Extracting physical tuning potentiometers from a complex control law: Application to flexible aircraft flight control

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Alazard, Daniel ^a  

^a UNIVERSITÉ DE TOULOUSE   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CONTROLLERS; FLIGHT CONTROL SYSTEMS; POTENTIOMETERS (ELECTRIC MEASURING INSTRUMENTS); POTENTIOMETERS (RESISTORS); ROBUST CONTROL;

COMPLEX CONTROL; COMPLEX CONTROLLERS; CONTROL APPROACH; CONTROLLER ARCHITECTURES; FLEXIBLE AIRCRAFT; FLIGHT CONTROL LAW; SYNTHESIS MODELS; TUNING PARAMETER;

AIRCRAFT CONTROL;

EID: 85086493348     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4102     Document Type: Conference Paper

References (13)

1. Balas, G. and Doyle, J., "Control of lightly damped, flexible modes in the controller crossover region," Journal of Guidance, Control and Dynamics, Vol. 17, No. 2, 1994, pp. 370-377.
2. M. Tahk and Speyer, J., "Parameter robust Linear-Quadratic-Gaussian design synthesis with flexible structure control applications," AIAA-Journal of Guidance, Vol. 12, No. 3, 1989, pp. 460-468.
3. Alazard, M., Chretien, J., and Du, M.L., "Attitude control of a telescope with flexible modes," Dynamic and control of structures in space HI, Computational Mechanics Publications, London (UK), 15-19 June 1996, pp. 167-184.
4. ∞ filter approach," Journal of Guidance, Control and Dynamics, Vol. 19, No.5, 1996, pp. 1000-1006.
5. Joshi, S. and Kelkar, A. G., "Inner loop control of supersonic aircraft in the presence of aeroelastic modes," IEEE Transaction on Control Systems Technology, Vol. 6, No. 6, 1998, pp. 730-739.
6. Kubica, F. and Livet, T., "Flight control law synthesis for a flexible aircraft," Guidance, Navigation and Control Conference, AIAA, Scottsdale, August 1994.
7. Zhou, K., "A new controller architecture for high performance, robust and fault tolerant control," 39th Conference on Decision and Control, IEEE, Sydney, December 2000, pp. 4120-4125.
8. 2. "design for lateral flight control of a highly flexible aircraft," Submitted to Journal of Guidance, Control and Dynamics.
9. ∞ and μ controllers," 39th Conference on Decision and Control, IEEE, Sydney, December 2000, pp. 2787-2792.
10. Alazard, D. and Apkarian, P., "Exact oberserver-based structures for arbitrary compensators," Internationnal Journal of Robust and Non-Linear Control, Vol. 9, 1999, pp. 101-118.
11. Champetier, C. and Magni, J., "Analysis and synthesis of modal control laws," Rech. Aérospatiale, 1989, pp. 17-35.
12. Tischler, M. B., Advances in Aircraft Flight Control.
13. Alazard, M., Bucharles, A., Ferreres, G., Magni, J. F., and Prudhomme, S., "Towards a global methodology for flexible aircraft control," Structural aspect of flexible aircraft control, RTO-AVT, Ottawa (CANADA), 18-20 October 1999, pp. 25.1-25.10.