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。
To improve the stability and precision of the time-varying system, an adaptive interpolate control method based on the online parameter identification is presented.
为提高时变系统的稳定性和精度，提出了基于在线参数辨识的自适应插补控制方法。
A synthesis method based on inverse dynamics and online parameter identification was developed and was directly used to design the attitude controller in the integrated control system.
提出了一种基于逆动力学和在线参数辨识的方法，用于直接设计综合控制系统中的姿态控制器。
应用推荐