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We propose a suitable parametrization for the modeling of sensor failures in flight control applications. The failures include bias, drift, loss of accuracy, calibration error, and freezing. Based on this parameterization, reconfigurable control algorithms are designed and stability and robustness analysis is carried out. Properties of the proposed algorithms are illustrated through simulations.
American Control Conference, 2002. Proceedings of the 2002 (Volume:3 )
Date of Conference: 2002