The cobra maneuver as a minimum time problem

22nd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1997, Pages 339-344

  Murayama, Kei ^a   Hull, David G ^a  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION;

FLIGHT PATH ANGLE; MINIMUM TIME; MINIMUM TIME PROBLEMS; RELATIVE DISTANCES; STALL SPEED; THREE DEGREE OF FREEDOMS;

SUPERSONIC AIRCRAFT;

EID: 84983099915     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Fink, D. E., et al., "Agile Sukhoi Su-27 Leads Strong Soviet Presentation, " Aviation Week and Space Technology, Vol. 130, No. 25, June 19, 1989, pp. 28-30.
2. Miele, A., Flight Mechanics, Vol. I, Theory of Flight Paths, Addison-Wesley, Massachusetts, 1962.
3. Nguyen, L. T., et al., "Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability, " NASA Tech. Paper 1538, NASA, Washington, D. C., Dec. 1979.
4. Stevens, B. L. and Lewis, F. L., Aircraft Control and Simulation, John Wiley and Sons, New York, 1992.
5. Hull, David G., "Conversion of Optimal Control Problems into Parameter Optimization Problems, " Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, January-February, 1997, pp. 57-60.