同时考虑操纵面偏转角度饱和及偏转速率饱和对系统的影响，设计出一种变结构可重构飞行控制系统。
The limitations on surface's deflection and deflection rate are addressed to develop the variable structure reconfigurable flight control system.
同时考虑操纵面偏转角度饱和及偏转速率饱和对系统的影响，设计出一种变结构可重构飞行控制系统。
The limitations on surface's deflection and deflection rate are addressed to develop the variable structure reconfigurable flight control system.
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