Employing the above design method, the decoupling flight control system of UH 60A helicopter is designed for attitude command attitude hold ( ACAH) response type. The simulation results show that the validity of the decoupling control design method with too fast mode of controller being limited.

  • 通过对UH-60直升机的姿态命令/姿态保持响应模式的解耦飞行控制器设计,验证了H∞控制理论对直升机解耦控制,以及所提解决控制器运动模态过快方案的有效性。

  • 互联网摘选 2025-01-20 17:31:47

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