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Extended Kalman Filter Based States Estimation of Unmanned Quadrotors for Altitude-Attitude Tracking Control

机译:基于扩展卡尔曼滤波器的无人四旋翼飞行器状态估计

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In this paper, state variables estimation and Fuzzy Sliding Mode Control (FSMC) are presented in order to estimate the state variables and altitude-attitude tracking control in presence of internal and external disturbances for unmanned quadrotor. The main idea of the proposed control strategy is the development of an Extended Kalman Filter (EKF) for the observation of the states. Fuzzy logic systems are used to adapt the unknown switching-gains to eliminate the chattering phenomenon induced by Sliding Mode Control (SMC). The stability of the system is guaranteed in the sense of Lyapunov. The effectiveness and robustness of the proposed controller-observer scheme that takes into account internal and external disturbances are demonstrated on computer simulation using Matlab environment.
机译:本文提出了状态变量估计和模糊滑模控制(FSMC),以估计在存在内部和外部干扰的情况下无人四旋翼的状态变量和高度-高度跟踪控制。所提出的控制策略的主要思想是开发用于状态观察的扩展卡尔曼滤波器(EKF)。模糊逻辑系统用于调整未知的开关增益,以消除由滑模控制(SMC)引起的颤动现象。从Lyapunov的角度,可以保证系统的稳定性。使用Matlab环境进行计算机仿真,证明了考虑内部和外部干扰的控制器-观察者方案的有效性和鲁棒性。

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