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首页> 外文期刊>Journal of intelligent & fuzzy systems: Applications in Engineering and Technology >Adaptive fuzzy control for a quadrotor helicopter robust to wind buffeting
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Adaptive fuzzy control for a quadrotor helicopter robust to wind buffeting

机译:具有抖振性的四旋翼直升机的自适应模糊控制

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摘要

The nonlinear and open-loop unstable dynamics of a quadrotor helicopter makes a control system design non-trivial. However, even more difficulty lies in adapting to an uncertain dynamic model and unknown payloads while remaining robust to significant buffeting wind disturbances. Fuzzy-adaptive or neural-adaptive control offer possible solutions, exhibiting computational efficiency and adaptation to arbitrary nonlinearities. A common method for making these adaptive controls robust to disturbances, e-modification, is found to be unsuitable when applied to the quadrotor in simulation. The adaptive parameters tend to drift to large values in the presence of a sinusoidal disturbance. In this work, we propose a method that uses alternate adaptive parameters in the adaptation scheme. The proposed method successfully controls the quadrotor in simulation, with realistic control signals and computational effort. The adaptive parameter drift and control chatter present with e-modification both vanish. Moreover, performance improves dramatically in the presence of disturbances.
机译:四旋翼直升机的非线性和开环不稳定动力学特性使控制系统设计变得不平凡。然而,更大的困难在于适应不确定的动态模型和未知的有效载荷,同时保持鲁棒性以应对重大的风振扰动。模糊自适应或神经自适应控制提供了可能的解决方案,表现出计算效率和对任意非线性的适应性。当将其应用于仿真中的四旋翼时,发现使这些自适应控制对干扰具有鲁棒性的通用方法(电子修改)不合适。在存在正弦波干扰的情况下,自适应参数往往会漂移到较大的值。在这项工作中,我们提出了一种在自适应方案中使用替代自适应参数的方法。所提出的方法在仿真中成功地控制了四旋翼飞机,具有逼真的控制信号和计算能力。带有电子修改的自适应参数漂移和控制抖动都消失了。此外,在存在干扰的情况下,性能也会大大提高。

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