高精度巡航导弹智能控制系统的计算机仿真

2022 International Conference on Smart Information Systems and Technologies (SIST) Pub Date : 2022-04-28 DOI:10.1109/SIST54437.2022.9945703

Moldamurat Khuralay, Akhmetov Kayrat Telektesovich, Otegen Alikhan Serikovich, Brimzhanova Saule Serikovna, Otyzbayeva Karlygash Zhalenovna, Zhiyenbek Arailym Oteulievna

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引用次数: 2

摘要

本文讨论了一种高精度巡航导弹智能飞行控制系统。在空间工程和技术领域，考虑使用计算机程序和在计算机程序中研究空间分析的最有效方面。对高速巡航导弹的精确制导和制导进行了计算和计算机研究。因此，控制系统采用基于人工智能的模糊逻辑方法进行设置。高精度巡航导弹智能控制系统的计算机建模。巡航导弹控制系统需要大量的参数和复杂的数学计算模型和物理问题来控制智能系统。本文在计算机程序中提供了一个高速巡航导弹测试模拟器。本模拟器是用c++编程语言在Matlab编辑器R2015b中编写的。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Computer Simulation of Intelligent Control Systems for High-Precision Cruise Missiles

This article discusses an intelligent flight control system for high-precision cruise missiles. In the field of space engineering and technologies, the most effective aspects of using computer programs and studying space analysis in a computer program are considered. Calculations and computer studies of precision guidance and guidance of high-speed cruise missiles are presented. Therefore, system of the control is set by the fuzzy logic method based on artificial intelligence. Computer modeling of intelligent control systems for high-precision cruise missiles. The cruise missile control system requires a large number of parameters and complex mathematical calculation models and physical problems to control the intelligent system. The article provides a simulator in a computer program to test high-speed cruise missiles. This simulator is written in Matlab editor R2015b in C ++ programming language.

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来源期刊

2022 International Conference on Smart Information Systems and Technologies (SIST)

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