Abstract:
On-orbit service technologies are used widely in the fields of satellite maintenance, large space module assembly, and space debris removal etc. These call for the application of a space robot equipped with grippers to perform tasks in the particularly harsh space environment. There exist three challenging issues in terms of satellite maintenance with space robots, i.e., i) how to design dexterous manipulating mechanisms with high stiffness for complex operating missions? ii) how to perform the dynamic control, combining the satellite and manipulating robots? iii) how to simulate the zero-gravity environment on ground for the verification of the design and control of manipulating robots? To handle these challenges, the speaker’s team has conducted systematic and in-depth research over the past decade.
This speech will introduce the mechanism design, control method and ground verification test of space manipulating robots. First, the design of space robotic manipulator, multi-functional end-effectors, and tool changer is presented. The manipulator utilizes a novel foldable serial-parallel hybrid mechanism, which is connected in a series by a 3-DOF parallel part with 1-PU&2-PUS configurations and a 4- DOF serial part with a 4R configuration. The multi-functional end-effectors can carry out all kinds of missions during satellite maintenance, such as detumbling, capturing and inspecting. Second, a control scheme for the hybrid manipulator with the end-effectors to capture a non-cooperative target in a zero-gravity environment is proposed, including three modules: admittance control, motion estimation of the target satellite, and feedforward of the reaction forces. Finally, a hardware-in-the-loop (HIL) simulation system with industrial robots is established and the zero-gravity simulating methodology is proposed. During the HIL simulation, a great challenge is to handle simulation divergence due to intrinsic time delay between the measured forces and the simulation driven reaction of the robot. A novel compensation strategy based on contact stiffness identification and damping amendment is proposed to eliminate the effects of time delays. In terms of the compensating method, an energy observer is designed to monitor the energy flow and an energy controller (EC) is established. The EC acts a variable damping and thus the contact damping is amended. Utilizing the presented method, space robotic operations with high fidelity of both contact force and contact velocity are reproduced on the presented HIL simulation system. In addition, the fully physical experiments based on air-bearing testbeds have conducted, which also confirm the validity of the proposed design and control methods.