The design and simulation of the yaw pointing mode dynamic decoupling fuzzy control system for an aircraft are studied in this paper.
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。
Multiple PID, Multiple Sliding mode and Multi-model based fuzzy controllers are introduced to solve the speed, depth, pitch and yaw control problem respectively.
以多模型PID、多模型滑模控制和多模型优化的模糊控制算法解决深度、速度、纵倾和航向控制问题。
Multiple PID, Multiple Sliding mode and Multi-model based fuzzy controllers are introduced to solve the speed, depth, pitch and yaw control problem respectively.
以多模型PID、多模型滑模控制和多模型优化的模糊控制算法解决深度、速度、纵倾和航向控制问题。
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