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Control performance simulation of a space robotic joint by estimation of motor fast shaft position and speed via a seven-state nonlinear Kalman Filter

机译:通过七态非线性卡尔曼滤波器估算电机快轴位置和速度来模拟太空机器人关节的控制性能

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This paper presents the results of a control performance simulation for a robotic joint, sized for space applications, via a seven-state nonlinear Kalman Filter. This leads to better estimation of joint mechanical state and in particular the motor fast shaft position and speed which are directly used for the commutation and speed control functions. In the presented simulation the sensor information assumed available to the Kalman Filter are the ones normally available in the drive electronics, like currents and voltages, motor windings temperatures and speed information of the joint output shaft, downstream the reducer, derived from an output shaft absolute position sensor. The general technique to utilize a Kalman Filter estimator to support the reconstruction of the motor shaft mechanical state have been already proposed in different variants and could be considered for robotic applications in hostile environments where active electronics, inclusive hall sensors, installed in the robotic arm should be reduced to the minimum and where the need to keep the arm design as light and as simple as possible suggests to reduce the number of components into the joint to the minimum. Possible scenarios are represented by Moon and Mars robotic exploration where the extreme environmental conditions of certain areas and the convenience to keep the mass of the robotic arm as low as possible suggest the use of techniques similar to the one discussed.
机译:本文介绍了通过七态非线性卡尔曼滤波器对大小适合空间应用的机器人关节进行控制性能仿真的结果。这样可以更好地估算关节机械状态,尤其是可以直接用于换向和速度控制功能的电动机快速轴位置和速度。在所提出的仿真中,假定卡尔曼滤波器可用的传感器信息是驱动电子设备中通常可用的信息,例如电流和电压,电动机绕组温度和减速器下游联轴器输出轴的速度信息(从输出轴绝对值得出)位置传感器。已经提出了利用卡尔曼滤波器估计器来支持电动机轴机械状态重构的通用技术,并且已经在不同的变体中提出了该技术,并且可以考虑将其用于敌对环境中的机器人应用,在这种环境中,应将主动电子装置(包括霍尔传感器)安装在机械臂中尽量减少臂架的重量,并尽可能将臂设计保持在尽可能轻巧的位置,这建议将关节中的零件数量减少到最小。月球和火星机器人探索代表了可能的场景,其中某些区域的极端环境条件以及将机器人手臂的质量保持得尽可能低的便利性,建议使用与所讨论的技术类似的技术。

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  • 来源
    《Aerotecnica missili & spazio》 |2013年第2期|41-51|共11页
  • 作者单位

    Selex ES, Viale Europa, 20014 Nerviano (MI), Italy;

    Politecnico di Milano, Dipartimento di Scienze e Tecnologie Aerospaziali, Via la Masa 34, 20156 Milano, Italia;

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