different scenes are displayed according to different azimuth angles, pitch angles and roll angles by changing different attitudes.
Description
Technical Field
The invention belongs to the technical field of airborne missile weapon system training devices, and particularly relates to a shooter training simulator of an airborne missile weapon system.
Background
At present, airborne missile trainers are shooter training simulators of a single missile weapon system, the functions are single, different missile types need different shooter training simulators, integral and comprehensive training of the missile weapon system cannot be formed, and the development requirement of modern military warfare cannot be met, so that various types of airborne missile shooter training simulators need to be developed.
Disclosure of Invention
The invention aims to solve the technical problem of single function of the existing airborne missile training simulator and provides an airborne shooter training simulator of an airborne missile weapon system with comprehensive and vivid training.
In order to achieve the purpose, the technical scheme adopted by the invention is as follows: the airborne missile shooter training simulator comprises a simulated delivery launch training cabin and an attitude six-axis control platform, wherein the simulated delivery launch training cabin is basically the same as the airplane missile launch cabin, the simulated delivery launch training cabin is fixed on the attitude six-axis control platform, the attitude six-axis control platform simulates a pilot to change the attitude of the airplane, and different scenes are displayed according to different azimuth angles, pitch angles and roll angles.
And a sound system is arranged in the simulated carrying and launching training cabin and is used for simulating sound when the missile launches.
And a shooter training computer is arranged in the simulated carrier launch training cabin to simulate a target, and the processes of missile launch, missile trajectory processing and target tracking are completed.
A master control station is arranged in the simulated delivery launching training cabin, the master control station is a coach monitoring station and is installed on the right side of the simulated delivery launching training cabin, missile categories, training items, training scenes, training sites and network subsystems are arranged in the master control station, the network subsystems enable a shooter training computer to be communicated with a comprehensive training computer, the training scenes comprise day time, night time, sunny days and rainy days, and the training sites can call local landform scenes according to the set sites and are synthesized with targets.
A scene display is arranged in the simulated carrying emission training cabin, and a master console outputs a scene and a target.
A shooter training posture collector is arranged in the simulated carrying launching training cabin and used for collecting the azimuth angle, the pitch angle and the roll angle of the shooter training cabin.
The simulated carrier launch training cabin is internally provided with a scene, a sighting display, a missile launch control panel, a left handle, a right handle, a periodic rod and the like.
A signal acquisition electronic box is arranged in the simulated carrying emission training cabin.
The control panel transmits the control information to the signal acquisition electronic box through the RS-422 bus.
The periodic rod is in signal transmission with the signal acquisition electronic box through the I/O interface.
The information of the left handle of the shooter is sent to the right handle information acquisition board through a cable, and the information acquisition board of the right handle transmits the information with the signal acquisition electronic box through the RS-422 bus.
The left display screen of the shooter performs signal transmission with the signal acquisition electronic box through the RS-422 bus.
And the right display screen of the shooter performs signal transmission with the signal acquisition electronic box through an RS-422 bus.
And a power supply control system is arranged in the master console and is used for supplying power to all the devices.
The general control station is internally provided with a comprehensive training computer system, and the control station display is in signal transmission with the comprehensive training computer system.
The six-axis turntable controller is in signal transmission with the comprehensive training computer system through an RS-232 bus, and the six-axis turntable controller is in signal transmission with the attitude six-axis control platform.
The satellite receiver is in signal transmission with the comprehensive training computer system.
The screen display is in signal transmission with the comprehensive training computer system.
The sound system and the comprehensive training computer system carry out signal transmission.
The comprehensive training computer system and the shooter training computer system perform signal transmission, the shooter training computer system performs signal transmission with the signal acquisition electronic box, the shooter training computer system performs signal transmission with the right shooter display through the VGA cable, and the shooter training computer system performs signal transmission with the left shooter display through the VGA cable.
The master console controls the attitude state of the attitude six-axis control platform, and the scene displayer displays different scenes by changing different attitudes (changing the azimuth angle, the pitch angle and the roll angle of the training cabin).
The invention follows the training principle of fully closing to the actual assembly operation and closing to actual combat, and the overall layout on the structure of the simulated carrying launching training cabin is basically consistent with that of the actual assembly shooter cabin; the operation parts on the hardware are basically consistent with the actual installation; the battle position operation process, the scene interface feeling and the ballistic characteristics of the software are basically consistent with those of the actual installation.
The invention introduces the live-action map and provides a training configuration tool, so that a training unit can develop training subjects by self to meet the actual combat training requirement.
