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Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance

机译:受到阵风干扰的欠驱动四旋翼直升机的稳定和轨迹跟踪控制

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The control of quadrotor helicopter has been a great challenge for control engineers and researchers since quadrotor is an underactuated and a highly unstable nonlinear system. In this paper, the dynamic model of quadrotor has been derived and a so-called robust optimal backstepping control (ROBC) is designed to address its stabilization and trajectory tracking problem in the existence of external disturbances. The robust controller is achieved by incorporating a prior designed optimal backstepping control (OBC) with a switching function. The control law design utilizes the switching function in order to attenuate the effects caused by external disturbances. In order to eliminate the chattering phenomenon, the sign function is replaced by the saturation function. A new heuristic algorithm namely Gravitational Search Algorithm (GSA) has been employed in designing the OBC. The proposed method is evaluated on a quadrotor simulation environment to demonstrate the effectiveness and merits of the theoretical development. Simulation results show that the proposed ROBC scheme can achieve favorable control performances compared to the OBC for autonomous quadrotor helicopter in the presence of external disturbances.
机译:对于四旋翼直升机来说,由于四旋翼是一个驱动不足且高度不稳定的非线性系统,因此对控制工程师和研究人员来说是一个巨大的挑战。在本文中,推导了四旋翼的动力学模型,设计了一种所谓的鲁棒最优反推控制(ROBC),以解决其在存在外部干扰的情况下的稳定性和轨迹跟踪问题。通过结合预先设计的具有开关功能的最佳反推控制(OBC),可以实现鲁棒的控制器。控制律设计利用开关功能来减弱外部干扰引起的影响。为了消除抖动现象,将符号函数替换为饱和函数。一种新的启发式算法,即引力搜索算法(GSA)已用于设计OBC。在四旋翼仿真环境下对提出的方法进行了评估,以证明该理论开发的有效性和优点。仿真结果表明,在存在外部干扰的情况下,提出的ROBC方案与自动四旋翼直升机的OBC相比具有更好的控制性能。

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