Observer design for satellite angular rate estimation using the state-dependent riccati equation method

  • Jaehyun Jin
  • Published 2015 in
    IEEE Transactions on Aerospace and Electronic…

Abstract

The problem of estimating the angular rate of a satellite is considered. A nonlinear observer based on the state-dependent Riccati equation method is proposed. A sufficient stability condition for the convergence of the estimation error is presented. This condition is related to a state-dependent algebraic Riccati equation. The Riccati equation is derived… (More)
DOI: 10.1109/TAES.2015.140159

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