直升机飞行控制系统中的计算机辅助设计与优化  

Computer-aided design and optimization in helicopter flight control system

作　　者：曹家骥 CAO Jiaji(Army Aviation Academy,Linfen,Shanxi 041000,China)

机构地区：[1]陆军航空兵学院,山西临汾041000

出　　处：《计算机应用文摘》2024年第17期79-81,共3页Chinese Journal of Computer Application

摘　　要：直升机飞行控制系统是直升机飞行过程中至关重要的一部分,其设计与优化对直升机的飞行性能、稳定性和安全性具有重要影响。文章通过分析当前直升机飞行控制系统的发展现状和存在的问题,探讨了计算机辅助设计与优化在直升机飞行控制系统中的应用。通过对控制系统的结构设计、控制算法的优化及仿真验证等方面进行研究,提出了一种基于计算机辅助设计与优化的直升机飞行控制系统设计方法,并通过实验验证了该方法的有效性和可行性。The helicopter flight control system is a crucial part of the helicopter flight process,and its design and optimization have a significant impact on the helicopters flight performance,stability,and safety.This paper analyzes the current development status and existing problems of helicopter flight control systems,and explores the application of computer-aided design and optimization in helicopter flight control systems.A helicopter flight control system design method based on computer-aided design and optimization was proposed through research on the structural design of the control system,optimization of control algorithms,and simulation verification.The effectiveness and feasibility of this method were verified through experiments.

关 键 词：直升机 飞行控制系统 计算机辅助设计 优化 

分 类 号：V249[航空宇航科学与技术—飞行器设计]