By Dr Sreenatha Gopalarao Anavatti

Journal articles

Kallapur AG; Petersen IR; Sreenatha AG, 2012, 'Robust Gyro-free Attitude Estimation for a Small Fixed-wing Unmanned Aerial Vehicle', Asian Journal of Control, 14, pp. 1484 - 1495, http://dx.doi.org/10.1002/asjc.507

Li C; Anavatti SG; Ray T, 2011, 'Short-term traffic flow prediction using different techniques', IECON Proceedings (Industrial Electronics Conference), pp. 2423 - 2428, http://dx.doi.org/10.1109/IECON.2011.6119689

Hassanein OI; Anavatti SG; Ray T, 2011, 'Robust position control for two-link manipulator', International Journal of Artificial Intelligence, 7, pp. 347 - 359

Salman S; Sreenatha AG; Asokan T, 2011, 'Adaptive fuzzy control of unmanned underwater vehicles', Indian Journal of Marine Sciences, 40, pp. 168 - 175

Trilaksono BR; Triadhitama R; Adiprawita W; Wibowo A; Sreenatha AG, 2011, 'Hardware-in-the-loop simulation for visual target tracking of octorotor UAV', Aircraft Engineering and Aerospace Technology, 83, pp. 407 - 419, http://dx.doi.org/10.1108/00022661111173289

Garratt MA; Sreenatha AG, 2011, 'Non-linear Control of Heave for an Unmanned Helicopter Using A Neural Network', Journal of Intelligent and Robotic Systems, pp. 1 - 10, http://dx.doi.org/10.1007/s10846-011-9634-9

Hassan O; Sreenatha AG; Ray T, 2011, 'Robust Position Control for Two-Link Manipulator', International Journal of Artificial Intelligence, 7, pp. 347 - 359, http://ceser.in/ceserp/index.php/ijai/index

Samal MK; Sreenatha AG; Ray T; Garratt MA, 2010, 'A Computationally Efficient Approach for NN Based System Identification of a Rotary Wing UAV', International Journal of Control Automation and Systems, 8, pp. 727 - 734, http://www.springerlink.com/content/t4v7193l46333851/fulltext.pdf

Sreenatha AG, 2010, 'Flight Implementation of Dual Network Control Technique for Low-Cost UAV', International Journal of Aerospace Innovations, 2, pp. 81 - 92, http://multi-science.metapress.com/content/y286758l62444768/fulltext.pdf

Kallapur AG; Petersen IR; Sreenatha AG, 2009, 'A discrete-time robust extended Kalman filter for uncertain systems with sum quadratic constraints', IEEE Transactions on Automatic Control, 54, pp. 850 - 854, http://dx.doi.org/10.1109/TAC.2008.2010962

Salman SA; Anavatti SG; Choi JY, 2008, 'Indirect Adaptive Fuzzy Control of Unmanned Aerial Vehicle', IFAC Proceedings Volumes, 41, pp. 13229 - 13234, http://dx.doi.org/10.3182/20080706-5-kr-1001.02241

Samal MK; Anavatti S; Garratt M, 2008, 'Neural Network Based System Identification for Autonomous Flight of an Eagle Helicopter', IFAC Proceedings Volumes, 41, pp. 7421 - 7426, http://dx.doi.org/10.3182/20080706-5-kr-1001.01254

Puttige VR; Sreenatha AG, 2008, 'Real-time system identification of unmanned aerial vehicles: A multi-network approach', Journal of Computers (JCP), 3, pp. 31 - 38

Puttige VR; Sreenatha AG, 2008, 'Real-time system identification techniques based on neural networks for a low-cost UAV', Journal of Engineering Computing and Architecture, 2

Kallapur AG; Salman SA; Sreenatha AG, 2007, 'Application of extended Kalman filter towards UAV identification', Autonomous Robots and Agents, 76/2007, pp. 199 - 207

Salman SA; Puttige VR; Anavatti SG, 2006, 'Real-time validation and comparison of fuzzy identification and state-space identification for a UAV platform', Proceedings of the IEEE International Conference on Control Applications, pp. 2138 - 2143, http://dx.doi.org/10.1109/CACSD-CCA-ISIC.2006.4776971

Salman SA; Sreenatha AG; Choi JY, 2006, 'Attitude dynamics identification of unmanned aircraft vehicle', International Journal of Control Automation and Systems, 4, pp. 782 - 787

Sreenatha AG; Choi JH; Chwa D, 2006, 'Observer-based adaptive guidance law considering target uncertainties and control loop dynamics', IEEE Transactions on Control Systems Technology, 14, pp. 112 - 123

Sreenatha AG; Choi JY, 2004, 'Design and Implementation of Fuzzy Logic Controller for Wing Rock', International Journal of Control Automation and Systems, 2, pp. 494 - 500

Sreenatha AG; Wong P, 2004, 'Suppression of wing rock using artifical neural networks and fuzzylogic controller', Journal of Aircraft, 41, pp. 1247 - 1252

Sreenatha AG; Pradhan M, 2002, 'Fuzzy Logic Controller for Position Control of Flexible Structures', ACTA Astronautica, 50, pp. 665 - 671

Sreenatha AG; Ong TK, 2002, 'Wing Rock Suppression using Recessed Angle Spanwise Blowing', Journal of Aircraft, 39, pp. 900 - 903

Sreenatha AG; Nair NK; Sudhakar K, 2000, 'Aerodynamic suppression of wing rock using fuzzy logic control', Journal of Aircraft, pp. 345 - 348

Sreenatha AG; Nayak SK, 2000, 'Analysis of the steady state effects of the control surface nonlinearities on the performance of a fighter aircraft', Journal of Vibration and Control, pp. 923 - 935

Sreenatha AG; Patki MV; Joshi SV, 2000, 'Fuzzy logic control for wing-rock phenomenon', Mechanics Research Communications, pp. 359 - 364

Rajasekhar V; Sreenatha AG, 2000, 'Fuzzy logic implementation of proportional navigation guidance', ACTA Astronautica, pp. 17 - 24

Sreenatha AG; Rajhans V; Bhardwaj N, 1999, 'Robust controller design for a skid to turn missile', Acta Astronautica, 45, pp. 85 - 92, http://dx.doi.org/10.1016/S0094-5765(99)00107-1

Anavatti SG, 1998, 'Suppression of wing rock of slender delta wings using a single neural controller', IEEE Transactions on Control Systems Technology, http://ieeexplore.ieee.org/document/709502/

Seetharama Bhat M; Sreenatha AG; Shrivastava SK, 1991, 'Robust low order dynamic controller for flexible spacecraft', IEE Proceedings D: Control Theory and Applications, 138, pp. 460 - 468, http://dx.doi.org/10.1049/ip-d.1991.0063

Sreenatha AG; Bhat MS; Shrivastava SK, 1990, 'An optimal dynamic output feedback controller for a flexible spacecraft', Optimal Control Applications and Methods, 11, pp. 51 - 66, http://dx.doi.org/10.1002/oca.4660110105

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