• DocumentCode
    158589
  • Title

    Ground tests of a rendezvous maneuver based on visual servoing

  • Author

    Palmerini, G.B. ; Sabatini, M. ; Pisculli, A. ; Gasbarri, P.

  • Author_Institution
    DIAEE Dept. of Astronaut., Electr. Eng. & Energetics, Sapienza Univ. di Roma, Rome, Italy
  • fYear
    2014
  • fDate
    1-8 March 2014
  • Firstpage
    1
  • Lastpage
    14
  • Abstract
    The problem of autonomous space rendezvous and docking is faced from both a numerical and an experimental point of view. A 2D free floating chaser platform has been equipped with a docking system and a camera dedicated to relative navigation with respect to a target platform. The image processing and filtering algorithms are processed in real time so that the target is identified and tracked, and the relative longitudinal and lateral displacements are evaluated. The GNC algorithms are first tested by means of a numerical tool where a multibody plant is modeled, so that contact forces and relevant post-contact dynamics can be accurately predicted. The experimental tests of the same GNC algorithms show the accuracy of the vision-based navigation, and the robustness of the docking strategy even with respect to some disturbances, such as the plume impingement effect, that were not included in the numerical model.
  • Keywords
    filtering theory; object detection; space vehicles; visual servoing; 2D free floating chaser platform; GNC algorithms; autonomous space rendezvous; docking strategy; docking system; filtering algorithms; image processing algorithms; lateral displacements; longitudinal displacements; multibody plant; numerical tool; plume impingement effect; post-contact dynamics; relative navigation; vision-based navigation; visual servoing; Accuracy; Electromagnets; Kinematics; Measurement errors; Navigation; Prediction algorithms; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2014 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5582-4
  • Type

    conf

  • DOI
    10.1109/AERO.2014.6836473
  • Filename
    6836473