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Robust Full Tracking Control Design of Disturbed Quadrotor UAVs with Unknown Dynamics

机译:具有未知动力学的扰动四旋翼无人机的鲁棒全跟踪控制设计

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In this study, we develop a rigorous tracking control approach for quadrotor unmanned aerial vehicles (UAVs) with unknown dynamics, unknown physical parameters, and subject to unknown and unpredictable disturbances. In order to better estimate the unknown functions, seven interval type-2-adaptive fuzzy systems (IT2-AFSs) and five adaptive systems are designed. Then, a new IT2 adaptive fuzzy reaching sliding mode system (IT2-AFRSMS) which generates an optimal smooth adaptive fuzzy reaching sliding mode control law (AFRSMCL) using IT2-AFSs is introduced. The AFRSMCL is designed a way that ensures that its gains are efficiently estimated. Thus, the global proposed control law can effectively achieve the predetermined performances of the tracking control while simultaneously avoiding the chattering phenomenon, despite the approximation errors and all disturbances acting on the quadrotor dynamics. The adaptation laws are designed by utilizing the stability analysis of Lyapunov. A simulation example is used to validate the robustness and effectiveness of the proposed method of control. The obtained results confirm the results of the mathematical analysis in guaranteeing the tracking convergence and stability of the closed loop dynamics despite the unknown dynamics, unknown disturbances, and unknown physical parameters of the controlled system.
机译:在这项研究中,我们为具有未知动力学,未知物理参数以及受到未知和不可预测干扰的四旋翼无人机(UAV)开发了严格的跟踪控制方法。为了更好地估计未知函数,设计了七个区间类型2自适应模糊系统(IT2-AFS)和五个自适应系统。然后,介绍了一种新的IT2自适应模糊到达滑模系统(IT2-AFRSMS),该系统使用IT2-AFS生成最优的平滑自适应模糊到达滑模控制律(AFRSMCL)。 AFRSMCL的设计方法可确保有效地估计其增益。因此,尽管存在近似误差和作用于四旋翼动力学的所有干扰,但全球提出的控制定律可以有效地实现跟踪控制的预定性能,同时避免出现颤动现象。利用Lyapunov的稳定性分析来设计适应律。仿真实例用于验证所提出的控制方法的鲁棒性和有效性。获得的结果证实了尽管受控系统的动力学,未知扰动和物理参数未知,但在保证闭环动力学的跟踪收敛性和稳定性方面的数学分析结果。

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