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High-altitude high-speed aircraft defense penetration survivability rapid evaluation device

A technology for evaluating devices and survivability, applied in design optimization/simulation, sustainable transportation, geometric CAD, etc., can solve problems such as poor design guidance and difficult theoretical analysis, to improve design efficiency, quickly verify feasibility, The effect of rapid evaluation

Active Publication Date: 2020-04-21
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the large number of variables affecting penetration survivability, theoretical analysis is difficult, and often only qualitative conclusions can be given, which has poor guidance for program design

Method used

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  • High-altitude high-speed aircraft defense penetration survivability rapid evaluation device

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Embodiment Construction

[0032] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with th...

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Abstract

The invention belongs to the field of aircraft overall design, and particularly relates to a high-altitude high-speed aircraft defense penetration survivability rapid evaluation device, which comprises: a missile performance model used for missile full-airspace trajectory simulation and outputting missile flight information in real time; an aircraft performance model which is used for truly simulating aerodynamic characteristics and maneuverability of the aircraft; a simulation framework module which is used for calling the aircraft performance model and the missile performance model; a processing module cluster which is controlled by the simulation framework module and is used for realizing high-altitude high-speed aircraft defense penetration survivability rapid evaluation simulation parallel computing; a simulation profile setting module which is used for providing simulation ranges and step lengths of corresponding parameters; and a simulation result analysis module which is used for analyzing the simulation result data. According to the high-altitude high-speed aircraft defense penetration survivability rapid evaluation device, rapid evaluation of defense penetration survivability of the high-altitude high-speed aircraft can be realized, design iteration of an aircraft platform scheme and a defense penetration scheme is accelerated, scheme feasibility is rapidly verified,and design efficiency is improved.

Description

technical field [0001] The application belongs to the field of overall aircraft design, and in particular relates to a rapid assessment device for high-altitude and high-speed aircraft penetration survivability. Background technique [0002] Air power plays a vital role in modern warfare and is the core of a country's military air power. High-altitude and high-speed aircraft are one of the most important air power, and their penetrating survivability against air-to-air missiles is an important factor in evaluating aircraft performance. Therefore, the rapid evaluation method for the penetration survivability of high-altitude and high-speed aircraft has become an important research topic for aeronautical engineers. [0003] The penetration survivability of high-altitude and high-speed aircraft is closely related to the aircraft's stealth capability, maneuverability, engine thrust, and penetration strategy. Therefore, many parameters are involved in the initial design of high-a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/20
CPCY02T90/00
Inventor 李俊男骆遥朴海音孙智孝宛旭詹光徐庆华刘士才刘云飞孙阳李思凝郎魁军史贵超
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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