Lateral directional parameter estimation of a miniature unmanned aerial vehicle using maximum likelihood and Neural Gauss Newton methods
暂无分享,去创建一个
[1] Abdallah Ben Mosbah,et al. A neural network controller new methodology for the ATR-42 morphing wing actuation , 2016 .
[2] Eugene A. Morelli,et al. Aircraft system identification : theory and practice , 2006 .
[3] Christina M. Ivler,et al. System Identification Modeling for Flight Control Design , 2008 .
[4] R. V. Jategaonkar,et al. Identification of Aircraft Stall Behavior from Flight Test Data , 1999 .
[5] Robert C. Nelson,et al. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers , 2003 .
[6] J. Leishman,et al. State-space representation of unsteady airfoil behavior , 1990 .
[7] William F. Milliken,et al. Progress in Dynamic Stability and Control Research , 1947 .
[8] Harry Greenberg. A survey of methods for determining stability parameters of an airplane from dynamic flight measurements , 1951 .
[9] Eugene A. Morelli,et al. Real-Time Aerodynamic Parameter Estimation without Air Flow Angle Measurements , 2012 .
[10] Ruxandra Botez,et al. New helicopter model identification method based on flight test data , 2011 .
[11] Colin R. Theodore,et al. Rapid Frequency-Domain Modeling Methods for Unmanned Aerial Vehicle Flight Control Applications , 2004 .
[12] Adam,et al. Control System Development and Flight Test Experience with the MQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) , 2007 .
[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] Marvin Shinbrot. A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data , 1951 .
[15] Thien-My Dao,et al. New methodology combining neural network and extended great deluge algorithms for the ATR-42 wing aerodynamics analysis , 2016, The Aeronautical Journal.
[16] Ajoy Kanti Ghosh,et al. Longitudinal parameter estimation from real flight data of unmanned cropped delta flat plate configuration , 2016 .
[17] D. Fischenberg,et al. Identification of an Unsteady Aerodynamic Stall Model from Flight Test Data. , 1995 .
[18] Mikhail Goman,et al. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .