This method realizes integration of attitude reference signal and guidance command, attitude control and mass center control. It can reduce precision requirements on aerodynamic data and the control parameters can be easily selected.
这种方法实现了姿态参考信号与导引指令的统一,姿态控制与质心控制的统一,能够充分降低对于气动等数据的精度要求,参数选择简单。
参考来源 - 飞航导弹高精度自适应预测控制设计·2,447,543篇论文数据,部分数据来源于NoteExpress
The engine speed is also used as ignition reference signal.
发动机转速信号同时也作为点火基准信号。
The pilot symbols were used to estimate channel and act as reference signal of beam-former.
利用导频符号进行信道估计,并作为空间波束成型器的参考信号。
The pilot symbols were used to estimate channel and acted as reference signal of beam-former.
利用导频符号进行权向量更新算法,并作为空间波束成型器的参考信号。
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