| 微扑翼飞行器控制系统相关技术研究进展 |
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| 引用本文： | 袁昌盛,李永泽,谭健.微扑翼飞行器控制系统相关技术研究进展[J].计算机测量与控制,2011,19(7). |
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| 作者姓名： | 袁昌盛 李永泽 谭健 |
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| 作者单位： | 西北工业大学航空学院,陕西西安,710072 |
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| 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。
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| 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 |
Investigation in Flight Control System of Flapping-Wing Micro Air Vehicles |
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| Yuan Changsheng,Li Yongze,Tan Jian.Investigation in Flight Control System of Flapping-Wing Micro Air Vehicles[J].Computer Measurement & Control,2011,19(7). |
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| Authors: | Yuan Changsheng Li Yongze Tan Jian |
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| Affiliation: | Yuan Changsheng,Li Yongze,Tan Jian(School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China) |
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| Abstract: | 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 co... |
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| Keywords: | FMAV flight control aerodynamics mathematic modeling control scheme |
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