Unmanned aerial vehicle reliability study. Office of the Secretary of Defense, 2003. ,
Historical Overview of Research in Reconfigurable Flight Control, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol.1, issue.4, pp.263-275, 2005. ,
DOI : 10.1243/095441005X30379
Analytical redundancy and the design of robust failure detection systems, IEEE Transactions on Automatic Control, vol.29, issue.7, pp.29-603, 1984. ,
DOI : 10.1109/TAC.1984.1103593
Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy, Automatica, vol.26, issue.3, pp.459-474, 1990. ,
DOI : 10.1016/0005-1098(90)90018-D
Supervision, fault-detection and fault-diagnosis methods ??? An introduction, Control Engineering Practice, vol.5, issue.5, pp.639-652, 1997. ,
DOI : 10.1016/S0967-0661(97)00046-4
Model-based fault diagnosis techniques: design schemes, algorithms, and tools, 2008. ,
DOI : 10.1007/978-1-4471-4799-2
Review of parity space approaches to fault diagnosis for aerospace systems, Journal of Guidance, Control, and Dynamics, vol.17, issue.2, pp.278-285, 1994. ,
DOI : 10.2514/3.21194
Fault Detection for Deep Space Satellites, AIAA Guidance, Navigation and Control Conference and Exhibit, pp.32-1570, 2009. ,
DOI : 10.2514/6.2008-7475
Nonlinear Geometric Approach to Fault Detection and Isolation in an Aircraft Nonlinear Longitudinal Model, 2007 American Control Conference, pp.5771-5776, 2007. ,
DOI : 10.1109/ACC.2007.4282876
Nonlinear FDI based on state derivatives, as provided by inertial measurement units, Proceedings of the 8th IFAC Symposium on Nonlinear Control Systems, pp.951-956, 2010. ,
DOI : 10.3182/20100901-3-IT-2016.00036
URL : https://hal.archives-ouvertes.fr/hal-00520799
Isolating incipient sensor faults and system reconfiguration in a flight control actuation system, Proc. IMechE Part G: J. Aerospace Engineering, pp.101-111, 2010. ,
DOI : 10.1243/09544100JAERO456
Fault diagnosis of inertia sensor in missile control systems, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol.220, issue.1, pp.220-51, 2006. ,
DOI : 10.1177/095441000622000104
A method for fault detection and isolation in the integrated navigation system for UAV, Measurement Science and Technology, vol.17, issue.6, pp.17-1522, 2006. ,
DOI : 10.1088/0957-0233/17/6/033
Design of residual generators and adaptive filters for the FDI of aircraft model sensors, Control Engineering Practice, vol.18, issue.5, pp.18-449, 2010. ,
DOI : 10.1016/j.conengprac.2008.11.006
Sensor Fault Detection for UAVs using a Nonlinear Dynamic Model and the IMM-UKF Algorithm, 2007 Information, Decision and Control, pp.230-235, 2007. ,
DOI : 10.1109/IDC.2007.374555
Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle, Proceedings of the IEEE International Conference on Control Applications, pp.1061-1066, 2007. ,
Efficient Nonlinear Actuator Fault Detection and Isolation System for Unmanned Aerial Vehicles, Journal of Guidance, Control, and Dynamics, vol.31, issue.1, pp.31-225, 2008. ,
DOI : 10.2514/1.31693
Fault Diagnosis of Microscope Satellite Thrusters Using H-infinity/H_ Filters, Journal of Guidance, Control, and Dynamics, vol.31, issue.3, pp.31-699, 2008. ,
DOI : 10.2514/1.31003
Robust FDI applied to thruster faults of a satellite system, Proceedings of the 17th IFAC Symposium on Automatic Control and Aerospace, 2007. ,
Fault diagnosis with matrix analysis for electrically actuated unmanned aerial vehicles, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol.18, issue.5, pp.223-543, 2009. ,
DOI : 10.1243/09544100JAERO422
