Multicriteria parametrical identification of the parafoil-load delivery system

Collection of Technical Papers - 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

Volumn , Issue , 2005, Pages 630-641

  Yakimenko, Oleg A ^a,b,c   Statnikov, Roman B ^a,d  

^a NAVAL POSTGRADUATE SCHOOL   (United States)

^b Code MAE/Yk ^*  (United States)

^c AIAA   (United States)

^d Information Sciences Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

IDENTIFICATION PARAMETERS; OPTIMIZATION PARAMETERS; PARAMETRICAL IDENTIFICATION;

AERODYNAMICS; CARGO AIRCRAFT; COMPUTER SOFTWARE; LOADS (FORCES); MATHEMATICAL MODELS; OPTIMIZATION; PROBLEM SOLVING;

IDENTIFICATION (CONTROL SYSTEMS);

EID: 29144536714     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (29)

1. th AIAA Aerodynamic Decelerator Systems Technology (ADST) Conference, Baltimore, MD, April 9-11, 1991.
2. Entchev, R.O., Rubenstein, D., Modeling Small Parafoil Dynamics, Final Report 16.622 Spring 2001.
3. th AIAA ADST Conference and Seminar, Monterey, CA, May 19-22, 2003.
4. Dobrokhodov, V.N., Yakimenko O.A, Junge, C.J., "Six-Degree-of- Freedom Model of a Controlled Circular Parachute"," AIAA Journal of Aircraft, 40(3), 2003, pp.482-493.
5. th AIAA Aerodynamic Decelerator Systems Technology Conference, Monterey, CA, 2003.
6. Graupe, D., Identification of Systems, Van Nostrand Reinhold, New York, 1972.
7. Ljung, L., System Identification: Theory for the User, Prentice Hall, Englewood Cliffs, 1987.
8. th AIAA ADST Conference, Clearwater Beach, FL, May 15-18, 1995.
9. th AIAA ADST Conference and Seminar, Boston, MA, May 21-24, 2001.
10. th AIAA ADST Conference and Seminar, Monterey, CA, May 19-22, 2003.
11. th AIAA ADST Conference and Seminar, Monterey, CA, May 19-22, 2003.
12. Rogers, R., "Aerodynamic Parameter Estimation for Controlled Parachutes," AIAA Paper 2002-4708, Proc. of the AIAA Atmospheric Flight Mechanics Conference, Monterey, CA, Aug. 5-8, 2002.
13. Hur, G., Valasek, J., "System Identification of Powered Parafoil-Vehicle from Flight Test Data," AIAA Paper 2003-5539, Proc. of the AIAA Atmospheric Flight Mechanics Conference, Austin, TX, Aug. 11-14, 2003.
14. Juang, J.-N., Applied System Identification, PTR Prentice Hall Englewood Cliffs, New Jersey, 1994.
15. Statnikov, R.B., Multicriteria Design. Optimization and identification, Kluwer Academic Publishers, Dordrecht/Boston/London, 1999.
16. Steuer, R.E., Multiple Criteria Optimization: Theory, computation and application, Wiley, New York, 1986.
17. White, D.J., A Bibliography on the Applications of Mathematical Programming Multiple-Objective Methods, Journal of the Operational Research Society, 8, 1990, pp.669-691.
18. Stadler, W., and Dauer, J.P., Multicriteria Optimization in Engineering: A Tutorial and Survey. Structural Optimization: Status and Promise, in AIAA Progress in Aeronautics and Astronautics, 150, 1992, pp.209-249.
19. Statnikov, R.B., and Matusov, J.B., Multicriteria Analysis in Engineering Using the PSI Method with MOVI 1.0, Kluwer Academic Publishers, Dordrecht/Boston/London, 2002.
20. Dunn, O.J., and Clark, V.A., Applied Statistics: Analysis of Variance and Regression, New York, Wiley, 1974.
21. τ Nets for the Approximation of the Edgeworth-Pareto Set in Multicriteria Optimization, Journal of Optimization: Theory and Applications, 91(3), 1996, pp.543-560.
22. Sobol', I.M., "On the Distribution of Points in a Cube and the Approximate Evaluation of Integrals," USSR Computational Mathematics and Mathematical Physics, 7(4), 1967, pp.784-802.
23. τ-Sequences," USSR Computational Mathematics and Mathematical Physics, 19(1), 1979, pp.252-256.
24. Bratley, P., and Fox, B.L., "Algorithm 659: Implementing Sobol's Quasirandom Sequence Generator," ACM Transactions on Mathematical Software, 14(1), 1988, pp.88-100.
25. Hailiang, M., and Zizeng, Q., "9-DoF Simulation of Controllable Parafoil System for Gliding and Stability," Journal of National University of Defense Technology, 16(2), 1994, pp.49-54.
26. th AIAA Aerodynamic Decelerator Systems Technology Conference, Munich, Germany, May 24-26, 2005.
27. Lee, C.K., Lanza, J., Buckley, J., "Apparatus and Method for Measuring Angular Positions of Parachute Canopies," Journal of Aircraft, 33(6), 1996, pp.1197-1199.
28. th CEAS/AIAA ADST Conference, Toulouse, France, June 8-11, 1999.
29. th AIAA ADST Conference and Seminar, Boston, MA, May 21-24, 2001.