微扑翼飞行器控制系统相关技术研究进展  

Investigation in Flight Control System of Flapping-Wing Micro Air Vehicles

作　　者：袁昌盛[1] 李永泽[1] 谭健 

机构地区：[1]西北工业大学航空学院,陕西西安710072

出　　处：《计算机测量与控制》2011年第7期1527-1529,1537,共4页Computer Measurement &Control

摘　　要：微型扑翼飞行器(FMAV)由于微型化和采用扑翼飞行方式的特征,许多传统理论和设计方法不再完全适用,相关理论和技术仍在不断地发展中,所以对国内外相关理论和技术的发展现状进行及时跟踪和研究,具有非常重要的参考意义;通过调查研究,介绍了与微型扑翼飞行器控制系统有关的低雷诺数非定常空气动力学、控制系统数学模型、控制方案和控制方法等的研究进展,总结出了微型扑翼对飞行器控制系统的设计要求,控制系统的特点和需要解决的关键问题,并展望了未来发展趋势。Flapping-Wing Micro Air Vehicle（FMAV）,as having the characteristic of miniaturization and flapping flight,some traditional theory and design methods are not completely applicable,related theory and technology is still in the progress of development,therefore,conducting immediately research of the present condition and developing trend at home and abroad is essential and instructive.Introduce the study progress of the unsteady and low Re aerodynamics;control system mathematical modeling,control scheme and control method relevant to Flapping-Wing Micro Air Vehicles,then on its basis to sum up the key technology which need to be resolved and the design requirement and characteristic of control system in our future study,and look forward to the future trend in the study of Flapping-Wing Micro Air Vehicle＇s control system.

关 键 词：微型扑翼飞行器 飞行控制 气动模型 动力学模型 控制方案 

分 类 号：TP301[自动化与计算机技术—计算机系统结构]