Robust and early detection of Oscillatory Failure Case for new generation Airbus aircraft

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Lavigne, L ^a,c   Zolghadri, A ^a,c   Goupil, P ^b   Simon, P ^a,c  

^a UNIVERSITÉ DE BORDEAUX   (France)

^b AIRBUS   (France)

^c UNIVERSITÉ BORDEAUX 1   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRBUS AIRCRAFT; ANALYTICAL REDUNDANCY; COLLABORATIVE PROJECTS; DETECTION PERFORMANCE; DYNAMICAL BEHAVIORS; EARLY DETECTION; FALSE ALARMS; FLIGHT CONTROL COMPUTER; FLIGHT TEST; HYDRAULIC ACTUATOR; MODEL QUALITIES; NEW STRATEGY; PHYSICAL PARAMETERS; RESEARCH ACTIVITIES;

ACTUATORS; AIRCRAFT CONTROL; AIRCRAFT DETECTION; FLIGHT CONTROL SYSTEMS; NAVIGATION; SIGNAL DETECTION;

AIRCRAFT;

EID: 78651070486     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (27)

1. Zolghadri A., Goetz C., Bergeon B. and Denoise X. Integrity monitoring of flight parameters using analytical redundancy. In UKACC International Conference on Control (CONTROL'98), pp. 1534-1539. Swansea, UK. 1998.
2. Chen J., Patton R. Robust model-based fault diagnosis for dynamic systems. Kluwer Academic Publisher. 1999.
3. Frank P., Ding S., Köppen-Seliger B. Current developments in the theory of FDI. Proceedings of SAFEPROCESS'2000, Budapest, pp. 16-27, IFAC. 2000.
4. Mangoubi, R.S. (1998). Robust estimation and failure detection: A concise treatment. Spronger Verlag.
5. Henry D., A. Zolghadri (2005). Design of Fault Diagnosis Filters: A Multi-Objective Approach. Journal of the Franklin Institute. Volume 342, Issue 4, July, Pages 421-446.
6. Henry D., A. Zolghadri (2005). Design and analysis of robust FDI filters for uncertain systems under feedback control. Automatica, Volume 41, Issue 2, February, Pages 251-264.
7. Frank P.M. Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy: A survey and some new results. In Automatica, volume 26, issue 3, pp. 459-474. 1990.
8. Zolghadri A. (2002). Early warning and prediction of flight parameter abnormalities for improved system safety assessment. Reliability Engineering and System Safety, vol. 16, pp 19-27.
9. Zolghadri A. (2000). A redundancy-based strategy for safety management in a modern civil aircraft. Control Engineering Practice, Vol. 8, No 5, pp 545-554.
10. Besch, H. M., H. G. Giesseler and J. Schuller (1996). Impact of Electronic Flight Control System (EFCS) Failure Cases on Structural Design Loads. AGARD Report 815, Loads and Requirements for Military Aircraft.
11. Goupil P. Oscillatory Failure Case detection in A380 Electrical Flight Control System by analytical redundancy. 17th IFAC Symposium on Automatic Control in Aerospace. Toulouse. France. 2007.
12. Frank, P.M. and Ding, S., X. (1997). Survey of robust residual generation and evaluation methods in observer-based fault detection systems. International journal of process control, 7(6), pp. 403-424.
13. Zolghadri A, F. Castang, D. Henry (2006). Design of robust fault detection filters for multivariable feedback systems. International journal of modelling and simulation. ACTA Press, Vol. 26, No 1
14. Ljung L. Söderstrôm T. Theory and practice of recursive identification. MIT PRESS, Cambridge, Mass. 1983
15. Reif, K., R. Unbehauen. The extended kalman filter as an exponential observer for nonlinear systems. IEEE Transactions on Signal Processing, 1999, 47(8), 2324-2328.
16. Nogaard M., Ravn, O., Poulsen, N. New developments in state estimation for nonlinear systems. Automatica 2000, 36, 1627-1638.
17. Zolghadri A., M. Monsion, D. Henry, C. Marcionini, O. Petrique. Development of an operational model-based warning system for tropospheric ozone concentrations in Bordeaux, France. Environmental Modelling and Software, 2004, 19, 369-382.
18. Kubica F, T. Livet, X. LeTron, and A. Bucharles, Parameter-robust flight control system for a flexible aircraft, Control Engineering Practice, Vol. 3, No. 9, pp.1209-1215 (1995).
19. Basseville, M., Distance measures for signal processing and pattern recognition. European Journal Signal Processing, vol.18, no 4, Dec. 1989, pp.349-369.
20. th IFIP World Computer Congress, Toulouse, France, pp.191-212.
21. Favre, C. (1994). Fly-by-wire for commercial aircraft: the Airbus experience. International Journal of Control, 59(1), 139-157.
22. CS 25, Certification Specifications for Large Aeroplanes, Amendment 1, published by European Aviation Safety Agency (EASA).
23. Lewis F.L. Optimal estimation. Wiley, New York. Ed. 1986.
24. Lin C.F. Modern Navigation, guidance, and control processing. Vol II. PTR Prentice Hall, New Jersey. 1991.
25. Brière B, C. Favre and P. Traverse (1995). A familly of fault-tolerant systems: electrical flight controls, from A320/330/340 to future military transport aircraft. Micoprocessors and Microsystems, Vol 19, No 2.
26. Pohjanpalo H. System identifiability based on the power series expansion of the solution. Math. Biosci. 41:21-33, 1978.
27. Anguelova M. Nonlinear Observability and Identifiability: General Theory and a Case Study of a Kinetic Model. Thesis for the degree of licentiate of engineering. Göteborg, april 2004.