基于绝对连续分数阶积分滑模的四旋翼飞行器姿态跟踪控制

A. Muñoz‐Vázquez, Vicente Parra‐Vega, A. Sánchez‐Orta, O. García, Carlos Izaguirre
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引用次数: 21

摘要

基于分数阶滑动曲面的无模型滑模控制建立在:i)一个绝对连续的控制结构,它不需要精确的动态模型来诱导有限时间内的分数阶滑动运动;ii)提出了一种在频域中具有明确对应的分数阶参考的设计方法。这是为了提高系统的响应,特别是瞬态期间,并产生一个高性能的滑动运动。数值模拟支持了该方案,并举例说明了闭环系统,从而更好地了解了所提出的方案。
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Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes
The model-free sliding mode control based on fractional order sliding surface is built upon: i) An absolutely continuous control structure that does not require the exact dynamic model to induce a fractional sliding motion in finite time, and ii) A methodology to design fractional references with a clear counterpart in the frequency domain is proposed. This in order to improve the system response, in particular the transient period, and to generate a high-performance during the sliding motion. Numerical simulations support the proposal and illustrates the closed-loop system, which provides a better insight of the proposed scheme.
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