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Języki publikacji
Abstrakty
A multi-level reconfiguration framework is proposed for fault tolerant control of over-actuated aerial vehicles, where the levels indicate how much authority is given to the reconfiguration task. On the lowest, first level the fault is accommodated by modifying only the actuator/sensor configuration, so the fault remains hidden from the baseline controller. A dynamic reallocation scheme is applied on this level. The allocation mechanism exploits the actuator/sensor redundancy available on the aircraft. When the fault cannot be managed at the actuator/sensor level, the reconfiguration process has access to the baseline controller. Based on the LPV control framework, this is done by introducing fault-specific scheduling parameters. The baseline controller is designed to provide an acceptable performance level along all fault scenarios coded in these scheduling variables. The decision on which reconfiguration level has to be initiated in response to a fault is determined by a supervisor unit. The method is demonstrated on a full six-degrees-of-freedom nonlinear simulation model of the GTM UAV.
Rocznik
Tom
Strony
117--131
Opis fizyczny
Bibliogr. 28 poz., rys., wykr.
Twórcy
autor
- Institute for Systems and Control, Hungarian Academy of Sciences, Kende u. 13.–17., Budapest H-1111, Hungary
autor
- Institute for Systems and Control, Hungarian Academy of Sciences, Kende u. 13.–17., Budapest H-1111, Hungary
autor
- Institute for Systems and Control, Hungarian Academy of Sciences, Kende u. 13.–17., Budapest H-1111, Hungary
autor
- Institute for Systems and Control, Hungarian Academy of Sciences, Kende u. 13.–17., Budapest H-1111, Hungary
Bibliografia
- [1] Alwi, H., Edwards, C. and Tan, C. (2011). Fault Detection and Fault-Tolerant Control Using Sliding Modes, Springer-Verlag, London.
- [2] Blanchini, F. (1999). Set invariance in control, Automatica 35(11): 1747–1767.
- [3] Chakraborty, A., Seiler, P. and Balas, G.J. (2011). Nonlinear region of attraction analysis for flight control verification and validation, Control Engineering Practice 19(4): 335–345.
- [4] Cunningham, K., Foster, J.V., Murch, A.M. and Morelli, E. (2008). Practical application of a subscale transport aircraft for flight research in control upset and failure conditions, AIAA Guidance, Navigation, and Control Conference, Honolulu, HI, USA, pp. 1–14.
- [5] Dorobantu, A., Murch, A.M. and Balas, G.J. (2012). H∞ robust control design for the NASA AirSTAR flight test vehicle, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, USA, pp. 1–14.
- [6] Edwards, C., Alwi, H. and Tan, C.P. (2012). Sliding mode methods for fault detection and fault tolerant control with application to aerospace systems, International Journal of Applied Mathematics and Computer Science 22(1): 109–124, DOI: 10.2478/v10006-012-0008-7.
- [7] Ganguli, S., Marcos, A. and Balas, G. (2002). Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis, American Control Conference, Anchorage, AK, USA, Vol. 5, pp. 3612–3617.
- [8] Gaspar, P., Nemeth, B. and Bokor, J. (2012). Design of an LPV-based integrated control for driver assistance systems, Robust Control Design (7th ROCOND), Aalborg, Denmark, pp. 511–516.
- [9] Gaspar, P., Szabó, Z. and Bokor, J. (2012). LPV design of fault-tolerant control for road vehicles, International Journal of Applied Mathematics and Computer Science 22(1): 173–182, DOI: 10.2478/v10006-012-0013-x.
- [10] Gaspar, P., Szabo, Z. and Bokor, J. (2008). An integrated vehicle control with actuator reconfiguration, IFAC World Congress, Seoul, Korea, pp. 2087–2092.
- [11] Goupil, P. and Marcos, A. (2011). Advanced diagnosis for sustainable flight guidance and control: The European ADDSAFE project, SAE Technical Paper 2011-01-2804.
- [12] Goupil, P. and Marcos, A. (2012). Industrial benchmarking and evaluation of ADDSAFE FDD designs, Fault Detection, Supervision and Safety of Technical Processes (8th SAFEPROCESS), Mexico City, Mexico, pp. 1131–1136.
- [13] Johansen, T.A. and Fossen, T.I. (2013). Control allocation—a survey, Automatica 49(5):1087–1103.
- [14] Mahmoud, M., Jiang, J. and Zhang, Y. (2003). Active Fault Tolerant Control System, Springer-Verlag, Berlin/Heidelberg.
- [15] Montes de Oca, S., Puig, V., Witczak, M. and Dziekan, Ł. (2012). Fault-tolerant control strategy for actuator faults using LPV techniques: Application to a two degree of freedom helicopter, International Journal of Applied Mathematics and Computer Science 22(1): 161–171, DOI: 10.2478/v10006-012-0012-y.
- [16] Murch, A.M. (2008). A flight control system architecture for the NASA AirSTAR flight test infrastructure, AIAA Guidance, Navigation, and Control Conference, Honolulu, HI, USA, pp. 1–8.
- [17] Peni, T., Vanek, B., Szabo, Z. and Bokor, J. (2014). Dynamic sensor allocation framework for fault tolerant flight control, 19th IFAC World Congress, Cape Town, South Africa, pp. 3482–3487.
- [18] Peni, T., Vanek, B., Szabo, Z., Gaspar, P. and Bokor, J. (2013). Supervisory fault tolerant control of the GTM UAV using LPV methods, International Conference on Control and Fault-Tolerant Systems (SysTol), Nice, France, pp. 655–660.
- [19] Sloth, C., Esbensen, T. and Stoustrup, J. (2010). Active and passive fault-tolerant LPV control of wind turbines, American Control Conference (ACC), 2010, Baltimore, MD, USA, pp. 4640–4646.
- [20] Staroswiecki, M. (2006). Robust fault tolerant linear quadratic control based on admissible model matching, 45th IEEE Conference on Decision and Control, San Diego, CA, USA, pp. 3506–3511.
- [21] Steinberg, M. (2005). A historical overview of research in reconfigurable flight control, Aerospace Control and Guidance Systems Committee Meeting No. 95, Salt Lake City, UT, USA, Subcomitee E, pp. 1–38.
- [22] Stoustrup, J. (2009). Plug and play control: Control technology towards new challenges, European Journal of Control 15(3–4): 311–330.
- [23] Trachtler, A. (2004). Integrated vehicle dynamics control using active brake, steering and suspension systems, International Journal of Vehicle Design 36(1): 1–12.
- [24] Xiao, H., Chen, W., Zhou, H. and Zu, J. (2011). Integrated control of active suspension system and electronic stability programme using hierarchical control strategy: Theory and experiment, Vehicle System Dynamics 49(1–2): 381–397.
- [25] Yang, H., Jiang, B., Cocquempot, V. and Lu, L. (2012). Supervisory fault tolerant control with integrated fault detection and isolation: A switched system approach, International Journal of Applied Mathematics and Computer Science 22(1): 87–97, DOI: 10.2478/v10006-012-0006-9.
- [26] Yu, F., Li, D. and Crolla, D. (2008). Integrated vehicle dynamics control: State-of-the art review, IEEE Vehicle Power and Propulsion Conference, Harbin, China, pp. 1–6.
- [27] Zaccarian, L. (2009). Dynamic allocation for input redundant control systems, Automatica 45(6): 1431–1438.
- [28] Zhang, Y. and Jiang, J. (2008). Bibliographical review on reconfigurable fault-tolerant control systems, Annual Reviews in Control 32(2): 229–252.
Typ dokumentu
Bibliografia
Identyfikator YADDA
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