[Boškovic, J.D., Bergstrom, S.E. and Mehra, R.K. (2005). Adaptive accommodation of failures in second-order flight control actuators with measurable rates, American Control Conference, Portland, OR, USA, pp. 1033-1038.]Search in Google Scholar
[Caglayan, A.K., Rahnamai, K. and Allen, S. (1988). Detection, identification and estimation of surface damage/actuator failure for high performance aircraft, American Control Conference, Atlanta, GA, USA, pp. 2206-2212.]Search in Google Scholar
[Eykeren, L.V., Chu, Q. and Mulder, J. (2012). Actuator fault detection by aerodynamic model identification, 8th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, Mexico City, Mexico, pp. 1353-1357.]Search in Google Scholar
[Gheorghe, A., Zolghadri, A., Cieslak, J., Goupil, P., Dayre, R. and Berre, H.L. (2013). Model-based approaches for fast and robust fault detection in an aircraft control surface servo loop, Control Systems Magazine 33(3): 20-30.]Search in Google Scholar
[Goupil, P. (2010). Oscillatory failure case detection in the A380 electrical flight control system by analytical redundancy, Control Engineering Practice 18(9): 1110-1119.10.1016/j.conengprac.2009.04.003]Search in Google Scholar
[Goupil, P., Boada-Bauxell, J., Marcos, A., Cortet, E., Kerr, M. and Costa, H. (2014). AIRBUS efforts towards advanced real-time fault diagnosis and fault tolerant control, 19th IFAC World Congress, Cape Town, South Africa, pp. 3471-3476.]Search in Google Scholar
[Marton, L. and Ossmann, D. (2012). Energetic approach for control surface disconnection fault detection in hydraulic aircraft actuators, 8th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, Mexico City, Mexico, pp. 1149-1154.]Search in Google Scholar
[Narendra, K.S. and Balakrishnan, J. (1997). Adaptive control using multiple models, IEEE Transactions on Automatic Control 42(2): 171-187.10.1109/9.554398]Search in Google Scholar
[Ossmann, D. (2014a). Fault Detection, Isolation and Identification in Electro-hydraulic Actuators of Modern Aircaft, Ph.D. thesis, Technical University of Munich, Munich.]Search in Google Scholar
[Ossmann, D. (2014b). Optimization based tuning of fault detection and diagnosis systems for safety critical systems, 19th IFAC World Congress, Cape Town, South Africa, pp. 8570-8575.10.3182/20140824-6-ZA-1003.00159]Search in Google Scholar
[Ossmann, D. and Varga, A. (2013). Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics, Torus Press, Moscow, pp. 263-281.]Search in Google Scholar
[Varga, A. (2009). Least order fault and model detection using multi-models, Conference on Decision and Control, Shanghai, China, pp. 1015-1019.]Search in Google Scholar
[Varga, A., Hecker, S. and Ossmann, D. (2011). Diagnosis of actuator faults using LPV-gain scheduling techniques, AIAA Guidance, Navigation, and Control Conference, Portland, OR, USA.10.2514/6.2011-6680]Search in Google Scholar
[Varga, A. and Ossmann, D. (2014). LPV-techniques based robust diagnosis of flight actuator faults, Control Engineering Practice 31: 135-147.10.1016/j.conengprac.2013.11.004]Search in Google Scholar
[Varga, A., Ossmann, D., Goupil, P. and Sabot, G. (2013). Verification and validation of a FDD system for identification of flight actuator jamming, 19th IFAC Symposium on Automatic Control in Aerospace, Wuerzburg, Germany, pp. 84-89.]Search in Google Scholar