SACCON stability and control analysis applying system identification techniques

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Rohlf, Detlef ^a,d   Schmidt, Stefan ^b,e   Irving, Jonathan ^c  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

^c BAE SYSTEMS   (United Kingdom)

^d Transport Aircraft   (Germany)

^e Air Vehicles Division   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; CURVE FITTING; DAMPING; LEAST SQUARES APPROXIMATIONS; NONLINEAR EQUATIONS; STIFFNESS; VEHICLE PERFORMANCE; WIND TUNNELS;

DYNAMIC WIND TUNNEL TESTS; HIGH ANGLE OF ATTACK; LEAST SQUARE CURVE FITTING; NONLINEAR MODEL EQUATIONS; STABILITY AND CONTROL; STIFFNESS AND DAMPING; SYSTEM IDENTIFICATION TECHNIQUES; UNSTEADY SIMULATIONS;

ANGLE OF ATTACK;

EID: 78649521600     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4399     Document Type: Conference Paper

References (18)

1. Iliff, K. W., "Parameter Estimation for Flight Vehicles," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 5, 1989, pp. 609-622.
2. Hamel, P. G., and Jategaonkar, R. V., "Evolution of Flight Vehicle System Identification," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 9-28.
3. Wang, K. C., and Iliff, K. W., "Retrospective and Recent Examples of Aircraft Parameter Identification at NASA Dryden Flight Research Center," Journal of Aircraft, Vol. 41, No. 4, 2004, pp. 752-764.
4. Jategaonkar, R. V., Fischenberg, D., and von Gruenhagen, W., "Aerodynamic Modeling and System Identification from Flight Data - Recent Applications at DLR," Journal of Aircraft, Vol. 41, No. 4, 2004, pp. 681-691.
5. Morelli, E. A., and Klein, V., "Application of System Identification to Aircraft at NASA Langley Research Center," Journal of Aircraft, Vol. 42, No. 1, 2005, pp. 12-24.
6. Jategaonkar, R. V., "Flight Vehicle System Identification: A Time Domain Methodology", Vol. 216, AIAA Progress in Astronautics and Aeronautics Series, Published by AIAA Reston, VA, USA, ISBN 1-56347-836-6, August 2006.
7. Cummings, R. M. and Schuette, A., "An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT- 161", AIAA 28th Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun - 1 Jul 2010, Paper 4392.
8. Loeser, T., Vicroy, D. D. and Schuette, A., "SACCON Static Wind Tunnel Tests at DNW- NWB and 14'×22' NASA LaRC", AIAA 28th Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun - 1 Jul 2010, Paper 4393.
9. Vicroy, D. D. and Loeser,T., "SACCON Dynamic Wind Tunnel Tests at DNW- NWB and 14'x22' NASA LaRC", AIAA 28th Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun - 1 Jul 2010, Paper. 4394.
10. Bergmann, A., Huebner, A.-R., "Integrated Experimental and Numerical Research on the Aerodynamics of Unsteady Aircraft", 3rd International Symposium on Integrating CFD and Experiments in Aerodynamics, 2007-06-20 - 2007-06-21, ASAFA, Colorado.
11. Bergmann, A., Huebner, A.-R., Loeser, T., "Experimental and numerical research on the aerodynamics of unsteady moving aircraft", Progress in Aerospace Sciences, Volume 44, Issue 2, February 2008, Pages 121-137.
12. Owens, D. B., Brandon, J. M., Fremaux, C. M., Heim, E. H. and Vicroy, D. D., "Overview of Dynamic Test Techniques for Flight Dynamic Research at NASA LaRC", AIAA-2006-3146, 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, June 5-8, 2006.
13. Schuette, A., Cummings, R. M., Loeser, T. and Vicroy, D. D., "Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control", 4th Symposium on Integrating CFD and Experiments in Aerodynamics, von Karman Institute, Rhode-Saint-Genèse, Belgium, 14-16 September 2009.
14. Cobalt, "User's Manual-Cobalt version 4.0", www.cobaltcfd.com.
15. Newman, D. M., "Measurement of Water Tunnel Model Dynamic Derivatives using a Force Balance Capable of Rotational Oscillation", Quantitative Aeronautics Report 2005.003, V0.20, 2006.
16. Rodden, W.P., "Giesing, J.P.: Application of Oscillatory Aerodynamic theory to Estimation of dynamic Stability derivatives", AIAA J. Aircraft, Volume 7, No 3, May-June 1970, Pages 272-275.
17. Rodden, W.P., "Bellinger, E.D.; Giesing, J.P.: Errata and Addenda to Application of Oscillatory Aerodynamic theory to Estimation of dynamic Stability derivatives", AIAA J. Aircraft, Volume 21, No 1, January 1984.
18. Seher-Weiss, Susanne, "User's Guide: FITLAB Parameter Estimation Using MATLAB - Version 2.0", DLR Internal Report, DLR-IB 111-2007/27, 65 pages.