Loads model development and analysis for the F/A-18 Active Aeroelastic Wing airplane

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2005, Pages 1357-1370

  Allen, Michael J ^a,b   Lizotte, Andrew M ^a,c   Dibley, Ryan P ^a,b   Clarke, Robert ^a,b  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b Flight Controls and Dynamics Branch   (United States)

^c Aerostructures Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BENDING MOMENTS; CONTROL SYSTEMS; MANEUVERABILITY; TORQUE; WINGS;

F/A-18 ACTIVE AEROELASTIC WING AIRPLANE; LINEAR REGRESSION TECHNIQUE; ONBOARD EXCITATION SYSTEM; STICK-DEFLECTION ROLLS;

AIRCRAFT MODELS;

EID: 29344458810     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6313     Document Type: Conference Paper

References (11)

1. Pendleton, E., Bessette, D., Field, P., Miller, G., and Griffin, K., "The Active Aeroelastic Wing Flight Research Program Technical Program & Model Analytical Development," AIAA-98-1972, 1998.
2. Dibley, R., Allen, M. J., Clarke, R., Gera, J., and Hodgkinson, J., "Development and Testing of Control Laws for the Active Aeroelastic Wing Program," AIAA-2005-6134, to be presented at the AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, CA, August 15-18, 2005.
3. Olney, C. D., Hillebrandt, H., and Reichenbach, E. Y., "An Evaluation Technique for an F/A-18 Aircraft Loads Model Using F/A-18 Systems Research Aircraft Flight Data," NASA TM-2000-209028, 2000.
4. Lewis, G. E., "AFTI/F-111 Mission Adaptive Wing Maneuver Load Control," available from the NASA Center for AeroSpace Information (CASI), CASI document identification 19910074478.
5. Haas, D. J., Flitter, L., and Milano, J., "Helicopter Flight Data Feature Extraction or Component Load Monitoring," Journal of Aircraft, Vol. 33, No. 1, Jan.-Feb. 1996.
6. Haas, D. J., and Imber, R., "Identification of Helicopter Component Loads Using Multiple Regression," Journal of Aircraft, Vol. 31, No. 4, July-Aug. 1994.
7. Haas, D. J., Milano, J., and Flitter, L., "Prediction of Helicopter Component Loads Using Neural Networks," Journal of the American Helicopter Society, Vol. 40, No. 1, Jan. 1995.
8. Allen, M. J., and Dibley, R. P., "Modeling Aircraft Wing Loads from Flight Data Using Neural Networks," NASA/TM-2003-212032, 2003.
9. Lokos, W. A., Olney, C. D., Chen, T., Crawford, N. D., Stauf, R., and Reichenbach, E. Y., "Strain-Gage Loads Calibration Testing of the Active Aeroelastic Wing F/A-18 Airplane," AIAA 2002-2926, 2002.
10. Lokos, W. A., and Stauf, R., "Strain-Gage Loads Calibration Parametric Study," NASA TM-2004-212853, 2004.
11. nd ed., McGraw-Hill, Inc., New York, St. Louis, San Francisco, 1988.