Analysis and Control of an Actuation-Redundant Parallel Mechanism Requiring Synchronization

Author:

Xi Fengfeng (Jeff)1,Moosavian Amin1,Campos Gabriel H.1,Choudhuri Upasana (Sana)1,Sun Cong Zhu (John)1,Buchkazanian Raffi1

Affiliation:

1. Department of Aerospace Engineering, Ryerson University, Toronto, ON, M5B 2K3, Canada

Abstract

Abstract Presented in this paper is a method for analysis and control of an actuation-redundant parallel mechanism requiring synchronization. The said mechanism is made up of two branches that are connected to drive a common end-effector with only one degree-of-freedom of motion. The two actuators must share the load exerted on the common end-effector during motion. The underlying problem is to synchronize the motion of the two actuators while balancing the forces on them so that the entire mechanism can move smoothly under the applied load on the end-effector. Due to the space limitation, the two branches are geometrically different leading to opposite force profiles for the two actuators. The proposed method combines the mechanism kinematics with force analysis. First, a closed-form solution is derived that relates the actuator strokes to the rotation angle of the end-effector. Second, a velocity relationship is obtained to relate the actuator velocities to the angular velocity of the end-effector. Third, a force relationship is established relating the actuator loads to the external load. Fourth, a control strategy is designed to synchronize the motion of the two actuators while maintaining the force balance between them to avoid the problem of motion mismatching and force fighting that could lead to the failure of the mechanism. A prototype was built and tested with the proposed method, which is also presented in this paper.

Funder

Natural Sciences and Engineering Research Council of Canada

Publisher

ASME International

Subject

Mechanical Engineering

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A Dynamic Loading Mechanism for a Morphing Winglet;Journal of Mechanisms and Robotics;2022-11-24

2. Dynamic Loading of an Aircraft Morphing Winglet;AIAA SCITECH 2022 Forum;2022-01-03

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