四旋翼与附加三自由度机械臂的协同控制

H. Ghasemi, Saeed Ansari-Rad, A. Kalhor, M. T. Masouleh
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摘要

自主四旋翼飞行系统在救援、检查设备等各种任务中引起了相当大的关注。因此,已采用各种控制方法使这些装置悬停。近年来,为了扩大四旋翼的应用范围,包括拾取和放置机械臂,需要对动力学方程和控制程序进行分析。然而,考虑到耦合系统是机器人-机器人相互作用的情况,由于动力学方程的复杂性,这些最先进的飞行系统很少受到关注。此外,飞行时间费用是附加臂飞行系统的另一个关键问题,由于臂负载过大和动力源限制,需要有效解决。为此,本文得到了带有三连杆臂的四旋翼的动力学方程,以便设计合适的控制方法。在此基础上,通过将四旋翼稳定在理想的协调位置并跟踪机械臂的理想路径,成功地解决了机器人与机器人交互的主要挑战——动态交互问题。在此基础上,提出了一种线性二次型调节器(LQR)来解决飞行时间问题,该方法通过对状态输入权重矩阵赋最优值来减小手臂连杆的运动,从而有效地增加飞行时间。为了证明该方法的优越性,在相同的条件下实现了两种著名的控制方法,即滑模控制(SMC)和极点配置。在Matlab软件的仿真中,通过采用不同的指标对上述方法的性能进行了比较,其中可以推断,尽管存在类似风条件的外力,但与SMC和Pole Placement方法相比,所提出的LQR方法的运动指数降低了24.14%,其跟踪指数与SMC和Pole Placement方法大致相似。
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Control of Quad-rotor in Cooperation with an Attached 3-DOF Manipulator
Autonomous quad-rotor flight systems have grabbed considerable attention for varied missions in rescue, inspection devices, and so forth. Accordingly, various control methods have been employed for hovering these devices. Recently, in order to extend the applications of quad-rotors, including, among the others, the pick-and-place, a robotic arm has been attached, which requires the analysis of both dynamic equations and control procedures. However, considering the coupled system as a case of robot-robot interaction, these state-of-the-art flight systems have rarely received attention due to much higher complexity of dynamic equations. Moreover, flight time expense is revealed as another critical issue in the flight systems with the attached arm, which requires effective solution due to excessive arm loads and power source limitations. To this end, in this paper, the dynamic equations of quad-rotor with a 3-link arm are obtained in order to be employed in designing suitable control methods. In this regard, by stabilizing the quad-rotor in desired coordinations and tracking desired paths for robotic arm, the dynamic interaction as the main challenge of the robot-robot interaction is successfully handled. Thereafter, a Linear Quadratic Regulator (LQR) is proposed to tackle the flight time issue in which by assigning optimal values to the state input weighting matrix, the motion of arm links reduced and as the result, the flight time effectively increases. In order to demonstrate the superiority of the proposed method, two well-known control approaches, namely, Sliding Mode Control (SMC) and Pole Placement are implemented in the same conditions. In simulation with Matlab software, the performance of the forgoing methods is compared by employing different indices, where it is inferred that despite presence of an external force resembling windy condition, the proposed LQR decreases the motion index by 24.14% in compare with SMC and Pole Placement methods, with approximately similar tracking index to them.
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