Integrated approach to flight dynamics and aeroservoelasticity of whole flexible aircraft - part I: System modeling

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Meirovitcht, Leonard ^a   Tuzcu, Ilhan ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSERVOELASTICITY; AIRCRAFT; AIRCRAFT CONTROL; ELASTIC DEFORMATION; FLEXIBLE WINGS; FLIGHT DYNAMICS; FUSELAGES; GRAVITATION; ORDINARY DIFFERENTIAL EQUATIONS; RIGID STRUCTURES; RIGID WINGS; ROTATION; STRUCTURAL DYNAMICS;

ELASTIC DISPLACEMENTS; FIRST ORDER PROBLEMS; FLEXIBLE COMPONENTS; FUNDAMENTAL PRINCIPLES; MATHEMATICAL FORMULATION; PERTURBATION APPROACH; SPATIAL DISCRETIZATIONS; UNIFIED FORMULATIONS;

EMPENNAGES;

EID: 85088755130     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4747     Document Type: Conference Paper

References (24)

1. Collar, A. R., "The Expanding Domain of Aeroe-lasticity," Journal of the Royal Aeronautical Society, Vol. 50, 1946, p. 428.
2. J. B. Rea Co., "Aeroelasticity in Stability and Control," Wright Air Development Center, Technical Report 55-173,1957.
3. Taylor, A. S., "The Present Status of Aircraft Stability Problems in the Aeroelastic Domain," Journal of the Royal Aeronautical Society, Vol. 63, 1959, p. 580.
4. Bisphinghoff, R. L. and Ashley, H., Principles of Aeroelasticity (Ch. 9), John Wiley & Sons, Inc., New York, 1962. (Reprinted by Dover Publications, Inc., New York, 1975).
5. Milne, R. D., "Dynamics of the Deformable Aeroplane, Parts I and II," Her Majesty's Stationery Office, Reports and Memoranda No. 3345, London, 1962.
6. Taylor, A. S. and Woodcock, D. L., "Mathematical Approaches to the Dynamics of Deformable Aircraft, Parts I and II, "Her Majesty's Stationery Office, Reports and Memoranda No. 3776, London, 1971.
7. Dusto, A.R. et al., "A Method for Predicting the Stability Characteristics of an Elastic Airplane, Vol. 1-FLEXSTAB Theoretical Description," NASA CR-114712, October 1974.
8. Miller, G. D., Wykes, J.H. and Brosnan, M. J., "Rigid-Body Structural Mode Coupling on a Forward Swept Wing Aircraft," Journal of Aircraft, Vol. 20, No. 8, 1983, pp. 696-702.
9. Weisshaar, T. A. and Zeiler, T. A., "Dynamic Stability of Flexible Forward Swept Wing Aircraft," Journal of Aircraft, Vol. 20, No. 12, 1983, pp. 1014-1020.
10. Cerra, J. J.II, Calico, R. A. and Noll, T E., "Modelling of Rigid-Body and Elastic Aircraft Dynamics for Flight Control Development," Proceedings of the Atmospheric Flight Mechanics Conference, Williamsburg, VA, Aug. 18-20,1986, pp. 386-395.
11. Waszak, M. R. and Schmidt, D. K., "Flight Dynamics of Aeroelastic Vehicles," Journal of Aircraft, Vol. 25, No. 6, 1988, pp. 563-571.
12. Meirovitch, L., Methods of Analytical Dynamics, McGraw-Hill Book Co., New York, 1970.
13. Meirovitch, L. and Nelson, H. D., "On the High-Spin Motion of a Satellite Containing Elastic Parts," Journal of Spacecraft and Rockets, Vol. 3, No. 11, 1966, pp. 1597-1602.
14. Meirovitch, L., "Hybrid State Equations of Motion for Flexible bodies in Terms of Quasi-Coordinates," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 5, 1991, pp. 1008-1013.
15. Meirovitch, L., "Derivation of Equations for Flexible Multibody Systems in Terms of Quasi-Coordinates from the Extended Hamilton's Principle," Journal of Shock and Vibration, Vol. 1, Issue 2, 1993/94, pp. 107-119.
16. Meirovitch, L. and Stemple, T. J., "Hybrid Equations of Motion for Flexible Multibody Systems Using Quasi-Coordinates," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 4, 1995, pp. 678-688.
17. Meirovitch, L., "A Unified Theory for the Flight Dynamics and Aeroelasticity of Whole Aircraft," Proceedings of the Eleventh Symposium on Structural Dynamics and Control, Blacksburg, VA, May 12-14, 1997, pp. 461-468.
18. Nydick, I. and Friedmann, P. P., "Aeroelastic Analysis of a Trimmed Generic Hypersonic Vehicle," Proceedings of the CEAS/AIAA/ICASE/NASA International Forum on Aeroelasticity, and Structural Dynamics, Research Center, Hampton, VA, 1999, pp. 777-809.
19. Meirovitch, L. and Tuzcu, I., "Multidisciplinary Approach to the Modeling of Flexible Aircraft," International Forum on Aeroelasticity and Structural Dynamics," Madrid, Spain, June 5-7, 2001, pp. 435-448.
20. Etkin, B., Dynamics of Flight (2nd Ed.), John Wiley & Sons, New York, 1982.
21. Meirovitch, L., Principles and Techniques of Vibrations, Prentice-Hall, Inc., Upper Saddle River, NJ, 1997.
22. Dowell, E. H. (Editor), A Modern Course in Aeroe-lasticity (3rd Ed.), Kluwer Academic Publishers, Dordrecht/Boston/London, 1995.
23. Meirovitch, L. and Seitz, T. J., "Structural Modeling for Optimization of Low-Aspect-Ratio Wings," Journal of Aircraft, Vol. 32, No. 5, 1995, pp. 1114-1123.
24. Meirovitch, L. and Tuzcu, I., "Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft," NASA Technical Report (submitted December 20, 2001).