The invention solves the technical problem of single function of the existing missile trainer, can train a weapon system under indoor conditions, can be repeatedly trained and used, greatly saves the use and installation training cost, and has comprehensive system and vivid training.
Drawings
FIG. 1 is a schematic structural diagram of the present invention.
FIG. 2 is a diagram illustrating the connection relationship of electronic systems according to the present invention.
Fig. 3 is a diagram of the software architecture of the present invention.
Fig. 4 is a flowchart of basic tracking technique training.
Fig. 5 is a battlefield skill training flow chart.
In the figure, 1 is a simulated carrying and launching training cabin, and 2 is a posture six-axis control platform.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more clearly apparent, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1, the airborne missile shooter training simulator comprises a simulated carrier launch training cabin 1 and an attitude six-axis control platform 2, wherein the simulated carrier launch training cabin 1 is basically the same as the aircraft missile launch cabin, the simulated carrier launch training cabin 1 is fixed on the attitude six-axis control platform 2, the attitude six-axis control platform 2 simulates a pilot to change the attitude of the aircraft, and different scenes are displayed according to different azimuth angles, pitch angles and roll angles.
The simulated carrier launch training cabin 1 is internally provided with a sound system used for simulating sound when a guided missile launches.
A shooter training computer is arranged in the simulated carrier launch training cabin 1 to simulate a target, and the processes of missile launch, missile trajectory processing and target tracking are completed.
A master control station is arranged in the simulated carrying and launching training cabin 1 and is a coach monitoring station, the master control station is installed on the right side of the simulated carrying and launching training cabin, missile categories, training items, training scenes, training places and a network subsystem are arranged in the master control station, the network subsystem is used for realizing communication between a shooter training computer and a comprehensive training computer, the training scenes comprise day, night, sunny days and rainy days, and the training places can call local landform scenes according to the set places and are synthesized with targets.
A large-screen scene display is arranged in the simulated carrying and launching training cabin 1, and a scene and a target are output by a master console.
A shooter training posture collector is arranged in the simulated carrying launching training cabin 1 and is used for collecting the azimuth angle, the pitch angle and the roll angle of the shooter training cabin.
The simulated carrier launch training cabin 1 is internally provided with a scene, a sighting display, a missile launch control panel, a left handle, a right handle, a periodic rod and the like.
As shown in fig. 2, a signal acquisition electronic box is arranged in the simulated carrying emission training cabin 1.
The control panel transmits the control information to the signal acquisition electronic box through the RS-422 bus.
The state information of the periodic rod is sent into the signal acquisition electronic box through a cable to be processed.
The information of the left handle of the shooter is sent to the right handle information acquisition board through a cable, and the information acquisition board of the right handle transmits the information with the signal acquisition electronic box through an RS-422 bus.
And 20 keys are arranged around the left display of the shooter, and the left display screen of the shooter performs signal transmission with the signal acquisition electronic box through an RS-422 bus.
And 20 keys are arranged on the periphery of the right display of the shooter, and the right display screen of the shooter performs signal transmission with the signal acquisition electronic box through an RS-422 bus.
The left display of the shooter, the right display of the shooter, the power switch and the state information of the character switch are collected by respective information collecting boards and are sent into the signal collecting electronic box through an RS-232 bus.
And a power supply control system is arranged in the master console and is used for supplying power to all the devices.
The general control station is internally provided with a comprehensive training computer system, and the control station display is in signal transmission with the comprehensive training computer system.
The six-axis turntable controller is in signal transmission with the comprehensive training computer system through an RS-232 bus, and the six-axis turntable controller is in signal transmission with the attitude six-axis control platform.
The satellite receiver and the comprehensive training computer system perform signal transmission.
The screen display is in signal transmission with the comprehensive training computer system.
The sound system and the comprehensive training computer system carry out signal transmission.
The comprehensive training computer system and the shooter training computer system perform signal transmission, the shooter training computer system performs signal transmission with the signal acquisition electronic box, the shooter training computer system performs signal transmission with the right shooter display through the VGA cable, and the shooter training computer system performs signal transmission with the left shooter display through the VGA cable.
The master control console controls the attitude state of the attitude six-axis control platform 2, and the scene display displays different scenes by changing different attitudes (changing azimuth angle, pitch angle and roll angle of the training cabin).
