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Optimal path planning of redundant free-floating revolute-jointed space manipulators with seven links

机译:具有七个链接的冗余自由浮动式旋转关节空间操纵器的最优路径规划

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The path planning of free-floating manipulators is of great interest in space operations. The manipulators in the free-floating mode exhibit nonholonomic characteristics due to the nonintegrability of the angular momentum, which makes the problem complicated. This paper analyzes the path planning of redundant, free-floating space manipulators with revolute joints and 7 degrees of freedom. The primary task of manipulators is to move the manipulator arms so that the desired end-effector position and orientation can be achieved. The motion of the manipulators can produce an attitude disturbance of the base, which has an adverse impact on the spacecraft operation. Thus, it is necessary to minimize the base attitude disturbance in order to reduce the fuel consumption for attitude maintenance. Practically, the path planning of redundant free-floating manipulators with higher degrees of freedom (7 degrees of freedom in this paper) in three-dimensional space is more complicated than path planning with fewer degrees of freedom, including planar or fixed base cases. This paper provides a tractable planning method to solve this problem, which could avoid the pseudo inverse of the Jacobian matrix. The sine functions, whose arguments are the polynomial functions with unknown coefficients, are used to specify the joint paths. The PSODE algorithm (particle swarm optimization combined with differential evolution) is applied to optimize the unknown coefficients of the polynomials in order to achieve the desired end-effector position and orientation and simultaneously minimize the base attitude disturbance. The simulations demonstrate that this method could provide satisfactory smooth paths for redundant free-floating space manipulators.
机译:自由浮动操纵器的路径规划在太空操作中引起了极大的兴趣。由于角动量的不可积分性,处于自由浮动模式的操纵器表现出非完整的特性,这使问题变得复杂。本文分析了具有旋转关节和7个自由度的冗余,自由浮动空间机械臂的路径规划。机械手的主要任务是移动机械臂,以便获得所需的末端执行器位置和方向。机械手的运动会产生基座的姿态干扰,这会对航天器的运行产生不利影响。因此,有必要使基本姿态干扰最小化以减少姿态维持的燃料消耗。实际上,在三维空间中具有较高自由度(本文中为7个自由度)的冗余自由浮动机械手的路径规划要比具有较少自由度的路径规划(包括平面或固定基础情况)更为复杂。本文提供了一种解决该问题的可行规划方法,可以避免雅可比矩阵的伪逆。正弦函数(其参数是系数未知的多项式函数)用于指定关节路径。为了获得所需的末端执行器位置和方向,同时最小化基本姿态扰动,应用了PSODE算法(粒子群优化与微分进化相结合)来优化多项式的未知系数。仿真表明,该方法可以为冗余的自由浮动空间机械手提供令人满意的平滑路径。

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