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Laser-guided missile virtual test system and its construction method

A laser-guided and virtual test technology, applied in the field of virtual test, can solve the problems of not being independent, not easy to reuse, not easy to configure, etc., and achieve the effect of meeting real-time requirements and reducing dependence

Active Publication Date: 2017-11-03
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a laser-guided missile virtual test system and its construction method in order to solve the problems that each model is not independent, difficult to configure and difficult to reuse in the existing laser-guided missile virtual test system

Method used

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  • Laser-guided missile virtual test system and its construction method
  • Laser-guided missile virtual test system and its construction method
  • Laser-guided missile virtual test system and its construction method

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specific Embodiment approach 1

[0023] Specific implementation mode one: the following combination figure 1 Describe this embodiment, the laser-guided missile virtual test system described in this embodiment, it comprises a laser-guided missile module, a laser irradiator module, a laser transmission effect module and a missile target;

[0024] The laser irradiator module emits incident laser light, the missile target receives the incident laser light and reflects the laser light, and the seeker of the laser-guided missile module guides the missile of the laser-guided missile module to adjust the course and track the missile target according to the reflected laser signal; the laser transmission effect module is used to provide Energy attenuation data during incident and reflected laser transmission under different weather conditions.

[0025] In this embodiment, the four components of the laser-guided missile module, the laser irradiator module, the laser transmission effect module and the missile target are ...

specific Embodiment approach 2

[0026] Specific implementation mode two: the following combination figure 2 Describe this embodiment. This embodiment will further explain Embodiment 1. The working mode of the laser transmission effect module includes: the ability to simulate the transmission effect of laser in the atmosphere; the ability to configure the parameters of the atmospheric environment and view the operating parameters.

[0027] In this embodiment, the simulated laser propagation effect in the atmosphere includes the propagation effect of laser light in sunny, rainy and foggy media. You can select an environmental model, configure the environmental parameters in the environmental model, and configure different rainfall intensities, atmospheric pressure, temperature and humidity of the space environment, etc. After all parameters are configured, you can save / retrieve the parameters by using the component parameter information use case , the user can view the set parameters at any time.

[0028] In...

specific Embodiment approach 3

[0031] Specific implementation mode three: the following combination image 3 Describe this embodiment. This embodiment will further describe Embodiment 1. The working mode of the laser irradiator module includes: being able to simulate the incident laser light, and being able to set the energy, beam angle and wavelength information of the incident laser light; being able to configure the parameters of the incident laser light , and can view the running parameters.

[0032] In this embodiment, simulating real incident laser light includes simulating energy, beam angle and wavelength information of the incident laser light. It can configure parameters such as the power, wavelength, beam angle information of the incident laser, and the initial position of the laser irradiator module. After all parameters are configured, the parameters can be saved by saving / retrieving parameter information, and users can view the set parameters at any time. It is possible to view the informatio...

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Abstract

A laser-guided missile virtual test system and a construction method thereof belong to the field of virtual tests. The invention aims to solve the problems in the existing laser-guided missile virtual test system that each model is not independent, difficult to configure and difficult to reuse. The laser-guided missile virtual test system of the present invention includes a laser-guided missile module, a laser irradiator module, a laser transmission effect module and a missile target; the laser irradiator module emits incident laser light, and the missile target reflects the laser light after receiving the incident laser light, and the laser guide The seeker of the missile module guides the missile of the laser-guided missile module to adjust the course and track the missile target according to the reflected laser signal; the laser transmission effect module is used to provide the energy attenuation data of the incident laser and reflected laser transmission under different weather conditions. The invention is used for the virtual experiment of laser-guided missiles.

Description

technical field [0001] The invention relates to a laser-guided missile virtual test system and a construction method thereof, belonging to the field of virtual tests. Background technique [0002] The laser-guided missile virtual test system is a virtual test system established to simulate the real laser-guided missile system. By simulating the operation process of the laser-guided missile under different weather conditions, the operating parameters of the laser missile are obtained and analyzed. The system needs to pass through different virtual systems. Establish a corresponding laser transmission model for the combat environment. In the current scientific research on laser transmission models, the focus is on establishing models with the same laser transmission effects as in the real environment, and these models are often included in various other missile models, and the transmission effect model is functionally coupled with the missile model. Independent, not easy to c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B17/02
Inventor 林连雷付文青宋欣益
Owner HARBIN INST OF TECH