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Adaptive backstepping trajectory tracking controller for a small-scaled helicopter

机译:小型直升机的自适应反步轨迹跟踪控制器

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An adaptive backstepping controller is proposed to achieve the trajectory tracking for a small-scaled helicopter. The helicopter model is first decomposed into a cascade structure between the position and attitude loops with uncertain dynamics. The backstepping technique is introduced to exploit the controller based on the decomposed model and the upper bounds of the unmodeled dynamics are compensated with the hyperbolic tangent function. The controller introduces a dynamic auxiliary system to obviate the singularity during the derivation of the command attitude; and criteria of controller parameters are developed to guarantee the bounded tracking. In addition, command filters are employed to ease complex derivative calculations. The stability analysis proves that the proposed controller realizes the ultimately bounded tracking of the helicopter system. Simulations verify the performance of the proposed controller.
机译:提出了一种自适应反推控制器来实现小型直升机的轨迹跟踪。首先将直升机模型分解为位置和姿态环之间具有不确定动力学的级联结构。引入了反步技术来利用基于分解模型的控制器,并用双曲正切函数补偿未建模动力学的上限。控制器引入了动态辅助系统,以消除在得出命令姿态时的奇异性。制定了控制器参数准则,以保证有界跟踪。另外,采用命令过滤器来简化复杂的导数计算。稳定性分析证明所提出的控制器实现了直升机系统的最终有界跟踪。仿真验证了所提出控制器的性能。

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