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	Identification of flight dynamics models of a small-scale unmanned helicopter in hover condition [悬停状态下小型无人直升机飞行动力学模型辨识]
	Wu, M.; Chen, M.; Wang, F.
刊名	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
	2019
卷号	45页码:546-559
关键词	Flight dynamics Frequency response Gyroscopes Identification (control systems) Linear systems Nonlinear analysis Nonlinear equations Nonlinear systems Religious buildings Unmanned aerial vehicles (UAV) 3-axis gyro Dynamics characteristic Flight dynamics model Frequency-domain identification High frequency domain Identification method Nonlinear mathematical model Small-scale unmanned helicopter Helicopters
ISSN号	10015965
DOI	10.13700/j.bh.1001-5965.2018.0384
URL标识	查看原文
收录类别	EI
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5919278
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Wu, M.,Chen, M.,Wang, F.. Identification of flight dynamics models of a small-scale unmanned helicopter in hover condition [悬停状态下小型无人直升机飞行动力学模型辨识][J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,2019,45:546-559.
APA	Wu, M.,Chen, M.,&Wang, F..(2019).Identification of flight dynamics models of a small-scale unmanned helicopter in hover condition [悬停状态下小型无人直升机飞行动力学模型辨识].Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,45,546-559.
MLA	Wu, M.,et al."Identification of flight dynamics models of a small-scale unmanned helicopter in hover condition [悬停状态下小型无人直升机飞行动力学模型辨识]".Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 45(2019):546-559.

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