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飞行/推进系统一体化控制综述

Integrated Flight/Propulsion Control Summarization
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摘要 先进战斗机采用飞行/推进一体化控制技术对各个子系统进行控制,使各个子系统达到整体性能优化,提高飞机综合性能,减轻驾驶员负担,大大提升飞机作战性能。文中针对飞行/推进系统一体化控制问题,对国内外的发展情况进行了研究分析,并提出新一代战斗机的主要发展方向,将以采用飞行控制、推力控制和公共设备管理等系统综合的飞行平台关系系统(IVMS)为基础,实现不同安全级别功能,在单处理器模块上的综合,在整个系统中实现功能的多余度配置和故障自动重构,并对我国新一代飞行/推进一体化控制系统提出了总体设计建议。 Which leads to the application of integrated flight/propulsion control in some advanced fighters to maximize the overall performance of various subsystems.In this way,the aerodynamic and operational performances are improved.This paper discusses the development of integrated flight/propulsion control at home and aboard.And the result shows that using Integrated Vehicle Management System(IVMS) to integrate flight control,propulsion control,public facilities management and other systems would be the main developing direction of newgeneration.The application of IVMS would integrate functions of different safety degrees in a single processor module,and realize the functional redundancy configuration and automatic fault refactoring.In the end of the paper,proposals of integrated flight/propulsion control were put forward.
作者 吴敬伟 宁永前 陈晗 王光豪 WU Jing-wei;NING Yong-qian;CHEN Han;WANG Guang-hao(Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
出处 《飞机设计》 2017年第6期6-12,共7页 Aircraft Design
关键词 飞行/推进一体化控制 飞行控制 发动机控制 integrate flight/propulsion control flight control engine control
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