Affordable Access

Stabilization of Periodic Solutions in a Thedered Satellite System by Damping Injection

Authors
Publication Date
Keywords
  • A Spacecraft With Electrodynamic Tether Orbiting The Earth Will Be Subject To A Periodic Forcing Ter
  • The Periodic Forcing Term Leads To A Family Of Unstable Periodic Solutions For A Tether Carrying A C
  • This Paper Presents A Control Design For Stabilizing These Periodic Solutions
  • The Design Consists Of A Control Law For Stabilising The Open-Loo Equibrilibrium And A Bias Term Whi
  • The Tether Needs To Be Positioned Away From Open-Loop Equilibrium For The Tether To Affect The Orbit
  • An Approximation Of The Periodic Solutions Of The Closed Loop System Is Found As A Series Expansion
  • The Stability Of The Solutions Is Investigated Using Linear Floquet Analysis Of The Variational Equa

Abstract

Stabilization of Periodic Solutions in a Thedered Satellite System by Damping Injection - DTU Orbit (20/04/14) Stabilization of Periodic Solutions in a Thedered Satellite System by Damping Injection - DTU Orbit (20/04/14) Larsen, MB & Blanke, M 2009, 'Stabilization of Periodic Solutions in a Thedered Satellite System by Damping Injection'. in Proceedings of European Control Conference 2009: ECC 2009. pp. 2169-2174.

There are no comments yet on this publication. Be the first to share your thoughts.