Active vortex flow control for vista f-16 envelope expansion

Guidance, Navigation, and Control Conference, 1994

Volumn , Issue , 1994, Pages 1259-1269

  Adams, Richard J ^a   Buffington, James M ^a   Banda, Siva S ^a  

^a AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; CONTROL THEORY; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLOW CONTROL; SUPERSONIC AIRCRAFT; VORTEX FLOW;

ANGLES OF ATTACK; CONTROL SYSTEM PERFORMANCE; LIMIT-CYCLE; NONLINEAR CONTROL LAWS; PERFORMANCE ANALYSIS; ROBUST STABILITY; VORTEX SYSTEMS;

VARIABLE STRUCTURE CONTROL;

EID: 84999266438     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1994-3681     Document Type: Conference Paper

References (10)

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8. Kramer, F.S., and K.H. Well (1987). “A Study on a Guidance and Control System Design for an Intelligent Munition,” Proceedings AIAA Guidance, Navigation and Control Conference, pp. 819-827.
9. Malcolm, G. N. (1991). “Forebody Vortex Control,” Progress in Aerospace Sciences, Vol. 28, No. 3, pp. 171-234.
10. Truxal, J.G. (1955). Automatic Feedback Control System Synthesis, McGraw-Hill, New York.