The information of each part is sent into the signal acquisition electronic box for 1 time every 50ms, the signal acquisition electronic box packs all the information, and the information is sent into the shooter training computer system for 1 time every 50 ms; the shooter training computer system and the comprehensive training computer system perform information interaction through a network.
The comprehensive training computer system sends the flight simulating parameter curve to the six-axis turntable controller according to the training requirement, the six-axis turntable controller controls the posture six-axis control platform to perform various actions according to the flight simulating parameter curve, and the posture angle of the shooter training cabin is fed back to the shooter training computer through the posture sensor, so that the stability of the shooter training cabin is ensured.
When a training place is set, the comprehensive training computer system receives a topographic map of the place through the satellite map APP, and synthesizes the map and a target to provide a training scene for use. The console display and the large screen display information are provided by the integrated training computer system.
The sound of the sound system is the sound simulating the launching process of the missile.
The power management system detects and stabilizes 220V alternating current, and automatically adjusts the output of the alternating current when the alternating current rises or falls, so as to always ensure that the alternating current output voltage is within 200V +/-2%.
As shown in fig. 3, the software of the present invention includes two major types, one type is upper computer software, and includes two types, i.e., comprehensive training software and shooter launching training software, which are run on Win7 and 64-bit operating systems and are developed by using a Unity3D three-dimensional engine through C # language. The second type is embedded software which is used for a signal acquisition board and provides operating signals of operators for signal acquisition board software, comprehensive training software and shooter launching training software.
The working process of the invention is as follows:
logging in a master control console, and selecting the type, air-ground and missile model of the missile;
selecting training subjects, wherein the training subjects comprise basic tracking skill training, operation skill training, team cooperation training, training places, training environments, training personnel and targets (airplanes, tanks, motor vehicles, fixed targets and the like).
1. And selecting a simulated shooter training table of a shooter training simulator for performing basic tracking technique training.
2. The six-axis turntable controller (simulating a driver) automatically adjusts the posture of the six-axis control platform 2 according to a turntable instruction given by the comprehensive training computer system, so that the included angle between the training cabin and the target is within +/-15 degrees.
The basic follow-up maneuver training is shown in FIG. 4.
3. And selecting to enter a battle position operation skill training, wherein a shooter battle position of a shooter training simulator and a six-axis turntable controller (a simulation driver) automatically adjust the posture six-axis control platform 2 according to a turntable instruction given by a comprehensive training computer system, so that an included angle between a training cabin and a target is within +/-10 degrees, and the battle position operation skill training is carried out.
The activities of the battlefield operation skill training are shown in fig. 5.
After training begins, a shooter training cabin 1 of the airborne shooter training simulator, a console display and a large screen display enter a training interface, and the operation method, program and requirements of the shooter training are consistent with those of the actual installation operation. After the training is finished, the master console finishes the training in a unified way, a score report is displayed on the master console, and the training process is directly stored in the master console and can be played back.
The simulated carrying and launching training cabin 1 adopts a semi-open layout, is convenient for a coach to supervise and other personnel to watch and study, the layout of internal equipment is basically consistent with the actual installation, and a main control console adopts a standard control console.
The invention follows the training principle of fully closing to the actual assembly operation and closing to the actual combat, and the overall layout of the simulated carrying launching training cabin 1 is basically consistent with that of the actual assembly shooter cabin; the operating parts on the hardware are basically consistent with the actual installation; the battle position operation process, the scene interface feeling and the ballistic characteristics of the software are basically consistent with those of the actual installation.
The invention introduces the live-action map and provides a training configuration tool, so that a training unit can develop training subjects by self to meet the actual combat training requirement.
The invention solves the technical problem of single function of the existing missile trainer, has the advantages of carrying out weapon system training under indoor conditions, being capable of repeatedly training and using, greatly saving the use and installation training cost, having comprehensive system and vivid training.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principles of the present invention are intended to be included therein.
Claims (2)
1. The airborne missile shooter training simulator is characterized by comprising a simulated carrier launch training cabin and an attitude six-axis control platform, wherein the simulated carrier launch training cabin is fixed on the attitude six-axis control platform, and the attitude six-axis control platform changes the azimuth angle, the pitch angle and the roll angle of the simulated carrier launch training cabin;
a sound system is arranged in the simulated carrying and launching training cabin and used for simulating sound when the missile launches;
a shooter training computer is arranged in the simulated carrying launching training cabin to realize target simulation;
a master control station is arranged in the simulated delivery launch training cabin, the master control station is installed on the right side of the simulated delivery launch training cabin, and missile categories, training items, training scenes, training sites and network subsystems are arranged in the master control station;
a scene display is arranged in the simulated carrying and launching training cabin, and a master console outputs a scene and a target;
a shooter training posture collector is arranged in the simulated carrying and launching training cabin and used for collecting the azimuth angle, the pitch angle and the roll angle of the shooter training cabin;
and the simulated carrying launching training cabin is internally provided with an aiming display, a missile launching control panel, a left handle, a right handle and a periodic rod.
