Spinning-Base Space Robot for Seamless Capture and Stabilization of Rotating Objects

IF 4.6 2区 计算机科学 Q2 ROBOTICS
Farhad Aghili
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Abstract

This paper introduces an innovative guidance and control method for simultaneously capturing and stabilizing a target satellite using a spinning-base servicing satellite equipped with a robotic manipulator, joint locks, and reaction wheels (RWs). We assume the target satellite reaches a state of minimum kinetic energy due to the slow dissipation of energy caused by internal friction, resulting in a pure major axis spin. The method involves controlling the RWs of the servicing satellite to replicate the spinning motion of the target satellite while locking the manipulator's joints to achieve spin-matching. This maneuver makes the target stationary with respect to the rotating frame of the servicing satellite located at its center-of-mass (CoM), simplifying the robot capture trajectory planning and eliminating post-capture trajectory planning entirely. In the next phase, the joints are unlocked, and a coordination controller drives the robotic manipulator to capture the target satellite while maintaining zero relative rotation between the servicing and target satellites. The spin stabilization phase begins after completing the capture phase, where the joints are locked to form a single tumbling rigid body consisting of the rigidly connected servicing and target satellites. An optimal controller applies negative control torques to the RWs to dampen out the tumbling motion of the interconnected satellites as quickly as possible, subject to the actuation torque limit of the RWs and the maximum torque and force exerted by the manipulator's end-effector.
用于无缝捕捉和稳定旋转物体的旋转基座太空机器人
本文介绍了一种创新的制导和控制方法,利用配备了机器人操纵器、关节锁和反作用轮(RW)的旋转基座服务卫星,同时捕获和稳定目标卫星。我们假设目标卫星由于内部摩擦导致能量耗散缓慢而达到最小动能状态,从而形成纯主轴旋转。该方法包括控制服务卫星的反作用力轮复制目标卫星的旋转运动,同时锁定操纵器的关节以实现自旋匹配。这一操作使目标相对于位于其质量中心(CoM)的服务卫星旋转框架静止,从而简化了机器人捕获轨迹规划,并完全消除了捕获后的轨迹规划。在下一阶段,关节解锁,协调控制器驱动机器人机械手捕捉目标卫星,同时保持服务卫星和目标卫星之间的零相对旋转。自旋稳定阶段在捕获阶段结束后开始,在这一阶段中,各关节被锁定,以形成由刚性连接的维修卫星和目标卫星组成的单一翻滚刚体。最佳控制器对旋转翼施加负控制扭矩,以尽快抑制相互连接的卫星的翻滚运动,但须遵守旋转翼的驱动扭矩限制以及操纵器末端执行器施加的最大扭矩和力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
IEEE Robotics and Automation Letters
IEEE Robotics and Automation Letters Computer Science-Computer Science Applications
CiteScore
9.60
自引率
15.40%
发文量
1428
期刊介绍: The scope of this journal is to publish peer-reviewed articles that provide a timely and concise account of innovative research ideas and application results, reporting significant theoretical findings and application case studies in areas of robotics and automation.
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