Non-linear aerodynamic modelling of unmanned cropped delta configuration from experimental data
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[1] Russell M. Cummings,et al. Unsteady Aerodynamics Modeling for Aircraft Maneuvers: a New Approach Using Time-Dependent Surrogate Modeling , 2012 .
[2] R. Kumar,et al. Parameter estimation using unsteady downwash model from real flight data of Hansa-3 aircraft , 2011 .
[3] Ajoy Kanti Ghosh,et al. Longitudinal parameter estimation from real flight data of unmanned cropped delta flat plate configuration , 2016 .
[4] R. V. Jategaonkar,et al. Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter , 2010 .
[5] Ruxandra Mihaela Botez,et al. New Approach for the Identification and Validation of a Nonlinear F/A-18 Model by Use of Neural Networks , 2010, IEEE Transactions on Neural Networks.
[6] R. V. Jategaonkar,et al. Identification of Aircraft Stall Behavior from Flight Test Data , 1999 .
[7] Ruxandra Botez,et al. New helicopter model identification method based on flight test data , 2011 .
[8] D. Fischenberg,et al. Identification of an Unsteady Aerodynamic Stall Model from Flight Test Data. , 1995 .
[9] Mikhail Goman,et al. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .
[10] R. V. Jategaonkar,et al. Evolution of flight vehicle system identification , 1996 .
[11] Rakesh Kumar,et al. Modelling of Cascade Fin Aerodynamics Near Stall using Kirchhoff's Steady-state Stall Model , 2011 .
[12] R. V. Jategaonkar,et al. Flight Vehicle System Identification: A Time-Domain Methodology, Second Edition , 2015 .
[13] Ruxandra Botez,et al. Identification of a non-linear F/A-18 model by the use of fuzzy logic and neural network methods , 2011 .
[14] Ruxandra Botez,et al. Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data , 2011 .
[15] Robert C. Nelson,et al. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers , 2003 .
[16] Raman K. Mehra,et al. Maximum likelihood identification of aircraft stability and control derivatives , 1974 .
[17] J. Leishman,et al. State-space representation of unsteady airfoil behavior , 1990 .
[18] Rakesh Kumar,et al. Nonlinear Modeling of Cascade Fin Aerodynamics Using Kirchhoff's Steady-State Stall Model , 2012 .
[19] Ajoy Kanti Ghosh,et al. Aircraft parameter estimation using a new filtering technique based upon a neural network and Gauss-Newton method , 2009, The Aeronautical Journal (1968).
[20] Ajoy Kanti Ghosh,et al. Parameter Estimation of Unmanned Flight Vehicle Using Wind Tunnel Testing and Real Flight Data , 2017 .
[21] Ruxandra Botez,et al. Improving the UAS-S4 Éhecal airfoil high angles-of-attack performance characteristics using a morphing wing approach , 2016 .