Output error method is one of the most widely applied methods in the region of aerodynamic parameter identification for aircraft.
输出误差法是飞行器气动参数辨识最广泛采用的一种方法。
The implementation of maximum likelihood estimation method to the nonlinear continuous ?discrete systems and application to aerodynamic parameter identification for vehicle are studied.
研究了非线性连续—离散系统极大似然估计方法的实现及其在飞行器气动参数辨识中的应用问题。
In this paper, the aerodynamic parameter identification of elastic aircraft is studied by the maximum likelihood estimation algorithm using, orthogonal test table for computing sensitivities.
本文基于正交计算灵敏度的极大似然估计算法研究了弹性飞行器的气动参数辨识问题。
The aerodynamic parameters wear estimated through online parameter identification method and were used for actuator deflect allocation.
使用在线参数辨识方法，对飞机的气动特性进行估计并用于舵面分配。
The aerodynamic parameters wear estimated through online parameter identification method and were used for actuator deflect allocation.
使用在线参数辨识方法，对飞机的气动特性进行估计并用于舵面分配。
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