Sliding mode observers for robust detection and reconstruction of actuator and sensor faults, International Journal of Robust and Nonlinear Control, vol.29, issue.5, pp.443-463, 2003. ,
DOI : 10.1002/rnc.723
An application of fault detection and isolation to a transport aircraft, Control Engineering Practice, vol.13, issue.1, pp.105-119, 2005. ,
DOI : 10.1016/j.conengprac.2004.02.006
Auxiliary Signal Design for Failure Detection, 2004. ,
DOI : 10.1515/9781400880041
Active fault diagnosis by temporary destabilization, Proceedings of the 6th IFAC Symposium on Fault Detection Supervision ans Safety for Technical Processes, pp.607-612, 2006. ,
Robust fault detection in open loop vs. closed loop, Proceedings of the 36th IEEE Conference on Decision and Control, pp.4496-4497, 1997. ,
DOI : 10.1109/CDC.1997.649678
On parametric and nonparametric fault detection in linear closed-loop systems, Proceedings of the 4th Workshop on Advanced Conrol and Diagnosis, 2006. ,
An integrated approach to controls and diagnostics using the four parameter controller, IEEE Control Systems, vol.11, issue.6, pp.22-22, 1991. ,
DOI : 10.1109/37.92987
A review of performance monitoring and assessment techniques for univariate and multivariate control systems, Journal of Process Control, vol.9, issue.1, pp.1-17, 1999. ,
DOI : 10.1016/S0959-1524(98)00031-6
Closed-loop performance monitoring using loop tuning, Journal of Process Control, vol.15, issue.2, pp.127-133, 2005. ,
DOI : 10.1016/j.jprocont.2004.06.004
Retrofit reconfigurable flight control in the presence of control effector damage, Proceedings of the 2005, American Control Conference, 2005., pp.2652-2657, 2005. ,
DOI : 10.1109/ACC.2005.1470368
A Nonlinear Fault Identification scheme for Reusable Launch Vehicles Control Surfaces, IFAC Proceedings Volumes, vol.42, issue.8, pp.492-503, 2008. ,
DOI : 10.3182/20090630-4-ES-2003.00009
URL : https://hal.archives-ouvertes.fr/hal-00338019
Modern navigation, guidance, and control processing, 1991. ,
Missile guidance and pursuit: kinematics, dynamics & control, 1998. ,
DOI : 10.1533/9781782420590
Tactical and strategic missile guidance, AIAA Progress in Astronautics and Aeronautics, 1990. ,
DOI : 10.2514/4.868948
Oscillatory failure case detection in the A380 electrical flight control system by analytical redundancy, Control Engineering Practice, vol.18, issue.9, pp.1110-1119, 2010. ,
DOI : 10.1016/j.conengprac.2009.04.003
Introduction to the DAMADICS actuator FDI benchmark study, Control Engineering Practice, vol.14, issue.6, pp.14-577, 2006. ,
DOI : 10.1016/j.conengprac.2005.06.015
A new model-free method performing closed-loop fault diagnosis for an aeronautical system, Proceedings of the 7th Workshop on Advanced Control and Diagnosis, 2009. ,
URL : https://hal.archives-ouvertes.fr/hal-00429745
Recursive time-to-go estimation for homing guidance missiles, IEEE Transactions on Aerospace and Electronic Systems, issue.1, pp.3813-3837, 2002. ,
Adaptive filtering and change detection, 2001. ,
DOI : 10.1002/0470841613
Detection of abrupt changes: theory and application, 1993. ,
URL : https://hal.archives-ouvertes.fr/hal-00008518
Automatic tuning via Kriging-based optimization of methods for fault detection and isolation, 2010 Conference on Control and Fault-Tolerant Systems (SysTol), pp.505-510, 2010. ,
DOI : 10.1109/SYSTOL.2010.5676075
URL : https://hal.archives-ouvertes.fr/hal-00520808
Robust trajectorytracking method for UAV guidance using proportional navigation, Proceedings of the IEEE International Conference on Control, Automation and Systems, pp.1404-1409, 2007. ,