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	Six-degree-of-freedom movement simulating method for self-rotated aircraft, involves calculating four equation systems according to known thrust force of engine to obtain space six-degree-of-freedom movement state of aircraft.
	HOU C SU B WANG M WU D YANG S
	2010
公开日期	2010-01-13
URL标识	查看原文
申请日期	2009-07-25
内容类型	专利
URI标识	http://www.corc.org.cn/handle/1471x/5282875
专题	大连理工大学
作者单位	UNIV DALIAN TECHNOLOGY UNIV DALIAN TECHNOLOGY (UYDA-C
推荐引用方式 GB/T 7714	HOU C SU B WANG M WU D YANG S. Six-degree-of-freedom movement simulating method for self-rotated aircraft, involves calculating four equation systems according to known thrust force of engine to obtain space six-degree-of-freedom movement state of aircraft.. 2010-01-01.

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