Modeling and simulation of unsteady aerodynamic effects on a tailless aircraft

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 700-710

  Myatt, James H ^a   Schumacher, Corey J ^a   McKeeherv, Phillip D ^a   Buffington, James M ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT; ANGLE OF ATTACK; CRITICAL CURRENT DENSITY (SUPERCONDUCTIVITY); VORTEX FLOW;

ADAPTIVE NEURAL NETWORKS; AERODYNAMIC DERIVATIVES; AERODYNAMIC RESPONSE; CLOSED-LOOP CONTROL; CONTROLLED RESPONSE; LARGE TIME CONSTANT; MODEL AND SIMULATION; UNSTEADY AERODYNAMICS;

PLANFORMS;

EID: 84983203519     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4455     Document Type: Conference Paper

References (18)

1. Herbst, W. B., "Future Fighter Technologies," Journal of Aircraft, Vol. 17, No. 8, 1980, pp. 561-566.
2. Brandon, J. M., "Dynamic Stall Effects and Applications to High Performance Aircraft," Special Course on Aircraft Dynamics at High Angles of Attack: Experiments and Modelling, AGARD R-776, Hampton, VA, Mar. 1991.
3. Jenkins, J. E., "Nonlinear Aerodynamic Characteristics of a 65 Degree Delta Wing in Rolling Motion: Implications to Testing and Flight Mechanics Analysis (Invited)," AIAA Paper 97-0742, 1997.
4. Klein, V. and Noderer, K. D., "Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3-Parameters Estimated from Flight Data," NASA-TM-110259, May 1, 1996.
5. Thompson, S., Batill, S. and Nelson, R., "The Separated Flow Field on a Slender Delta Wing Undergoing Transient Motion," AIAA Paper 89-0194, 1989.
6. Ngo, A. N., Reigelsperger, W. C., Banda, S. S. and Bessolo, J. A., "Multivariable Control Law Design for a Tailless Aircraft," 1996 AIAA Guidance, Navigation and Control Conference, AIAA Paper 96-3866, July 1996.
7. Tobak, M., Chapman, G. T. and Ünal, A., "Modeling Aerodynamic Discontinuities and Onset of Chaos in Flight Dynamics Systems," Extrait Des Annales Des Telecommunications, Tome 42, n° 5-6, May-June 1987, pp. 300-314.
8. Tecplot Version 6 Users Manual, Amtec Engineering, Inc., Bellevue, WA, 1988-1993, pp. 23-34-23-36.
9. Press, W. H., Teukolsky, S. A., Vetterling, W. T. and Flannery, B. P., Numerical Recipes in Fortran: The Art of Scientific Computing, 2nd ed., Press Syndicate of the University of Cambridge, Cambridge, 1992, pp. 107-122.
10. Grismer, D. S., Myatt, J. H., McKeehen, P. D. and Buffington, J. M., "Application of a Nonlinear-lndicial-Response Model to a Tailless Aircraft Simulation," AIAA Paper 97-3644, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug. 1997.
11. McKeehen, P. D., Myatt, J. H., Grismer, D. S. and Buffington, J. M., "Simulation of a Tailless Aircraft Using Nonlinear Indicial Response Aerodynamic Modeling Methods," AIAA Paper 97-3790, Modeling and Simulation Technologies Conference, New Orleans, LA, Aug 1997.
12. Rockwell, D., "Three-Dimensional Flow Structure on Delta Wings at High Angle-of-Attack: Experimental Concepts and Issues," AIAA Paper 93-0550, Jan. 1993.
13. nd Shear Flow Conference, Tempe, AZ, Mar. 1989.
14. th Applied Aerodynamics Conference, New Orleans, LA, June 1996.
15. Albright, A. E., Dixon, C. J. and Hegedus, M. C., "Modification and Validation of Conceptual Design Aerodynamic Prediction Method HASC95 with VTXCHN," NASA Contractor Report 4712, Mar. 1996.
16. Myatt, J. H., "Modeling the Rolling 65-Degree Delta Wing with Critical State Encounters," AIAA Paper 97-3646, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug. 1997.
17. Leitner, J., Calise, A., Prasad, J. V. R., Analysis of Adaptive Neural Networks for Helicopter Flight Control, Journal of Guidance, Control, and Dynamics, vol. 20, no. 5, Sept. 1997, pp. 972-979.
18. Wong, J. P., et al., "Companion Guide to GENESIS Software Version 2. 2," Vol. I-User's Guide, Vol. 11-Programmer's Guide, Vol. III-Linearization Guide, Northrop Corporation B-2 Division, Sept. 1993.