Abstract

In this paper, a design of modularized flexible-joint servo control system for a space manipulator system is presented. First of all, the structure and sensor system of dual-joint is introduced. Next, the features of the hardware system of the dual-joint controller is described, as well as design details and fault tolerant mechanism. Moreover, the working principle of joint torque sensor is analyzed emphatically. The structural optimization design of the joint torque sensor is carried out with the help of the ANSYS program for weight minimization. After that, a position control strategy with joint torque feedback is provided to improve both precision and bandwidth of the control system. Finally, the performance specifications of the dual-joint control system are presented. Experimental results demonstrate the effectiveness of the compact joint servo controller for the space manipulator system.

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