Control law reconfiguration using robust linear parameter varying control

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 977-987

  Bennani, S ^a   van Der Sluis, R ^a   Schram, G ^a,b   Mulder, J A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b SKF ENGINEERING AND RESEARCH CENTRE   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL ENGINEERING;

CONTROL EFFECTIVENESS; FAILURE SCENARIOS; FAULT TOLERANT CONTROL; LINEAR PARAMETER VARYING CONTROL; NONLINEAR SIMULATIONS; PERFORMANCE OBJECTIVE; PERFORMANCE SPECIFICATIONS; SYSTEM UNCERTAINTIES;

AIRCRAFT CONTROL;

EID: 77953775531     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4137     Document Type: Conference Paper

References (16)

1. Athans M. (1977).“The Stochastic Control of the F-8G Aircraft using a Multiple Model Adaptive Control (MMAC) Method-Paxt LEquilibrium Flight”, IEEE-AC, Vol. 22, pp. 768-780.
2. Balas G. J., Doyle J. C., Glover K., Packard A., Smith R. (1993).“Analysis and Synthesis TOOLBOX, For Use with MATLAB”, Math-Works Inc., Natick, MA.
3. Bell T. E. (1989).“Managing Risk in Large Complex Systems”, IEEE Spectrum, Vol. 26, No. 6, pp. 24-27.
4. Bennani S., Willemsen D. M. C., Scherer C. W. (1998).“Robust Control of Linear Parametrically Varying Systems with Bounded Rates”, Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, pp. 916-922.
5. Bennani S., Looye G. (1997). A /i-Synthesis Approach (1). in J. F. Magni, S. Bennani, J. Ter-louw (eds), Robust Flight Control, A Design Challenge, Lecture Notes in Control and Information Sciences 224, Springer Verlag.
6. Biannic J. M., Apkarian P., Gaxraxd W. L. (1996). Parameter Varying Control of a High Performance Aircraft. Technical Report.
7. Brinker J. S., Wise K. A. (1998).“Reconfigur-able Flight Control for a Tailless Advanced Fighter Aircraft”, Proceedings of the AI A A Guidance, Navigation and Control Conference, Boston MA, August 1998, AIAA-98-4107.
8. Burken J. J., Burcham Jr. F. W. (1997).“Flight-Test Results of Propulsion-Only Emergency Control System on MD-11 Airplane”, Journal of Guidance, Control, and Dynamics, Vol. 20, No. 5, pp. 980-987.
9. Lambrechts P., Bennani S., Looye G., Moormann, D. (1997). The RCAM Design Challenge Problem Description, in J. F. Magni, S. Bennani, J. Terlouw (eds), Robust Flight Control, A Design Challenge, Lecture Notes in Control and Information Sciences 224, Springer Verlag.
10. Gahinet P., Nemirovski A., Laub A. J., Chilali M. (1995). LMI Toolbox. For Use with MATLAB. The Math Works, Inc.
11. Jonckheere E. A., Yu G-R. (1999).“Propulsion Control of Crippled Aircraft by H^ Model Matching”, IEEE Transactions on Control Systems Technology. To appear, 1999.
12. Schram G., Copinga G. J. C., Bruijn P. M., Verbruggen H. B. (1998).“Failure-Toler ant Control of Aircraft;a Fuzzy Logic Approach”, American Control Conference, pp. 2281-2285, Philadelphia, PA, USA.
13. Spillman M., Blue P., Banda S., Lee L. (1996).”A Robust Gain-scheduling Example Using Linear Parameter Varying Feedback”. IFAC 13i/l Triennial World Congress, San Francisco.
14. Stengel R. F. (1991).“Intelligent Failure-Tolerant Control”, IEEE Control Systems Mag., Vol. 11, No. 4, pp. 14-23.
15. Vorotnikov V. I. (1998). Partial Stability and Control. Birkhäuser Boston.
16. Wise K. A., Sedwick J. L. (1998).“Stability Analysis of Reconfigurable and Gain Scheduled Flight Control Systems Using LMIs”, Proceedings of the AIAA Guidance, Navigation and Control Conference, Boston MA, August 1998, AIAA-98-4111, pp. 118-126.