• DocumentCode
    2731383
  • Title

    Deployment and retrieval simulation of a single tether satellite system

  • Author

    Carter, J. Theron ; Greene, Michael

  • Author_Institution
    Dept. of Electr. Eng., Auburn Univ., AL, USA
  • fYear
    1988
  • fDate
    0-0 1988
  • Firstpage
    657
  • Lastpage
    660
  • Abstract
    The Getaway Tether Experiment (GATE) is a single-tether satellite system for the study of tether dynamics and electrodynamic technology. One goal of GATE is to measure and control tether disturbances such as those induced by micrometeorite impact, using an active reel type deployer that can retrieve and deploy the tether. A computer simulation of the retrieval and deployment characteristics is essential in properly designing a closed-loop controller for the tethered system. A simulation of a single-tether system has been written which allows the tether to be actively reeled in (retrieval) or passively reeled out (deployment) of the mother subsatellite. Simulation results are presented which show the effects of retrieval and deployment on the system. Three cases are considered: exponential retrieval rate, constant retrieval rate, and pulsed deployment.<>
  • Keywords
    aerospace computing; aerospace control; artificial satellites; digital simulation; GATE; Getaway Tether Experiment; aerospace computing; aerospace control; closed-loop controller; deployment; micrometeorite impact; retrieval simulation; single tether satellite system; Aerodynamics; Artificial satellites; Computational modeling; Computer simulation; Control systems; Electrodynamics; Equations; Lagrangian functions; Potential energy; Springs;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    System Theory, 1988., Proceedings of the Twentieth Southeastern Symposium on
  • Conference_Location
    Charlotte, NC, USA
  • ISSN
    0094-2898
  • Print_ISBN
    0-8186-0847-1
  • Type

    conf

  • DOI
    10.1109/SSST.1988.17130
  • Filename
    17130