Parameter Estimation for Extending Flight Models into Post-Stall Regime - Invited
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[1] John V. Foster,et al. Simulation Study of Flap Effects on a Commercial Transport Airplane in Upset Conditions , 2005 .
[2] R. V. Jategaonkar,et al. Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter , 2010 .
[3] Harold L. Stalford. Application of the Estimation-Before-Modeling (EBM) System Identification Method to the High Angle of Attack/Sideslip Flight of the T-2C jet Trainer Aircraft. Volume 3. Identification of T-2C Aerodynamics Stability and Control Characteristics from Actual Flight Test Data , 1979 .
[4] Vladislav Klein,et al. Partitioning of flight data for aerodynamic modeling of aircraft at high angles of attack , 1989 .
[5] Eugene A. Morelli,et al. Generic Global Aerodynamic Model for Aircraft , 2015 .
[6] M. Psiaki. Backward-Smoothing Extended Kalman Filter , 2005 .
[7] Joris Field,et al. SUPRA - Enhanced upset recovery simulation , 2012 .
[8] W. J. Mccroskey,et al. The Phenomenon of Dynamic Stall. , 1981 .
[9] Ralph E. Bach,et al. Applications of state estimation in aircraft flight-data analysis , 1983 .
[10] A. Khrabrov,et al. Mathematical Modelling of Aircraft Unsteady Aerodynamics at High Incidence with Account of Wing-Tail Interaction , 2004 .
[11] Eugene A. Morelli,et al. Global Aerodynamic Modeling for Stall/Upset Recovery Training Using Efficient Piloted Flight Test Techniques , 2013 .
[12] J. A. Mulder,et al. NON-LINEAR AIRCRAFT FLIGHT PATH RECONSTRUCTION REVIEW AND NEW ADVANCES , 1999 .
[13] Ralph E. Bach. A Variational Technique for Smoothing Flight-Test and Accident Data , 1982 .
[14] Eugene A. Morelli,et al. Aircraft system identification : theory and practice , 2006 .
[15] Nobuhiro Yokoyama. Parameter Estimation of Aircraft Dynamics via Unscented Smoother with Expectation-Maximization Algorithm , 2011 .
[16] J. Singh,et al. Identification of Lateral-Directional Behavior in Stall from Flight Data. , 1996 .
[17] David R. Gingras,et al. Flight Simulator Augmentation for Stall and Upset Training , 2014 .
[18] Mikhail Goman,et al. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .
[19] Eugene A. Morelli,et al. A New Formulation of the Filter-Error Method for Aerodynamic Parameter Estimation in Turbulence , 2015 .
[20] John V. Foster,et al. Dynamics Modeling and Simulation of Large Transport Airplanes in Upset Conditions , 2005 .
[21] John V. Foster,et al. Upset Simulation and Training Initiatives for U.S. Navy Commercial Derived Aircraft , 2012 .
[22] Richard Newman,et al. Airplane Upsets: Old Problem, New I ssues * , 2008 .
[23] Alice Park,et al. Loss of Control on Approach Colgan Air, Inc., Operating as Continental Connection Flight 3407 Bombardier DHC-8-400, N200WQ Clarence Center, New York February 12, 2009 , 2010, SIGGRAPH '10.
[24] V. Klein,et al. Determination of airplane model structure from flight data using splines and stepwise regression , 1983 .
[25] John V. Foster,et al. Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics at Extreme Flight Conditions , 2002 .
[26] Patrick C. Murphy,et al. Determination of model structure and parameters of an airplane from pre- and post-stall flight data , 1981 .
[27] Jeffery A. Schroeder,et al. An Evaluation of Several Stall Models for Commercial Transport Training , 2014 .
[28] Hafid Smaili,et al. Pushing Ahead - SUPRA Airplane Model for Upset Recovery , 2012 .