Fault tolerant flight control system: QFT design

International Journal of Robust and Nonlinear Control

Volumn 7, Issue 6, 1997, Pages 551-559

  Keating, M S ^a   Pachter, M ^a   Houpis, C H ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Fault tolerant control system; Quantitative feedback theory; Robust control theory with parametric uncertainty

Indexed keywords

CONTROL SYSTEM ANALYSIS; FEEDBACK CONTROL; FLIGHT DYNAMICS; ROBUSTNESS (CONTROL SYSTEMS);

FAULT TOLERANT FLIGHT CONTROL SYSTEM; PARAMETRIC UNCERTAINTY; QUANTITATIVE FEEDBACK THEORY;

CONTROL SYSTEM SYNTHESIS;

EID: 0031161965     PISSN: 10498923     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1099-1239(199706)7:6<551::AID-RNC290>3.0.CO;2-Z     Document Type: Article

References (6)

1. D' Azzo, J. J. and C. H. Houpis, Linear Control System Analysis and Design, Fourth edition, McGraw-Hill, NY, 1995.
2. Keating, M. S., 'Design of a flight control system for an unmanned research vehicle with control surface failures using quantitative feedback theory', MS Thesis, Air Force Institute of Technology, OH, 1993.
3. Horowitz, I., 'Quantitative feedback theory', Proceedings of the IEEE, 129D (6), 215-226 (1982).
4. Houpis, C. H., 'Quantitative feedback theory (QFT) - technique for designing multivariable control systems', Technical Report AFWAL-TR-86-3107, Flight Dynamics Laboratory AFWAL/FIGL, Wright-Patterson AFB, OH 45433-6553, 1987.
5. 'MIMO/QFT CAD Program', Version 2, Air Force Institute of Technology, Department of Electrical and Computer Engineering, Wright-Patterson AFB, OH 45433-6553, 1993.
6. Houpis, C. H. and G. B. Lamont, Digital Control Systems, Second edition, McGraw-Hill, NY, 1992.