In this paper, the aerodynamic parameter identification of elastic aircraft is studied by the maximumlikelihood 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。
2
The parameters of Fisher distribution model are estimated by maximumlikelihood, and the model is finally verified by using Pearson test.
利用所提出的快速聚类分析方法及其推导的计算公式，可以方便地求解费歇尔分布的参数。
3
The parameters of model are measured by taking into account the stochastic characteristic of entire test data, which is connected with a maximumlikelihood method and math programming.