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Compensation of base disturbance using optimal trajectory planning of dual-manipulators in a space robot

机译:使用空间机器人的双控器最优轨迹规划基础扰动的补偿

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This paper presents a trajectory planning algorithm for a space robot with dual-manipulators. Here one manipulator of the space robot captures a target, and another manipulator is free. In this case, this study uses one manipulator as the mission manipulator to capture the target, and another as the balance manipulator aiming at the compensation of the pose disturbance. For this method, a novel trajectory planning algorithm applied to the balance manipulator is presented. The trajectory planning problem is transformed into series of problems of the optimal state solution, and then the iterative algorithms for the trajectory planning are designed. In the iterative algorithms, the bias force on the spacecraft base caused by the balance manipulator is used as the compensation force. Then, to calculate the expected compensation force and torque, a pose control law for the spacecraft base is introduced. The expected compensation force and torque provide equality constraints for optimization problems, which implies that the trajectory planning algorithm compensates for not only the disturbance generated by the manipulator's motion, but also environmental disturbances. This is because the expected compensation force and torque depend on the pose change of the spacecraft base rather than the type of the disturbance. Numerical simulation was carried out to analyze the proposed trajectory planning method. It was observed that the method greatly reduces the disturbance of Manipulator A on the spacecraft base. These results validated the effectiveness of the proposed method for the trajectory planning to make the spacecraft base disturbance up to minimum. (C) 2018 COSPAR. Published by Elsevier Ltd. All rights reserved.
机译:本文介绍了具有双控器的空间机器人的轨迹规划算法。这里,空间机器人的一个操纵器捕获目标,另一个机械手是自由的。在这种情况下,本研究使用一个机器人作为使命操纵器来捕获目标,另一个是瞄准姿势干扰补偿的余额操纵器。对于这种方法,介绍了应用于余量操纵器的新型轨迹规划算法。轨迹规划问题转变为最佳状态解决方案的串行问题,然后设计了轨迹规划的迭代算法。在迭代算法中,由余量操纵器引起的航天器底座上的偏置力用作补偿力。然后,为了计算预期的补偿力和扭矩,引入了航天器基座的姿势控制法。预期补偿力和扭矩为优化问题提供平等约束,这意味着轨迹规划算法不仅补偿了机械手运动产生的干扰,还可以补偿环境干扰。这是因为预期的补偿力和扭矩取决于航天器基地的姿势变化而不是干扰的类型。进行数值模拟,以分析所提出的轨迹规划方法。观察到该方法大大降低了操纵器A在航天器基础上的干扰。这些结果验证了所提出的方法对轨迹规划的有效性,使航天器基础干扰最小。 (c)2018 Cospar。 elsevier有限公司出版。保留所有权利。

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