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  • VIBRATION CONTROL OF A FLEXIBLE SPACE MANIPULATOR DURING ON ORBIT OPERATIONS

    Paper number

    IAC-10.C2.3.6

    Author

    Prof. Paolo Gasbarri, Università di Roma "La Sapienza", Italy

    Coauthor

    Prof. Giovanni B. Palmerini, Universita' di Roma 'La Sapienza', Italy

    Coauthor

    Dr. Marco Sabatini, Università di Roma "La Sapienza", Italy

    Year

    2010

    Abstract
    Space manipulators are complex systems, composed by robotic arms accommodated on an orbiting platform. They can be used to perform a variety of tasks: launch of satellites; retrieval of spacecraft for inspection, maintenance and repair; movement of cargo; conduct of experiments and so on. Their operating mode requires extreme accuracy and smoothness because of   the delicate assembly  involved, the risk of potentially destructive collisions, and to the extraordinary environment, . However, in order  to respect  the mass at launch requirements, manipulators’arms  are usually very light and flexible, and their motion involves   significant structural vibrations,  expecially after a grasping  maneouver. In order to fulfill the maneuvers  of space robotic systems  it is hence necessary to properly model all the forces acting on the space robot.
    
    
    The model must  include the orbital motion, gravity gradient, aerodynamic effects, as well as flexibility of the links and of the joints. The case is furthermore  complicated by the fact that the manipulator, together with its supporting spacecraft, is  an unconstrained body.  Therefore the motion of  any of its parts affects the entire system configuration.  The governing equations of the dynamics of such robotic systems are highly nonlinear and fully coupled. The present paper aims to design and study different strategies and control devices that could  be used to  reduce the structural  vibrations of a space manipulator with flexible links during its on orbit operations like  the grasping  and  the  recovery of a large payload-to-manipulator  mass ratio.  In particular a recent wave-based -control technique will be compared with an optimized adaptative vibration control via piezo electric devices.   Performance of different strategies and algorithms will be also analyzed in terms of control effort,  flexible response of the manipulator and  computational cost.
    Abstract document

    IAC-10.C2.3.6.brief.pdf

    Manuscript document

    IAC-10.C2.3.6.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.