... control messages 控制讯息 control mode 控制模态 control nondata I/O operations 控制非数据输出入操作 ...
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并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
因在由控制模态方程推导时滞最优控制律的过程中无近似处理，所给控制方法易于保证控制系统的稳定性。
Since no approximation is made in the derivation of the time-delay optimal controller from the mode-controlled equation, the system stability is easy to guarantee.
用该综合方法对某型飞机的侧向直接力控制模态(航向指向)进行了分析与设计，并将其与动态逆方法进行了比较。
The design and simulation of the yaw pointing mode dynamic decoupling fuzzy control system for an aircraft are studied in this paper.
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