... 模型参考(自)适应控制 model reference adaptive control 模型带飞试验 model flight test 模型锻造 closed die forging ...
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In this paper, the mathematical model of compatibility check of flight test date is set up based on the kinematic equations with six freedom of aircraft.
本文采用飞行器六自由度运动方程组,建立了飞行试验数据相容性检验的数学模型。
ARMAX model method and subspace-based state space method were used to process the flight flutter test data, and identify the flutter modal parameters of aircraft.
论文使用了现代参数辨识技术的AR MAX模型递推法和状态子空间辨识法,对飞行颤振试验数据进行处理,辨识飞机的颤振模态参数。
The engine model identification using flight test signals is introduced.
利用飞行试验信号对发动机模型辨识进行了研究。
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