The procedure presented in this paper applies to the design of longitudinal or lateral flight control systems and to the selection of twelve parameters of a system for optimization design.
本文介绍的方法适用于纵向或侧向的飞行控制系统，可对系统中十二个参数作优化设计。
The procedure presented in this paper applies to the design of longitudinal or lateral flight control systems and to the selection of twelve parameters of a system for optimization design.
本文介绍的方法适用于纵向或侧向的飞行控制系统，可对系统中十二个参数作优化设计。
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