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Weighted pseudo-inverse based control allocation of heterogeneous redundant operating mechanisms for DPC aircraft

机译:基于加权伪逆的DPC飞机异构冗余运行机制控制分配

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Distributed propulsion configuration (DPC) usually have heterogeneous redundant operating mechanisms including redundant control surfaces and thrust vector actuators, thus producing strong and complex control coupling between flight and propulsion systems. Then control allocation of heterogeneous redundant actuators is certainly required to realize integrated control. First, the formulation of this specific control allocation problem is given, and then the Moore-Penrose pseudo-inverse method and weighted pseudo-inverse method are introduced to improve control accuracy and coordinate the complex relationship between different types of actuators. Simulation results reveal that the weighted pseudo-inverse method has higher accuracy in allocation result, and it is suitable for the specific control allocation problem for DPC aircraft.
机译:分布式推进配置(DPC)通常具有异构冗余操作机制,包括冗余控制面和推力矢量执行器,因此在飞行和推进系统之间产生强大而复杂的控制耦合。因此,必须实现异构冗余执行器的控制分配,以实现集成控制。首先给出了具体控制分配问题的公式,然后引入了Moore-Penrose伪逆方法和加权伪逆方法,以提高控制精度并协调不同类型执行器之间的复杂关系。仿真结果表明,加权伪逆法在分配结果上具有较高的精度,适用于DPC飞机的具体控制分配问题。

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