Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft

Melvin Rafi; James E. Steck; John Watkins

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Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft

机译：基于卡尔曼滤波器的自适应控制：通用航空飞机的飞行测试

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Model reference adaptive control brings various practical benefits to general aviation aircraft. In addition to being a control system conducive to an easier workload on pilots, it adds an additional layer of redundancy in scenarios where uncertainties arise, or where part of an aircraft system has failed. In enhancing the capability of the model reference adaptive control (MRAC) in handling unexpected uncertainties in the form of sensor-induced noise and atmospheric turbulence, a Kalman filter was designed and implemented within the existing three-degree-of-freedom MRAC framework developed at Wichita State University.

机译：模型参考自适应控制为通用航空飞机带来了各种实际好处。除了是有助于减轻飞行员工作量的控制系统外，它还可以在出现不确定性或飞机系统的一部分出现故障的情况下增加一层冗余。为了增强模型参考自适应控制（MRAC）处理传感器引起的噪声和大气湍流形式的意外不确定性的能力，在现有的三自由度MRAC框架下，设计并实施了卡尔曼滤波器威奇托州立大学。

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《Journal of guidance, control, and dynamics》 |2017年第9期|2307-2316|共10页
作者
Melvin Rafi; James E. Steck; John Watkins;
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Wichita State University, Wichita, Kansas 67260;

Wichita State University, Wichita, Kansas 67260;

Wichita State University, Wichita, Kansas 67260;

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Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft

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