直升机悬停状态全耦合飞行动力学模型辨识方法
Identification Method for Helicopter Fully Coupled Flight Dynamics Model in Hover Condition
Received date: 2010-04-22
Revised date: 2010-07-19
Online published: 2011-02-25
吴伟, 陈仁良. 直升机悬停状态全耦合飞行动力学模型辨识方法[J]. 航空学报, 2011, 32(2): 202-211. DOI: CNKI:11-1929/V.20101118.0908.001
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