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首页> 外文期刊>International journal of aerospace engineering >Trajectory Planning Based on Screw Theory with Consideration of the Optimal Berth Position for a Space Robot
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Trajectory Planning Based on Screw Theory with Consideration of the Optimal Berth Position for a Space Robot

机译:基于螺杆理论的轨迹规划,考虑到空间机器人的最佳泊位位置

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摘要

Trajectory planning is a prerequisite for the tracking control of a free-floating space robot. There are usually multiple planning objectives, such as the pose of the end-effector and the base attitude. In efforts to achieve these goals, joint variables are often taken as exclusive operable parameters, while the berth position is neglected. This paper provides a novel trajectory planning strategy that considers the berth position by applying screw theory and an optimization method. First, kinematic equations at the position level are established on the basis of the product of exponential formula and the conservation of the linear momentum of the system. Then, generalized Jacobian matrices of the base and end-effector are derived separately. According to the differential relationship, an ordinary differential equation for the base attitude is established, and it is solved by the modified Euler method. With these sufficient and necessary preconditions, a parametric optimization strategy is proposed for two trajectory planning cases: zero attitude disturbance and attitude adjustment of the base. First, the berth position is transformed into the desired position of the end-effector, and its constraints are described. Joint variables are parameterized using a sinusoidal function combined with a five-order polynomial function. Then, objective functions are constructed. Finally, a genetic algorithm with a modified mutation operator is used to solve this optimization problem. The optimal berth position and optimized trajectory are obtained synchronously. The simulation of a planar dual-link space robot demonstrates that the proposed strategy is feasible, concise, and efficient.
机译:轨迹规划是对自由浮动空间机器人的跟踪控制的先决条件。通常存在多种规划目标,例如末端效应器的姿势和基本姿态。在实现这些目标的努力中,联合变量通常被视为独家可操作的参数,而泊位位置被忽视。本文提供了一种新的轨迹规划策略,通过应用螺杆理论和优化方法来考虑泊位位置。首先,基于指数公式的乘积和系统的线性动量的乘积建立位置水平的运动方程。然后,碱基和末端效应器的广义雅可族族基质分别导出。根据差异关系,建立了基本姿态的普通微分方程,并通过修改的欧拉方法解决。利用这些充分和必要的前提条件,为两个轨迹规划案例提出了参数优化策略:零姿态干扰和基地的态度调整。首先,将泊位位置转化为末端效应器的所需位置,并描述其约束。使用正弦函数与五阶多项式功能相结合的联合变量参数化。然后,构建客观函数。最后,使用具有修改的突变算子的遗传算法来解决该优化问题。相同地获得最佳泊位位置和优化的轨迹。平面双连杆空间机器人的仿真表明,所提出的策略是可行的,简洁和高效的。

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  • 来源
    《International journal of aerospace engineering 》 |2019年第4期| 1034705.1-1034705.14| 共14页
  • 作者

    Wang Yong; Liao Ying; Gong Kejie;

  • 作者单位

    Natl Univ Def Technol Coll Aerosp Sci & Engn 109 Deya Rd Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Coll Aerosp Sci & Engn 109 Deya Rd Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Coll Aerosp Sci & Engn 109 Deya Rd Changsha 410073 Hunan Peoples R China;

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  • 正文语种 eng
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