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首页> 外文期刊>Journal of robotics >Dynamics Modeling and Control of a Quadrotor with Swing Load
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Dynamics Modeling and Control of a Quadrotor with Swing Load

机译:具有回转载荷的四旋翼动力学建模与控制

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Nowadays, aerial robots or Unmanned Aerial Vehicles (UAV) have many applications in civilian and military fields. For example, of these applications is aerial monitoring, picking loads and moving them by different grippers. In this research, a quadrotor with a cable-suspended load with eight degrees of freedom is considered. The purpose is to control the position and attitude of the quadrotor on a desired trajectory in order to move the considered load with constant length of cable. So, the purpose of this research is proposing and designing an antiswing control algorithm for the suspended load. To this end, control and stabilization of the quadrotor are necessary for designing the antiswing controller. Furthermore, this paper is divided into two parts. In the first part, dynamics model is developed using Newton-Euler formulation, and obtained equations are verified in comparison with Lagrange approach. Consequently, a nonlinear control strategy based on dynamic model is used in order to control the position and attitude of the quadrotor. The performance of this proposed controller is evaluated by nonlinear simulations and, finally, the results demonstrate the effectiveness of the control strategy for the quadrotor with suspended load in various maneuvers.
机译:如今,空中机器人或无人飞行器(UAV)在民用和军事领域有许多应用。例如,这些应用包括空中监视,拾取负载并通过不同的夹具移动它们。在这项研究中,考虑了具有八个自由度的电缆悬吊负载的四旋翼。目的是在所需的轨迹上控制四旋翼飞机的位置和姿态,以便在恒定长度的电缆上移动所考虑的负载。因此,本研究的目的是提出并设计一种针对悬吊载荷的防摆控制算法。为此,在设计防摆控制器时必须控制和稳定四旋翼。此外,本文分为两部分。在第一部分中,使用牛顿-欧拉公式建立了动力学模型,并与拉格朗日方法进行了比较验证了所得到的方程。因此,使用基于动态模型的非线性控制策略来控制四旋翼的位置和姿态。通过非线性仿真对所提出的控制器的性能进行了评估,最后,结果证明了在不同操纵下具有悬浮负载的四旋翼控制策略的有效性。

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