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Novel reaction control techniques for redundant space manipulators: Theory and simulated microgravity tests
Authors:Silvio Cocuzza  Isacco Pretto  Stefano Debei
Institution:1. CISAS “G. Colombo”—Center of Studies and Activities for Space, Università degli Studi di Padova, via Venezia 15, Padova 35131, Italy;2. Deparment of Mechanical Engineering, Università degli Studi di Padova, via Venezia 1, Padova 35131, Italy;1. Astrodynamics and Control Lab., Department of Astronomy, Yonsei University, 120-749 Seoul, Republic of Korea;2. School of Aerospace & Mechanical Engineering, Korea Aerospace University, 412-791 Gyeonggi-do, Republic of Korea;1. DIAEE, University of Rome “La Sapienza”, Italy;2. DIMA, University of Rome “La Sapienza”, Italy;1. Dirección de Ingeniería en Redes y Telecomunicaciones, Universidad Politécnica del Estado de Guerrero (UPEG), Puente Campuzano, Carretera Federal Iguala-Taxco K.M. 105, C.P. 40321 Taxco de Alarcón, Guerrero, Mexico;2. Tecnológico Nacional de México/CENIDET, Interior Internado Palmira S/N, Col. Palmira, C.P. 62490 Cuernavaca, Morelos, Mexico;3. CONACyT-Tecnológico Nacional de México/CENIDET, Interior Internado Palmira S/N, Col. Palmira, C.P. 62490 Cuernavaca, Morelos, Mexico;4. Department of Information Technology, Faculty of Computing and Information Technology, King Abdulaziz University, Jeddah, Saudi Arabia
Abstract:This paper presents two novel redundancy resolution schemes aimed at locally minimizing the reaction torque transferred to the spacecraft during manipulator manoeuvres. The subject is of particular interest in space robotics because reduced reactions result in reduced energy consumption and longer operating life of the attitude control system. The first presented solution is based on a weighted Jacobian pseudoinverse and is derived by using Lagrangian multipliers. The weight matrix is defined by means of the inertia matrix which appears in the spacecraft reaction torque dynamics. The second one is based on a least squares formulation of the minimization problem. In this formulation the linearity of the forward kinematics and of the reaction torque dynamics equations with respect to the joint accelerations is used. A closed-form solution is derived for both the presented methods, and their equivalence is proven analytically. Moreover, the proposed solutions, which are suitable for real-time implementation, are extended in order to take into account the physical limits of the manipulator joints directly inside the solution algorithms. A software simulator has been developed in order to simulate the performance of the presented solutions for the selected test cases. The proposed solutions have then been experimentally tested using a 3D free-flying robot previously tested in an ESA parabolic flight campaign. In the test campaign the 3D robot has been converted in a 2D robot thanks to its modularity in order to perform planar tests, in which the microgravity environment can be simulated without time constraints. Air-bearings are used to sustain the links weight, and a dynamometer is used to measure the reaction torque. The experimental validation of the presented inverse kinematics solutions, with an insight on the effect of joint flexibility on their performance, has been carried out, and the experimental results confirmed the good performance of the proposed methods. In particular, two test cases have been analyzed in order to validate and evaluate the performance of both the unconstrained solution and the solution which takes into account the robot physical limits.
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