随机模型预测控制四旋翼直升机轨迹跟踪

Yanhua Yang, Y. Chen, Chaoquan Tang, Li Chai
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引用次数: 4

摘要

针对具有随机扰动的四旋翼直升机,提出了一种随机模型预测控制(SMPC)方法。随机扰动假定为高斯白噪声。现有的鲁棒控制方法一般都能保证在最坏干扰下的跟踪性能满足给定条件。但在实际应用中,最坏情况下的扰动发生的概率可能非常小,因此这些方法具有很大的保守性。在本文中,干扰引起的跟踪误差在给定的概率下被限制在可接受范围内。采用分层控制结构。外环为位置环,采用SMPC控制器进行位置跟踪。在内环姿态环中,采用反馈线性化策略对非线性动力学进行线性化,并设计了SMPC控制器进行姿态跟踪。最后,仿真结果验证了所提方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Quadrotor helicopters trajectory tracking with stochastic model predictive control
A stochastic model predictive control (SMPC) method is proposed for trajectory tracking of quadrotor helicopters with stochastic disturbances. The stochastic disturbances are assumed to be Gaussian white noises. The existing robust control methods generally guarantee that the tracking performances under the worst-case disturbances satisfying given conditions. However, the worst-case disturbances may have a vanishingly small probability of occurrence in practice, so these methods show great conservative. In this paper, the tracking errors caused by the disturbances are limited in the acceptable range with the given probability. The hierarchical control structure is used. In the outer loop, the position loop, SMPC controllers are designed for position tracking. In the inner loop, the attitude loop, the nonlinear dynamics are linearized by the feedback linearization strategy, and an SMPC controller is designed for attitude tracking. Finally, simulation results verify the effectiveness of the proposed method.
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