Modelling and control of an electro-hydrostatic actuator

International Journal of Robust and Nonlinear Control

Volumn 7, Issue 6, 1997, Pages 591-608

  Pachter, M ^a   Houpis, C H ^a   Kang, K ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Actuator compensator design; Quantitative feedback theory; Robust control theory with parametric uncertainty

Indexed keywords

CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; ROBUSTNESS (CONTROL SYSTEMS);

ELECTROHYDROSTATIC ACTUATOR; PARAMETRIC UNCERTAINTY; QUANTITATIVE FEEDBACK THEORY; ROBUST CONTROL THEORY;

ACTUATORS;

EID: 0031169735     PISSN: 10498923     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1099-1239(199706)7:6<591::AID-RNC293>3.0.CO;2-M     Document Type: Article

References (8)

1. de Silva, C. W., Control Sensors and Actuators, Prentice-Hall, Inc., Englewood Cliffs, NJ, 1989.
2. Houpis, C. H., et al., 'Quantitative feedback theory for the engineer', Wright Laboratory Technical Report, WL-TR-95-3061, Wright Laboratory, Wright-Patterson AFB, OH, 1995. Available from the National Technical Information Service, 5285 Port Royal Road, Springfield, VA 22151, U.S.A., document number AD-A297574.
3. D'Azzo, J. J. and C. H. Houpis, Linear Control System Analysis and Design - Conventional and Modern, Third edition, McGraw-Hill Inc., NY, 1988.
4. Pachter, M., 'Class notes: EENG 640 automatic flight control I', Air Force Institute of Technology, OH, 1993.
5. Blackelock, J. H., Automatic Control of Aircraft and Missiles, John Wiley & Sons, Inc., NY, 1991.
6. Kang, K. H., 'Electro-hydrostatic actuator controller design using quantitative feedback theory', MS Thesis AFIT/GE/ENG/94D-18, Graduate School of Engineering, Air Force Institute of Technology, Wright-Patterson AFB, OH, 1994.
7. Reynolds, O. R., 'Design of a subsonic envelope flight control system for the VISTA F-16 using quantitative feedback theory', MS Thesis, AFIT/GE/ENG/93D-34, Graduate School of Engineering, Air Force Institute of Technology, Wright-Patterson AFB, OH, 1993.
8. 'Interface control sheets, servo cylinder, stabilator/canard', GE Aerospace Technical Report, Johnson City, NY, 1987.