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II-based adaptive control of a four-rotor mini helicopter

机译:基于I&I的四旋翼小型直升机的自适应控制

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For a four-rotor mini helicopter, an adaptive controller is presented based on Immersion and Invariance (I&I) approach. Although there are many aerodynamic coefficients such as thrust coefficients and drag coefficients with uncertainty in the model, a new parameterization with a fewer uncertain coefficients is developed to simplify the complex multivariable parameter adaptation. It is shown that the adaptive controller is capable of estimating not only the unknown parameters but also external torque disturbances and rejecting them. Numerical simulation illustrates the robustness of the controller against the parametric uncertainty and external torque disturbances.
机译:对于四旋翼微型直升机,提出了一种基于沉浸和不变性(I&I)方法的自适应控制器。尽管模型中存在许多具有不确定性的空气动力学系数,例如推力系数和阻力系数,但仍开发了具有较少不确定系数的新参数化方法,以简化复杂的多变量参数自适应。结果表明,自适应控制器不仅能够估计未知参数,而且能够估计并拒绝外部转矩干扰。数值仿真说明了控制器针对参数不确定性和外部转矩扰动的鲁棒性。

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