The proposed method is applied to satellite attitude controller design to cope with the errors arising while linearization procedure.

将所得结果应用于卫星姿态控制系统的设计，以解决对模型进行线性化处理时产生的误差。

youdao

Then, base on the problem of attitude control of a satellite under development, we design a NN compensation controller for high accuracy orientation phase.

然后，基于某型小卫星的姿态控制问题，设计了高精度定向阶段的神经网络补偿控制器。

youdao

According to the singularity perturbation theory, dynamic inversion is adopted to design the basic attitude controller including fast inverse loop and slow inverse loop.

利用多重时间尺度奇异摄动理论，结合非线性动态逆方法设计了基本姿态控制器，包括快逆回路和慢逆回路两部分。

youdao