Aerodynamic Modeling and System Identification from Flight Data
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[1] Aharon Isser,et al. A Model of the Unsteady Aerodynamics of a Hovering Helicopter Rotor That Includes Variations of the Wake Geometry , 1995 .
[2] R. V. Jategaonkar,et al. Identification of C-160 Simulator Data Base from Flight Data , 1994 .
[3] R. V. Jategaonkar,et al. ESTIMA – an integrated software tool for nonlinear parameter estimation , 2002 .
[4] Detlef Rohlf,et al. Global Model Approach for X-31 VECTOR System Identification , 2005 .
[5] D Vicroy Dan,et al. Characterizing the Hazard of a Wake Vortex Encounter , 1997 .
[6] V. Klein,et al. Compatibility check of measured aircraft responses using kinematic equations and extended Kalman filter , 1977 .
[7] R. Jategaonkar,et al. Bounded-Variable Gauss-Newton Algorithm for Aircraft Parameter Estimation , 2000 .
[8] Dirk Schawe,et al. Aerodynamic design assessment of Strato 2C and its potential for unmanned high altitude airborne platforms , 2002 .
[9] Vladislav Klein,et al. Estimation of aircraft aerodynamic parameters from flight data , 1989 .
[10] R. V. Jategaonkar,et al. Identification of Actuation System and Aerodynamic Effects of Direct-Lift-Control Flaps , 1993 .
[11] Dan D. Vicroy,et al. Model Validation of Wake-Vortex / Aircraft Encounters , 2000 .
[12] P. G. Hamel,et al. The Role of System Identification for Flight Vehicle Applications - Revisited , 1999 .
[13] R. V. Jategaonkar,et al. Identification of Speed Brake, Air-Drop, and Landing Gear Effects from Flight Data , 1997 .
[14] Graham C. Goodwin,et al. Aircraft Flight Data Compatibility Checking Using Maximum Likelihood and Extended Kalman Filter Estimation , 1985 .
[15] Peter G. Hamel,et al. Advances in rotorcraft system identification , 1997 .
[16] J. Leishman,et al. State-space representation of unsteady airfoil behavior , 1990 .
[17] Thomas L. Trankle,et al. Identification of a nonlinear aerodynamic model of the F-14 aircraft , 1995 .
[18] R. E. Maine,et al. AGARD Flight Test Techniques Series. Volume 3. Identification of Dynamic Systems - Applications to Aircraft. Part 1. The Output Error Approach , 1986 .
[19] D. Fischenberg,et al. Identification of STRATO 2C Aerodynamic Data Base. Part 1: Low Speed, 0 - 30000 ft. , 1995 .
[20] Mikhail Goman,et al. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .
[21] R. V. Jategaonkar,et al. Evaluation of Parameter Estimation Methods for Unstable Aircraft , 1994 .
[22] D. Fischenberg,et al. Identification of an Unsteady Aerodynamic Stall Model from Flight Test Data. , 1995 .
[23] R. V. Jategaonkar,et al. Identification of DO-328 Aerodynamic Database for a Level D Flight Simulator. , 1997 .
[24] R. V. Jategaonkar,et al. Evolution of flight vehicle system identification , 1996 .
[25] Wilhelm Gockel,et al. IDENTIFICATION OF DORNIER-328 REVERSIBLE FLIGHT CONTROL SYSTEMS , 1998 .
[26] D. Fischenberg,et al. S-WAKE. Results of Flight Test Data Analysis , 2002 .
[27] Roberto Celi,et al. Helicopter Flight Dynamic Simulation with Refined Aerodynamics and Flexible Blade Modeling , 2000 .
[28] A.M.H. Nieuwpoort,et al. Determination of the mathematical model for the new dutch government civil aviation flying school flight simulator , 1987 .
[29] Paul Ray,et al. Federal Aviation Administration flight simulation standards - A regulatory update , 1995 .
[30] David A. Peters,et al. Theoretical prediction of dynamic inflow derivatives , 1980 .
[31] R. V. Jategaonkar,et al. CALIBRATION OF FIVE-HOLE PROBE FOR FLOW ANGLES FROM DYNAMIC AND TOWER FLY-BY MANEUVERS , 2002 .
[32] L. Allen,et al. Evolution of flight simulation , 1993 .
[33] Kendall Neville,et al. Flight update of aerodynamic math model , 1993 .
[34] Bernard Gimonet,et al. A systematic approach to nonlinear rotorcraft model identification , 2002 .
[35] Detlef Rohlf,et al. X-31A System Identification Using Single-Surface Excitation at High Angles of Attack. , 1996 .