本文采用了一种基于广义卡尔曼滤波的自适应追踪技术对结构的参数进行辨识。
In this paper, we proposed an adaptive tracking technique, based on extended Kalman filter approach, to identify the structural parameters and their changes.
利用参数自适应控制技术，提出了一种能够自适应补偿飞机参数变化的快速采样控制律。
This paper provides an adaptive fast sampling control law to compensate for changing aircraft parameters by the parameter adaptive control techniques.
参数装定技术是实现开舱时间自适应修正系统功能的关键技术之一。
Parameter setting technology is the key technology to realize the functions of dispending time adaptive correction system.
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