Then a two-step method for the set-membership identification of a helicopter fully coupled flight dynamics model is established.
在此基础上,建立了直升机全耦合飞行动力学模型集员辨识的两步法。
A set membership identification approach is provided to deal with the problem of fault detection of systems with models not precisely known.
为了处理数学模型不精确已知系统的故障检测问题,给出了一种故障检测的集员辨识方法。
Assuming that noise is unknown but bounded, set membership identification problem for flight vehicle aerodynamic parameters is studied in this paper.
在噪声未知但有界的情况下,本文研究了飞行器气动参数的集员辨识问题。
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