2015
DOI: 10.1016/j.ifacol.2015.09.556
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IMU Sensor Fault Diagnosis and Estimation for Quadrotor UAVs

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Cited by 54 publications
(24 citation statements)
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“…Marzat J. and Avram R.C. et al proposed sensor fault detection and isolation algorithms using control model information [11] and sliding mode observer [12], respectively. The evaluation and performance of model-based fault detection and isolation algorithms always depend on the accuracy of the system model used.…”
Section: Introductionmentioning
confidence: 99%
“…Marzat J. and Avram R.C. et al proposed sensor fault detection and isolation algorithms using control model information [11] and sliding mode observer [12], respectively. The evaluation and performance of model-based fault detection and isolation algorithms always depend on the accuracy of the system model used.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, the aerodynamic coefficients highly depend on the specific aircraft structure and flight envelope, thus the corresponding FDI and estimation methods might fail in any unexpected condition [16]. In contrast, the second category adopts an aerodynamicsindependent model, e.g., the wind velocity triangle [17]- [19], the aircraft dynamic model with three-axis load factors as inputs [20]- [22], or a combination of the above two models [16], [23]. Such aerodynamics-independent models simplify the design of FDI and estimation algorithms by avoiding the use of uncertain aerodynamics, hence the corresponding algorithms can be easily configured for different aircraft without adapting to the changing aerodynamics [16], [20].…”
Section: Introductionmentioning
confidence: 99%
“…Based on fault estimation, FTC controller is reconfigured to compensate or reject faults [29,30]. For the quadrotor UAV, there have been a great deal of research [31,32]. For example, considering disturbances of unknown bounds, Chang et al [33] propose an adaptive sliding mode algorithm to deal with bias fault and noise.…”
Section: Introductionmentioning
confidence: 99%
“…(1) For the quadrotor UAV, different from the sensor fault research [31][32][33][34][35], this paper addresses the diverse sensor faults (three additive and one multiplicative faults), and simultaneously considers uncertain parameters, external disturbances, and measurement noises. (2) Different from the adaptive backstepping methods for special second-order system in [19,20], the proposed approach can be used for different kinds of systems besides quadrotor UAV.…”
Section: Introductionmentioning
confidence: 99%