[Alwi, H., Edwards, C. and Tan, C.P. (2011). Fault Detection and Fault Tolerant Control Using Sliding Modes, Springer-Verlag, London.10.1007/978-0-85729-650-4]Search in Google Scholar
[Athans, M. (1977). The stochastic control of the F-8c aircraft using a multiple model adaptive control (MMAC) method, Part I: Equilibrium flight, IEEE Transactions on Automatic Control 22(5): 768-780.10.1109/TAC.1977.1101599]Search in Google Scholar
[Azam, M., Pattipati, K., Allanach, J., Poll, S. and Petterson-Hine, A. (2005). In-flight fault detection and isolation in aircraft flight control systems, Proceedings of the IEEE Aerospace Conference, Big Sky, MT, USA, paper 1429.10.1109/AERO.2005.1559659]Search in Google Scholar
[Bateman, F., Noura, H. and Ouladsine, M. (2011). Active fault diagnosis and major actuator failure accommodation: Application to a UAV, in A. Balint (Ed.), Advances in Flight Control Systems, InTech, Rijeka, pp. 135-158.10.5772/15207]Search in Google Scholar
[Belcastro, C. and Chang, B.-C. (2002). Uncertainty modeling for robustness analysis of failure detection and accommodation systems, Proceedings of the IEEE American Control Conference, Anchorage, AK, USA, pp. 4776-4782.]Search in Google Scholar
[Benini, B., Castaldi, P. and Simani, S. (2009). Fault Diagnosis for Aircraft System Models: An Introduction from Fault Detection to Fault Tolerance, VDM Verlag Dr. Muller, Saarbrucken.]Search in Google Scholar
[Blanke, M., Kinnaert, M., Lunze, J. and Staroswiecki, M. (2006). Diagnosis and Fault Tolerant Control, Springer Verlag, London.]Search in Google Scholar
[Bonfè, M., Castaldi, P., Mimmo, N. and Simani, S. (2011). Active fault tolerant control of nonlinear systems: The cart-pole example, International Journal of Applied Mathematics and Computer Science 21(3): 441-455, DOI: 10.2478/v10006-011-0033-y.10.2478/v10006-011-0033-y]Search in Google Scholar
[Boskovic, J.D., Redding, J. and Mehra, R.K. (2007). Robust fault tolerant flight control using a new failure parameterization, Proceedings of the IEEE American Control Conference, New York, NY, USA, pp. 5753-5758.]Search in Google Scholar
[Brown, R.G. and Hwang, P.Y.C. (1997). Introduction to Random Signals and Applied Kalman Filtering, JohnWiley & Sons, New York, NY.]Search in Google Scholar
[Campbell, M.E., Lee, J.W., Scholte, E. and Rath Bun, D. (2007). Simulation and flight test of autonomous aircraft estimation, planning, and control algorithms, AIAA Journal of Guidance, Control, and Dynamics 30(6): 1597-1609.10.2514/1.29719]Search in Google Scholar
[Campbell, S.L. and Nikoukhah, R. (2004). Auxiliary Signal Design for Failure Detection, Princeton University Press, Princeton, NJ.10.1515/9781400880041]Search in Google Scholar
[Castaldi, P., Geri, W., Bonf`e, M., Simani, S. and Benini, M. (2010). Design of residual generators and adaptive filters for the FDI of aircraft model sensors, Control Engineering Practice 18(5): 449-495, DOI:10.1016/j.conengprac.2008.11.006.10.1016/j.conengprac.2008.11.006]Search in Google Scholar
[Chen, J. and Patton, R.J. (1999). Robust Model-Based Diagnosis for Dynamic Systems, Kluwer Academic, Boston, MA.10.1007/978-1-4615-5149-2]Search in Google Scholar
[Ducard, G. (2009). Fault-tolerant Flight Control and Guidance Systems: Practical Methods for Small Unmanned Aerial Vehicles, Advances in Industrial Control, Springer-Verlag, London.10.1007/978-1-84882-561-1]Search in Google Scholar
[Ducard, G. (2013). The SMAC fault detection and isolation scheme: Discussions, improvements, and application to a UAV, Proceedings of the IEEE 2013 Conference on Control and Fault Tolerant Systems (SysTol’13), Nice, France, pp. 480-485.]Search in Google Scholar
[Ducard, G. and Geering, H.P. (2006). A reconfigurable flight control system based on the EMMAE method, Proceedings of the IEEE American Control Conference, Minneapolis, MN, USA, pp. 5499-5504.]Search in Google Scholar
[Ducard, G. and Geering, H.P. (2008). Efficient nonlinear actuator fault detection and isolation system for unmanned aerial vehicles, AIAA Journal of Guidance, Control, and Dynamics 31(1): 225-237.10.2514/1.31693]Search in Google Scholar
