Identification update of aerodynamic models with sensor consistency checks

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2004, Pages 901-913

  Crassidis, Agamemnon L ^a,b  

^a ROCHESTER INSTITUTE OF TECHNOLOGY   (United States)

^b Department of Mechanical Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; IDENTIFICATION (CONTROL SYSTEMS); KALMAN FILTERING; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION; SENSORS;

AERODYNAMIC COEFFICIENT; AERODYNAMIC MODELS; DEFLECTION CONTROL; SENSOR CONSISTENCY CHECKS;

AERODYNAMICS;

EID: 19644391553     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5062     Document Type: Conference Paper

References (13)

1. Klein, V., and Schiess, J. R., "Compatibility Check of Measured Aircraft Responses Using Kinematic Equations and Extended Kalman Filter," NASA-TN-D-8514, Langley Research Center, Hampton, Virginia, 1977.
2. Klein, V., and Morgan, D. R., "Estimation of Bias Errors in Measured Airplane Responses Using Maximum Likelihood Method," NASA TM-89059, Langley Research Center, Hampton, Virginia, 1987.
3. Morelli, E. A., "Optimal Input Design for Aircraft Instrumentation Systemic Error Estimation," AIAA Atmospheric Flight Mechanics Conference Proceedings, AIAA paper 91-2850, New Orleans, Louisiana, August 1991, pp. 60-70.
4. Garza, F. R., and Morelli, E. A, "A Collection Non-Linear Aircraft Simulations in MATLAB," NASA-2003-212145, Langley Research Center, Hampton, Virginia, 2003.
5. Morelli, E. A., "Global Nonlinear Parametric Modeling Using Multivariate Orthogonal Functions," AIAA Journal of Aircraft. Vol. 32, No. 2, March-April 1998, pp. 270-277.
6. Morelli, E. A., "Global Nonlinear Parametric Modeling with Application to F-16 Aerodynamics," American Control Conference, Philadelphia, PA, June 24-28, 1998.
7. Lin, G., and Lan C. E., and Brandon, J. M., "A Generalized Dynamic Aerodynamic Coefficient Model for Flight Dynamics Applications," AIAA Paper 97-3643, 1997.
8. Trankle, T. L., and Bachner, S. D., "Identification of a Nonlinear Aerodynamic Model of the F-14 Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 6, November-December 1995, pp. 1292-1297.
9. Klein, V., and Murphy, P. C., "Aerodynamic Parameters of High Performance Aircraft Estimated From Wind Tunnel and Flight Test Data," AGARD Symposium on System Identification for Integrated Aircraft Development and Flight Testing, Madrid, Spain, May 5-8, 1998.
10. Klein, V., and Murphy, P. C., "Estimation of Aircraft Nonlinear Unsteady Parameters From Wind Tunnel Data," NASA/TM-1998-208969, Langley Research Center, Hampton, Virginia, 1998.
11. Gainer, G. G., and Hoffman, S., "Summary of Transformation Equations and Equations of Motion Used in Free-Flight and Wind-Tunnel Data Reduction and Analysis," NASA SP-3070, Langley Research Center, Hampton, Virginia, 1972.
12. Kalviste, J., "Flight Dynamics Reference Handbook," Aircraft Division Northrop Corporation E07488, April 1988.
13. Crassidis, J. L., and Junkins, J. L., Optimal Estimation of Dynamic Systems, Chapman & Hall/CRC, Boca Raton, Florida, 2004, pp. 48-50.