PC-based simulation of the F-16/MATV

1997 Modeling and Simulation Technologies Conference

Volumn , Issue , 1997, Pages 481-489

  O’Rourke, Matthew J ^a   Ralston, John N ^a   Bell, Jeffery W ^a   Lash, Stanley F ^b  

^a Bihrle Applied Research Inc   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; COMPUTER CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); FIGHTER AIRCRAFT; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; MICROCOMPUTERS; PERSONAL COMPUTERS;

AERODYNAMIC DATA; FLIGHT STABILITY; HIGH ANGLE OF ATTACK; HIGH ANGLES OF ATTACK; NONLINEAR EFFECT; SIMULATION ENVIRONMENT; SIMULATION MODEL; SIX DEGREE-OF-FREEDOM;

SUPERSONIC AIRCRAFT;

EID: 84978224430     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. McKeehen, P., “ F-16/VISTA High-Angle-of- Attack Aerodynamic Modeling and Analysis,” WLTM- 91-304, February 1991.
2. Kay, J., Ralston, J., Lash S., “Development of a Non-Linear, Low-Speed Aerodynamic Database for theF-16/VISTA,” AIAA-97-3576, August 1997.
3. Baxter, J. et al,, “Flight Test Demonstration Report for the F-16 Multi-Axis Thrust Vectoring Program,” WL-TR-95-3086, January 1995.
4. Ralston, J., Kay J., “The Utilization of High Fidelity Simulation in the Support of High-Angle of Attack Flight Testing,” AIAA-96-3354, July 1996.