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Differential-Flatness and Control of Quadrotor(s) with a Payload Suspended through Flexible Cable(s)

机译:具有有效载荷的四旋翼的差分平坦性和控制   通过柔性电缆悬挂

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摘要

We present the coordinate-free dynamics of three different quadrotor systems: (a) single quadrotor with a point-mass payload suspended through a flexiblecable; (b) multiple quadrotors with a shared point-mass payload suspendedthrough flexible cables; and (c) multiple quadrotors with a shared rigid-bodypayload suspended through flexible cables. We model the flexible cable(s) as afinite series of links with spherical joints with mass concentrated at the endof each link. The resulting systems are thus high-dimensional with highdegree-of-underactuation. For each of these systems, we show that the dynamicsare differentially-flat, enabling planning of dynamically feasibletrajectories. For the single quadrotor with a point-mass payload suspendedthrough a flexible cable with five links (16 degrees-of-freedom and 12degrees-of-underactuation), we use the coordinate-free dynamics to develop ageometric variation-based linearized equations of motion about a desiredtrajectory. We show that a finite-horizon linear quadratic regulator can beused to track a desired trajectory with a relatively large region ofattraction.
机译:我们介绍了三种不同的四旋翼系统的无坐标动力学:(a)具有通过柔性电缆悬挂的点质量有效载荷的单四旋翼; (b)多个四点旋翼,通过挠性电缆悬挂一个共享的点质量载荷; (c)多个四旋翼,它们通过挠性电缆悬挂,具有共享的刚体有效载荷。我们将柔性电缆建模为具有球形接头的一系列有限链节,质量集中在每个链节的末端。因此,生成的系统是高维度的,而欠驱动程度很高。对于这些系统中的每一个,我们都表明动力学是差分平坦的,从而可以规划动态可行的轨迹。对于具有四点负载有效载荷的单四旋翼飞机,它通过具有五个链接(16个自由度和12个欠驱动度)的柔性电缆悬挂,我们使用无坐标动力学来开发基于年龄变化的基于线性的运动方程所需的轨迹。我们表明,可以使用有限水平的线性二次调节器来跟踪具有相对较大吸引力区域的期望轨迹。

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