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Adaptive Control of a Morphing Aircraft through Updating the Number of Actuators

机译:通过更新执行器的数量,对变形飞机的自适应控制

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An adaptive control scheme with control allocation through updating the number of operating actuators is proposed for a morphing aircraft which is called Innovative Control Effectors (ICE) aircraft. For the ICE morphing aircraft, there are hundreds of shape-change devices in an array on each wing. Different flight conditions correspond to different numbers of actuating devices to adapt to a changing mission environment. In this paper, firstly, the time-continuous morphing aircraft model is transformed into time-discrete model because of an uncertain quantization parameter in the model, and subsequently the adaptive flight control law is designed for the uncertain discrete time morphing aircraft model to track a desired reference model. Then the update rule of the number of actuators in control allocation module is derived in an implicit method. Finally, the simulation results are given to demonstrate the effectiveness of scheme proposed.
机译:通过更新操作致动器的数量的传感飞机提出了一种具有控制分配的自适应控制方案,称为创新控制效果(ICE)飞机。对于冰变形飞机,每个翼上有数百个形状更换设备。不同的飞行条件对应于不同数量的致动设备,以适应改变的使命环境。在本文中,首先,由于模型中的量化参数不确定的量化参数,将时间连续的变形飞机模型转化为时间分离模型,随后设计了自适应飞行控制规律,专为追踪了不确定的离散时间变形飞机模型而设计所需的参考模型。然后,控制分配模块中的执行器数量的更新规则是以隐式方法导出的。最后,给出了模拟结果来证明所提出的方案的有效性。

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