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Adaptive tracking control for a model helicopter with disturbances

机译:具有干扰的模型直升机的自适应跟踪控制

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A nonlinear adaptive control algorithm is presented for a model helicopter to achieve the trajectory tracking in the presence of external disturbances. The design process is based on the backstepping technology with the simplified helicopter model. A command filter is utilized to avoid the complicated derivative computation of the virtual control. With the property of the hyperbolic tangent function, upper bounds of the disturbing terms composed by unmodeled dynamics, command filter errors and other external disturbances are estimated by adaptive algorithms and compensated for in control laws. It is proved that the proposed control algorithm guarantees uniform boundedness of the tracking error of the complete closed-loop system. Simulations verify the significant tracking performance of the proposed controller.
机译:提出了一种用于模型直升机的非线性自适应控制算法,以在存在外部干扰的情况下实现轨迹跟踪。设计过程基于具有简化直升机模型的后推技术。利用命令过滤器来避免虚拟控件的复杂的导数计算。利用双曲正切函数的性质,通过自适应算法估计由未建模动力学,命令滤波器误差和其他外部干扰组成的干扰项的上限,并在控制律中对其进行补偿。实践证明,所提出的控制算法保证了完整闭环系统跟踪误差的均匀有界性。仿真验证了所提出控制器的显着跟踪性能。

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