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。
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 controller output error method (COEM) is used to design the adaptive fuzzy controller.
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。
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.
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。
The implementation of maximum likelihood estimation method to the nonlinear continuous ?discrete systems and application to aerodynamic parameter identification for vehicle are studied.
为了提高气动参数辨识的精度，根据飞机运动方程，给出了测量中的系统偏差、尺度因子误差和随机噪声描述，并提出了一种飞行数据相容性检验的快速算法。
To get high accuracy of the identification of aerodynamic parameters, based on the motion equation of an aircraft, a fast algorithm for flight data compatibility check is presented in this paper.
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.
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。
Assuming that noise is unknown but bounded, set membership identification problem for flight vehicle aerodynamic parameters is studied in this paper.
主要讨论了测量参数间的时间延迟对飞机气动导数辨识结果的影响。
This paper briefly discusses the effects on the aerodynamic derivative identification results caused by time delay in measured parameters.
主要讨论了测量参数间的时间延迟对飞机气动导数辨识结果的影响。
This paper briefly discusses the effects on the aerodynamic derivative identification results caused by time delay in measured parameters.
应用推荐