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Avionics weapon attack test system

An attack test and weapon technology, which is applied in the field of avionics weapon attack test system, can solve problems such as lack of intuition, lack of correlation of data, and difficulty in obtaining situational information related to carrier aircraft and target characteristics.

Inactive Publication Date: 2019-11-22
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1) During the attack test of avionics weapons, the parameters of the carrier aircraft, the target parameters corresponding to the airborne sensors, and the loading parameters of the weapon were respectively simulated, resulting in the lack of correlation of the obtained data, and it is difficult to obtain the relationship between the carrier aircraft and the characteristics of the target. situational information;
[0004] 2) It verifies the control logic of the weapon by analyzing the recorded bus data, which lacks intuitiveness, time-consuming and laborious

Method used

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Embodiment Construction

[0042] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the related application, not to limit the application. In addition, it should be noted that, for ease of description, only parts relevant to the present application are shown in the drawings.

[0043] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0044] It should be noted that in the description of this application, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The terms of the indicated direction or positional relationship are based on the direction or positional ...

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Abstract

The invention relates to an avionics weapon attack test system which comprises a story generation system for generating carrier parameters, target parameters and weapon loading parameters, a flight simulation system for acquiring the carrier parameters and generating a carrier flight data based on the carrier parameters, and transmitting the carrier flight data to an inertial navigation unit and an atmospheric aircraft, a target simulator used for obtaining the target parameters, generating a target analog signals according to the target parameters, and sending the target analog signals to a corresponding airborne device on a carrier, a weapon simulator for obtaining the weapon loading parameters, simulating corresponding weapon states according to weapon loading parameters, and performingdata interaction with an external system of the carrier, a carrier bus test system used for obtaining output data of the inertial navigation unit, the atmospheric aircraft, the airborne device and the external system and analyzing the output data to obtain analysis data, and a data analysis system used for obtaining the analysis data and analyzing and / or storing the analysis data.

Description

technical field [0001] The application belongs to the technical field of avionics weapon attack testing, and in particular relates to an avionics weapon attack testing system. Background technique [0002] The avionics weapon attack test system is used for the avionics weapon attack test. The current avionics weapon test system has the following defects: [0003] 1) During the attack test of avionics weapons, the parameters of the carrier aircraft, the target parameters corresponding to the airborne sensors, and the loading parameters of the weapon were respectively simulated, resulting in the lack of correlation of the obtained data, and it is difficult to obtain the relationship between the carrier aircraft and the characteristics of the target. situational information; [0004] 2) It verifies the control logic of the weapon by analyzing the recorded bus data, which lacks intuition and is time-consuming and laborious. [0005] The present application is proposed in view ...

Claims

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Application Information

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IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 郭操张中方姜卓万文章
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA