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Trajectory tracking control for a quadrotor using fuzzy PID control scheme

机译:基于模糊PID控制方案的四旋翼轨迹跟踪控制

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Quadrotor is an unmanned aerial vehicle (UAV) with high maneuverability. However, motion control of quadrotor is a challenging problem due to its nonlinear under actuated dynamics. In this paper, trajectory tracking control of quadrotor is studied for a nonlinear under actuated model. An inner-outer loop control paradigm is applied to control lateral motion of quadrotor. The outer loop generates desired forces to control lateral translations of quadrotor. While, the inner loop controls roll and pitch maneuvers. Also, analytical inversion is obtained to generate desired roll and pitch angles from desired lateral forces. A fuzzy proportional-integral-derivative (PID) control scheme is applied as the main part of the control law for all six degrees of freedom (DOFs). Also a feedback linearization term is considered in the control laws to compensate model nonlinearities. Performance of the proposed controller is examined by numerical simulation and is compared with a conventional PID controller.
机译:Quadrotor是具有高机动性的无人机(UAV)。然而,由于四转子的非线性在致动动力学下,其运动控制是一个具有挑战性的问题。针对非线性模型,研究了四旋翼的轨迹跟踪控制问题。内外环控制范例应用于控制四旋翼的横向运动。外环产生所需的力来控制四旋翼的横向平移。同时,内部循环控制侧倾和俯仰操纵。同样,获得了解析反演,以根据所需的侧向力生成所需的侧倾角和俯仰角。模糊比例积分微分(PID)控制方案被用作所有六个自由度(DOF)的控制律的主要部分。在控制定律中还考虑了反馈线性化项,以补偿模型非线性。通过数值模拟检查了所提出控制器的性能,并将其与常规PID控制器进行了比较。

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