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Adaptive tracking control for a model helicopter with disturbances

机译:用于造型造型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:为模型直升机提出了非线性自适应控制算法,以实现外部干扰存在的轨迹跟踪。设计过程基于简化直升机模型的BackStepping技术。使用命令过滤器来避免虚拟控制的复杂衍生计算。对于双曲线切线函数的性质,通过自适应算法估计了由未拼接动态,命令滤波器误差和其他外部干扰组成的扰动术语的上限,并在控制法中得到补偿。事实证明,该控制算法保证了完整闭环系统的跟踪误差的均匀界限。仿真验证了所提出的控制器的显着跟踪性能。

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