Dynamic inversion to control large flexible transport aircraft

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 1224-1232

  Gregory, Irene M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN; FLIGHT ENVELOPES; TRANSPORT AIRCRAFT;

CONTROL DESIGN; DYNAMIC INVERSION; ELASTIC MODES; FLEXIBLE AIRCRAFT; FLIGHT CONTROL; FREQUENCY SEPARATION; HIGH PERFORMANCE AIRCRAFTS;

AIRCRAFT CONTROL;

EID: 29344463553     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Wykes, John, Byar, Thomas, MacMiller, Cary, and David Greek. Analyses and Tests of the B-l Aircraft Structural mode Control System. NASA CR 144887. 1980.
2. Newman, Brett, and Carey Buttrill. "Conventional Control for an Aeroelastic, Relaxed Static Stability high-Speed Transport" AIAA paper 95-3250-CP.
3. Bugajski, Daniel, Dale Enns, and Russ Hendrick. Multi-Application Control (MAOD: F-18 High Angle-of-Attack Research Vehicle (HARV) Reports. Honeywell Technology Center. November, 1994.
4. Application of Multivariable Control Theory to Aircraft Control Laws. Final Report: Multivariable Control Design Guidelines. WL-TR-96-3099. May 1996.
5. Enns, Dale, Dan Bujaski, Russ Hendrick, and Gunter Stein. "Dynamic Inversion: An Evolving Methodology for Flight Control Design. " Int. J. Control, 1994, Vol. 59, No. 1, 71-91.
6. Etkin, B. Dynamics of Aerodynamic Flight Wiley. 1956.
7. Tiffany, Sherwood, and William Adams. NASA TP-2776. Nonlinear Programming Extensions to Rational Function Approximation Methods for Unsteady Aerodynamic Forces. July 1988.