Observer design for satellite angular rate estimation using the state-dependent riccati equation method PROJECT TITLE :Observer design for satellite angular rate estimation using the state-dependent riccati equation methodABSTRACT:The matter of estimating the angular rate of a satellite is taken into account. A nonlinear observer primarily 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 springs 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. Did you like this research project? To get this research project Guidelines, Training and Code... Click Here facebook twitter google+ linkedin stumble pinterest Overview of Wireless Microphones—Part II: Frequency Bands, Interference, and Regulation C/A code cross-correlation at a high doppler offset