Identification of a full subsonic envelope nonlinear aerodynamic model of the F-14 aircraft

Author:

TRANKLE THOMAS1,BACHNER STEPHEN2

Affiliation:

1. Lockheed Research Labs., Palo Alto, CA

2. U.S. Navy, Naval Air Warfare Center, Patuxent River, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. Barnhart, B. "Incremental Rotational Aerodynamic Model for the F-14 Airplane," Bihrle AppliedResearch Report 83-6, 1983. Barnhart,B."Incremental Rotational Aerodynamic Math Model for the F-14 Airplane," Bihrle Applied Research Report 86-4, 1986. Grafton, S.,Anglin, E. "Dynamic StabilityDerivatives at Angles of Attack from -5" to 90" for a Variable-Sweep Fighter Configuration with Twin Vertical Tails,"NASATND-6909,October 1972. Anon., F-14A Stability and Control and Flying Qualities Report, Status 111, Part 11: Aerodynamic Characteristics and Dimensional Data, GAC report numberA51-335-R-70-2. Vincent, J. H., Franklin, S. N., Rabin, U. H., Trankle, T. L. "Nonlinear System Identification Methodology Development Based on F-4s Flight Test Data Analysis,"Final ReporttoNaval AirTestCenterunder ContractNo. N00421-81-C-0289,Dec. 1983. Trankle,T.L.,Vincent,James H.,Franklin,S.Norman, "System Identification of Nonlinear Aerodynamic Models," AGARDograph No. 256, Advances in the Techniques and Technology of the Application of Nonlinear Filters and Kalman Filters,March, 1982. Batterson, James G., Klein, Vladislav, "Partitioningof Flight Data for Aerodynamic Modeling of Aircraft at High Angles of Attack," J. Aircraft. Vol. 26, No. 4, April 1989,pp.334-339. Trankle, T. L., Rabin, U. H. "Maximum Likelihood Tuning of a Vehicle Motion Filter," .I. of Guidance, Control, and Dynamics, Vol. 13, No. 5, Sept.Oct. 1990,pp. 842-849. Levenberg, K. "A Method for the Solution of Certain Nonlinear Problems in Least Squares," Quarterly Applied Mathematics,Vol. 2, 1944,pp. 164-168. Marquardt, D. W. "An Algorithm for Least Squares Estimation of Nonlinear Parameters," J. Soc. Indust. Appl. Math., Vol. 11,No. 2, 1963,pp.431-441. Brown, K., M., Dennis, J. E. "Derivative Free Analogues for the Levenberg-Marquardt and Gauss Algorithms for Nonlinear Least Squares Approximation," Nunzer.Math., Vol. 18,pp.289-297. Jategaonkar, Ravindra V., Plaetschke, Ermin, "Algorithms for Aircraft Parameter Estimation Accounting for Process and Measurement Noise," J. Aircraft,Vol.26,No. 4, April 1989,360-372. 14 Hall, W. Earl Jr., Gupta, N. K., Snith,R. G.

2. "Identification of Aircraft Stability and Control Coefficients for the High Angle-of-Attack Regime," Technical Report No. 2 to Office of Naval Research undercontract No. N00014-72-c-0328, March 1974. 15 Fumival,G. M., Wilson, Jr.R. W. "Regressions by

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