Incorporating flight data into a robust aeroelastic model

Journal of Aircraft

Volumn 35, Issue 3, 1998, Pages 470-477

  Lind, Rick ^a,b   Brenner, Marty ^a,b  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FIGHTER AIRCRAFT; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; MATHEMATICAL OPERATORS; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY;

ROBUST AEROELASTIC MODELS;

FLIGHT DYNAMICS;

EID: 0032075494     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2320     Document Type: Article

References (13)

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11. Vernon, L., "In-Flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing," NASA TM-4512, June 1993.
12. Brenner, M., Lind, R., and Voracek, D., "Overview of Recent Flight Flutter Testing Research at NASA Dryden," AIAA Paper 97-1023, April 1997.
13. Reed, W., III, "A New Flight Flutter Excitation System," Proceedings of the Society of Flight Test Engineers, 19th Annual Symposium (Arlington TX), 1988.