2. The simulated launch vehicle according to claim 1, wherein said simulated launch vehicle has a signal acquisition electronics box;
the control information of the control panel is in signal transmission with the signal acquisition electronic box through the RS-422 bus;
the periodic rod is in signal transmission with the signal acquisition electronic box through the I/O interface;
control information of the left handle of the shooter is sent to the right handle information acquisition board through a cable, and the control information is transmitted to the signal acquisition electronic box through the RS-422 bus by the right handle information acquisition board;
the left display screen of the shooter performs signal transmission with the signal acquisition electronic box through an RS-422 bus;
the right display screen of the shooter performs signal transmission with the signal acquisition electronic box through an RS-422 bus;
the general control console is internally provided with a comprehensive training computer system, and a console display and the comprehensive training computer system perform signal transmission;
the six-axis rotary table controller transmits signals with the comprehensive training computer system through an RS-232 bus, and transmits signals with the posture six-axis control platform;
the satellite receiver and the comprehensive training computer system carry out signal transmission;
the screen display and the comprehensive training computer system perform signal transmission;
the sound system and the comprehensive training computer system carry out signal transmission;
the comprehensive training computer system and the shooter training computer system perform signal transmission, the shooter training computer system performs signal transmission with the signal acquisition electronic box, the shooter training computer system performs signal transmission with the right shooter display through the VGA cable, and the shooter training computer system performs signal transmission with the left shooter display through the VGA cable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211202403.5A CN115479499A (en) | 2022-09-29 | 2022-09-29 | Airborne missile shooter training simulator |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211202403.5A CN115479499A (en) | 2022-09-29 | 2022-09-29 | Airborne missile shooter training simulator |
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| CN115479499A true CN115479499A (en) | 2022-12-16 |
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| CN202211202403.5A Pending CN115479499A (en) | 2022-09-29 | 2022-09-29 | Airborne missile shooter training simulator |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20050023714A (en) * | 2003-09-02 | 2005-03-10 | 주식회사 유니텍 | Simulator of armoured vehicle for an amphibious |
| US20100092926A1 (en) * | 2008-10-14 | 2010-04-15 | Haywood Keith Fabling | Flight crew training system |
| CN202632580U (en) * | 2012-03-07 | 2012-12-26 | 北京欣远诚业科技有限公司 | Integrated training simulator of flight and ejector of airplane |
| KR20150061913A (en) * | 2013-11-28 | 2015-06-05 | 삼성탈레스 주식회사 | System for verifying aircraft target training controller and method for operating the same |
| CN107293177A (en) * | 2017-08-15 | 2017-10-24 | 科盾科技股份有限公司北京分公司 | A kind of analogue simulation trainer |
-
2022
- 2022-09-29 CN CN202211202403.5A patent/CN115479499A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20050023714A (en) * | 2003-09-02 | 2005-03-10 | 주식회사 유니텍 | Simulator of armoured vehicle for an amphibious |
| US20100092926A1 (en) * | 2008-10-14 | 2010-04-15 | Haywood Keith Fabling | Flight crew training system |
| CN202632580U (en) * | 2012-03-07 | 2012-12-26 | 北京欣远诚业科技有限公司 | Integrated training simulator of flight and ejector of airplane |
| KR20150061913A (en) * | 2013-11-28 | 2015-06-05 | 삼성탈레스 주식회사 | System for verifying aircraft target training controller and method for operating the same |
| CN107293177A (en) * | 2017-08-15 | 2017-10-24 | 科盾科技股份有限公司北京分公司 | A kind of analogue simulation trainer |
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Address after: 030003 No. 86, Yangxing South Street, Zhongbei High tech Industrial Development Zone, Taiyuan City, Shanxi Province Applicant after: SHANXI HUAYANG JILU TECHNOLOGY CO.,LTD. Address before: No.86, Yangxing South Street, Taiyuan Stainless Steel Industrial Park, Shanxi Province 030003 Applicant before: SHANXI HUAYANG JILU TECHNOLOGY CO.,LTD. |