Identifiability of a nonlinear delayed-differential aerospace model
Identifiability of a nonlinear delayed-differential aerospace model
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DOI：
10.1109/tac.2005.861700
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发表时间：
2006-01-01
影响因子：
6.8
通讯作者：
Joly-Blanchard, G
中科院分区：
文献类型：
--
作者：
Denis-Vidal, L;Jauberthie, C;Joly-Blanchard, G
本技术说明说明了描述飞机动力学的非线性延迟微分模型的辨识性。这一结果是由Grewal和Goverer的结果推广到时滞系统和Orlov等人的线性时滞-微分模型可辨识性的应用而得到的。它需要与平衡状态相对应的初始条件，这是在实验过程中实现的。
This technical note shows the identiliability of a nonlinear delayed-differential model describing aircraft dynamics. This result is obtained by an original combination: An extension of the results of Grewal and Glover to delay systems and an application of linear delayed-differential model identifiability of Orlov et aL. It requires initial conditions corresponding to an equilibrium state, which is implemented during the experimentation.