Stability result for dynamic inversion devised to control large flexible aircraft

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Gregory, Irene M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT ENVELOPES; SUPERSONIC AIRCRAFT;

CONTROL LAWS; DYNAMIC INVERSION; FLEXIBLE AIRCRAFT; FLIGHT CONTROL; GLOBAL STABILITY; HIGH PERFORMANCE AIRCRAFTS; HIGH SPEED CIVIL TRANSPORTS; STABILITY RESULTS;

AIRCRAFT CONTROL;

EID: 85088756998     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4284     Document Type: Conference Paper

References (9)

1. 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.
2. Gregory, Irene M. "Dynamic Inversion to Control Large Flexible Transport Aircraft." 1998 AIAA Guidance, Navigation, and Controls Conference, Boston, MA. AIAA paper 98-4323.
3. Gregory, Irene M. "Modified Dynamic Inversion to Control Large Flexible Aircraft-What's Going On?." 1999 AIAA Guidance, Navigation, and Controls Conference, Portland, OR. AIAA paper 99-3998.
4. Morton, B., D. Enns and B.Y. Zhang. "Stability of Dynamic Inversion Control Laws Applied to Nonlinear Aircraft Pitch-Axis Models." International Journal of Control, Volume 63, Issue: 1, pp. 1-25. Jan, 1996.
5. La Salle, J.P. The Stability of Dynamical Systems. Regional Conference Series in Applied Mathematics, vol. 25, 1976.
6. Gregory, Irene M. "Stability Results for Dynamic Inversion Applied to Aeroelastic Vehicles" Submitted to 2002 American Control Conference, Anchorage, AK.
7. Markus, L. "Asymptotically Autonomous Differential Systems." Contributions to the Theory of Nonlinear Oscillations, vol. III. S. Lefschetz ed., Princeton University Press, 1956, pp. 17-29.
8. Yoshizawa, T. Stability Theory and the Existence of Periodic Solutions and Almost Periodic Solutions. Springer-Verlag, 1975.
9. Christilf, D. Implemenattion of Dynamic Aeroelastic Degree-of Freedom in the HSR Ref.H Cycle 3 HSCT Concept. NASA CR. July, 1997.