飞行器智能结构系统研究进展与关键问题  

Progress and Challenges in Aeronautical Smart Structure Systems

作　　者：陈勇[1] 熊克[1] 王鑫伟[1] 梁大开[1] 

机构地区：[1]南京航空航天大学智能材料与结构航空科技重点实验室,江苏南京210016

出　　处：《航空学报》2004年第1期21-25,共5页Acta Aeronautica et Astronautica Sinica

基　　金：国家自然基金(50135030;90205031);江苏省自然基金(BK2001213);航空基金(01I52056);国防基金(51463040801HK0204;00J12.2.3.HK0205)资助项目

摘　　要：飞行器智能结构是由传感器、驱动器、控制元件和基体结构组成的集成系统,它具有承载、检测、判断与动作等功能,可显著提升飞行器的性能。根据国内外飞行器智能结构系统研究的最新进展,论述了飞行器结构动力响应主动控制、智能机翼、旋翼以及飞行载荷谱监测与结构损伤诊断等的基本原理与技术问题;指出了飞行器智能结构系统研究在埋入式功能元件、复杂非线性多场耦合系统的动力学建模与控制以及智能结构系统中的损伤和失效问题等方面所面临的关键技术问题和挑战。Aeronautical smart structure is an integrated system composed of distributed sensor, actuator and controller network. It provides load-bearing, measuring, decision making and actuation functions to aeronautical structures, and improves the performance of modern aircraft. A comprehensive review is made of state of the art research in aeronautical smart structures. The basic principles, technical approaches and latest progress in online load monitoring and damage diagnosis technology, active vibration control and noise suppression technology, adaptive wing and smart rotor technology, and active fluid control of micro aerial vehicle technology are discussed. Some important topics, including the development of reliable embedded sensor and actuator elements, dynamic modeling and control method in multi-fields coupling non-linear systems, the damage failure and tolerance theories, are put forward as the fundamental problems and technical challenges in future aeronautical smart structure system research. Multi-scale and multi-disciplinary modeling, analysis, simulation and optimization method, advanced information processing and fusion technology, and robust control theories are suggested as potential technical approaches to solve these difficulties.

关 键 词：智能结构 振动控制 自适应机翼 智能旋翼 结构健康监测 

分 类 号：V214.9[航空宇航科学与技术—航空宇航推进理论与工程]