SPHERES tethered formation flight testbed: Application to NASA's SPECS mission

Soon Jo Chung, Edmund M. Kong, David W. Miller

Research output: Contribution to journalConference articlepeer-review

Abstract

This paper elaborates on theory and experiment of the formation flight control for the future space-borne tethered interferometers. The nonlinear equations of multi-vehicle tethered spacecraft system are derived by Lagrange equations and decoupling method. The preliminary analysis predicts unstable dynamics depending on the direction of the tether motor. The controllability analysis indicates that both array resizing and spin-up are fully controllable only by the reaction wheels and the tether motor, thereby eliminating the need for thrusters. Linear and nonlinear decentralized control techniques have been implemented into the tethered SPHERES testbed, and tested at the NASA MSFC's flat floor facility using two and three SPHERES configurations. The nonlinear control using feedback linearization technique performed successfully in both two SPHERES in-line configuration and three triangular configuration while varying the tether length. The relative metrology system, using the ultra sound metrology system and the inertial sensors as well as the decentralized nonlinear estimator, is developed to provide necessary state information.

Original languageEnglish (US)
Article number58990L
Pages (from-to)1-13
Number of pages13
JournalProceedings of SPIE - The International Society for Optical Engineering
Volume5899
DOIs
StatePublished - 2005
EventUV/Optical/IR Space Telescopes: Innovative Technologies and Concepts II - San Diego, CA, United States
Duration: Jul 31 2005Aug 1 2005

Keywords

  • Formation flight
  • Space tether
  • Stellar interferometer

ASJC Scopus subject areas

  • Electronic, Optical and Magnetic Materials
  • Condensed Matter Physics
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

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