Failure-tolerant control of aircraft; A fuzzy logic approach

Proceedings of the American Control Conference

Volumn 4, Issue , 1998, Pages 2281-2285

  Schram, G ^a   Copinga, G J C ^a   Bruijn, P M ^a   Verbruggen, H B ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATOR FAILURES; ADAPTIVE CONTROL SCHEMES; DIFFERENT STRUCTURE; FUZZY CONTROLLERS; FUZZY LOGIC APPROACH; MULTIPLE-MODEL ADAPTIVE CONTROLS; SIX DEGREES OF FREEDOM; SMOOTH TRANSITIONS;

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; FUZZY LOGIC; TRANSPORT AIRCRAFT;

AIRCRAFT CONTROL;

EID: 84881326439     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.1998.703035     Document Type: Conference Paper

References (18)

1. Athans M. (1977), The stochastic control of the F-8C aircraft using a multiple model adaptive control (MMAC) method - Part I: equilibrium flight. IEEE-AC, 22: 768-780.
2. Burken J.J., Burcham F.W. (1997), Flight-test results of propulsion-only emergency control system on MD-11 airplane. AIAA-GCD, 20(5): 980-987.
3. Copinga G.J.C. (1997). Master Thesis A 97.019 (765), Failure-Tolerant Control of Aircraft; an Adaptive-Fuzzy Approach, Delft University of Technology, Netherlands.
4. Frank P.M. (1996), Analytical and qualitative model-based fault diagnosis - A survey and some new results. European Journal of Control, 2: 6-28.
5. Isermann R. (1993), Fault diagnosis of machines via parameter estimation and knowledge processing - Tutorial paper. Automatica, 29(4): 815-835.
6. Lambrechts P., Bennani S., Looye G., Moormann D. (1997), The RCAM design challenge. In: Robust Flight Control, a Design Challenge, Magni R.F., Bennani S., Terlouw J. (Eds.), Springer Verlag Lecture Notes on Control and Information Sciences 224, pp. 149-179.
7. Maybeck P.S., Stevens R.D. (1991), Reconfigurable flight control via multiple model adaptive control methods. IEEE-AES, 27(3): 470-480.
8. Menke T.E., Maybeck P.S. (1995) System/actuator failure detection in the vista F-16 by multiple model adaptive estimation. IEEE-AES, 31(4):1218-1228.
9. Moerder D.D., Halyo N., Broussard J.R., Caglayan A.K. (1989), Application of precomputed control laws in a reconfigurable aircraft flight control system. AIAA-GCD, 12(3): 325-333.
10. Ostroff A.J. (1985), Techniques for accomodating control effector failures on a mildly statistically unstable airplane. ACC-85.
11. Patton R.J. (1997), Failure-tolerant control: The 1997 situation. SafeProcess-97, Hull, UK.
12. Schram G., Verbruggen H.B. (1997), RCAM: A fuzzy logic approach. In: Robust Flight Control, a Design Challenge, Magni R.F., Bennani S., Terlouw J. (Eds.), Springer Verlag Lecture Notes on Control and Information Sciences 224, pp. 397-416.
13. Schram G., Gopisetty S.M., Stengel R.F. (1998), A fuzzy logic - parity space approach for actuator failure detection and identification. AIAA 98-1014. AIAA Aerospace Sciences Meeting and Exhibit, San Reno, USA.
14. Schram G., Gopisetty S.M., Stengel R.F. (1998), Nonlinear rule-based failure detection and identification of control systems. ACC-98, Philadelphia, USA.
15. Schram G., Verschoor B., Sousa J.S., Verbruggen H.B. (1997), Using multiple fuzzy controllers for failure tolerant control. 6th FUZZ-IEEE, Barcelona, Spain.
16. Stengel R.F. (1991), Intelligent failure-tolerant control. IEEE-CS, 11(4): 14-23.
17. Shamma J.S., Athans M. (1990), Analysis of gain scheduled control for nonlinear plants. IEEE-AC, Vol. 35(8): 898-907.
18. Zadeh L.A. (1965), Fuzzy sets. Information and Control, 8(3): 338-353.