[Ducard, G. and Geering, H.P. (2010). SMAC-FDI: New active fault detection and isolation scheme with high computational efficiency, Proceedings of the IEEE 2010 Conference on Control and Fault Tolerant Systems, Nice, France, pp. 30-37.]Search in Google Scholar
[Eide, P. and Maybeck, P.S. (1996). An MMAE failure detection system for the F-16, IEEE Transactions on Aerospace and Electronic Systems 32(3): 1125-1136.10.1109/7.532271]Search in Google Scholar
[Elgersma, M., Enns, D., Shald, S. and Voulgaris, P. (1998).]Search in Google Scholar
[Parameter identification for systems with redundant actuators, Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Boston, MA, USA, pp. 109-117.]Search in Google Scholar
[Elgersma, M. and Glavaski, S. (2001). Reconfigurable control for active management of aircraft system failures, Proceedings of IEEE American Control Conference, Arlington, VA, USA, pp. 2627-2639.]Search in Google Scholar
[Fekri, S., Athans, M. and Pascoal, A. (2006). Issues, progress and new results in robust adaptive control, International Journal of Adaptive Control and Signal Processing 20(10): 519-579.10.1002/acs.912]Search in Google Scholar
[Isermann, R. (2006). Fault-Diagnosis Systems, An Introduction from Fault Detection to Fault Tolerance, Springer-Verlag, Berlin/Heidelberg.10.1007/3-540-30368-5]Search in Google Scholar
[Magill, D.T. (1965). Optimal adaptive estimation of sampled stochastic processes, IEEE Transactions on Automatic Control 10(4): 434-439.10.1109/TAC.1965.1098191]Search in Google Scholar
[Maybeck, P.S. (1999). Multiple model adaptive algorithms for detecting and compensating sensor and actuator/surface failures in aircraft flight control systems, International Journal of Robust and Nonlinear Control 9(14): 1051-1070.10.1002/(SICI)1099-1239(19991215)9:14<1051::AID-RNC452>3.0.CO;2-0]Search in Google Scholar
[Maybeck, P.S. and Stevens, R.D. (1991). Reconfigurable flight control via multiple model adaptive control methods, IEEE Transactions on Aerospace and Electronic Systems 27(3): 470-479.10.1109/7.81428]Search in Google Scholar
[Möckli, M. (2006). Guidance and Control for Aerobatic Maneuvers of an Unmanned Airplane, Ph.D. thesis, Diss. No. 16586, ETH Zurich, Zurich.]Search in Google Scholar
[Patton, R.J. and Chen, J. (1997). Observer-based fault detection and isolation: Robustness and applications, Control Engineering Practice 5(5): 671-682.10.1016/S0967-0661(97)00049-X]Search in Google Scholar
[Patton, R.J., Uppal, F.J., Simani, S. and Polle, B. (2008).]Search in Google Scholar
[Reliable fault diagnosis scheme for a spacecraft control system, Journal of Risk and Reliability 222(2): 139-152, DOI: 10.1243/1748006XJRR98.10.1243/1748006XJRR98]Search in Google Scholar
[Rodrigues, M., Theilliol, D., Aberkane, S. and Sauter, D. (2007). Fault tolerant control design for polytopic LPV systems, International Journal of Applied Mathematics and Computer Science 17(1): 27-37, DOI:10.2478/v10006-007-0004-5.10.2478/v10006-007-0004-5]Search in Google Scholar
[Simani, S., Fantuzzi, C. and Patton, R. (2003). Model- Based Fault Diagnosis in Dynamic Systems Using Identification Techniques, Advances in Industrial Control, Springer-Verlag, London.10.1007/978-1-4471-3829-7]Search in Google Scholar
[Tanaka, N., Suzuki, S., Masui, K. and Tomita, H. (2006).]Search in Google Scholar
[Restructurable guidance and control for aircraft with failures considering gusts effects, AIAA Journal of Guidance, Control, and Dynamics 29(3): 635-642.]Search in Google Scholar
[Theilliol, D., Join, C. and Zhang, Y. (2008). Actuator fault tolerant control design based on a reconfigurable reference input, International Journal of Applied Mathematics and Computer Science 18(4): 553-560, DOI:10.2478/v10006008-0048-1.]Search in Google Scholar
[Zhang, Y. and Jiang, J. (2000). Integrated design of reconfigurable fault-tolerant control systems, AIAA Journal of Guidance, Control, and Dynamics 24(1): 133-136. 10.2514/2.4687]Search in Google Scholar