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- W1650783417 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 by transforming nonlinear error dynamics into a Lipschitz nonlinearity. Observer gains are obtained from this state-dependent algebraic Riccati equation. Numerical simulations are presented to demonstrate the proposed method." @default.
- W1650783417 created "2016-06-24" @default.
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- W1650783417 date "2015-07-01" @default.
- W1650783417 modified "2023-09-27" @default.
- W1650783417 title "Observer design for satellite angular rate estimation using the state-dependent riccati equation method" @default.
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- W1650783417 doi "https://doi.org/10.1109/taes.2015.140159" @default.
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