基于增量非线性动态反演的四旋翼飞行器部分执行器故障鲁棒自适应控制

Karim AHMADİ DASTGERDİ, D. Asadi, Seyed Yaser NABAVİ CHASHMİ, Önder Tutsoy
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引用次数: 0

摘要

提出了一种基于增量非线性动态反演(INDI)的非线性鲁棒自适应轨迹跟踪控制体系,用于四旋翼飞行器在执行器局部故障情况下的稳定控制。在一种新颖的方法中,提出了一种三环级联结构的控制器。内环采用INDI算法作为基准控制器,外环增加非线性模型参考自适应控制器,为内环未建模故障提供鲁棒性。在所提出的控制策略中,在最外环中引入一个改进的PID控制器来跟踪期望的路径。考虑了电动机推力和转矩的突然变化,对故障效应进行了建模。为了提高控制算法的鲁棒性,在鲁棒自适应结构中引入了投影算子。将所提出的控制器的性能与先前在四旋翼模型上成功实现的算法进行了比较。结果表明,在执行器部分故障高达50%的情况下,所提出的控制器可以在俯仰、横滚和偏航通道上提供所需故障四旋翼的完全可控性。
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Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault
In this paper, a nonlinear robust adaptive trajectory tracking control architecture based on Incremental Nonlinear Dynamic Inversion (INDI) is introduced to stabilize and control a quadrotor in presence of actuator partial fault. In a novel approach, a three-loop cascade architecture of the controller is proposed. The INDI algorithm is applied as the baseline controller in the inner-loop and a nonlinear model reference adaptive controller is augmented in the outer-loop to provide robustness for the unmodeled fault in the inner-loop. In the proposed control strategy, a modified PID controller is introduced in the most outer-loop for tracking the desired path. The fault effect has been modeled by considering the sudden variations of motor thrust and torques. To increase the robustness of the control algorithm the projection operator has been applied in the robust adaptive structure. The performance of the proposed controller is compared with a previous successful algorithm, which had been implemented on a quadrotor model. The results demonstrate that the proposed controller can provide full controllability of the desired faulty quadrotor in pitch, roll, and yaw channels in presence of partial fault of actuator up to 50%.
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