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Abhay Pashilkar
Abhay Pashilkar
National Aerospace Laboratories Bangalore India
Verified email at nal.res.in
Title
Cited by
Cited by
Year
A fault-tolerant neural aided controller for aircraft auto-landing
AA Pashilkar, N Sundararajan, P Saratchandran
Aerospace Science and Technology 10 (1), 49-61, 2006
1032006
Flutter control of a composite plate with piezoelectric multilayered actuators
S Raja, AA Pashilkar, R Sreedeep, JV Kamesh
Aerospace Science and Technology 10 (5), 435-441, 2006
742006
Estimating pilots’ cognitive load from ocular parameters through simulation and in-flight studies
MD Babu, DV JeevithaShree, G Prabhakar, KPS Saluja, A Pashilkar, ...
Journal of Eye Movement Research 12 (3), 2019
602019
Adaptive back-stepping neural controller for reconfigurable flight control systems
AA Pashilkar, N Sundararajan, P Saratchandran
IEEE Transactions on Control Systems Technology 14 (3), 553-561, 2006
572006
Evaluation of recursive least squares algorithm for parameter estimation in aircraft real time applications
C Kamali, AA Pashilkar, JR Raol
Aerospace science and technology 15 (3), 165-174, 2011
382011
Adaptive nonlinear neural controller for aircraft under actuator failures
AA Pashilkar, N Sundararajan, P Saratchandran
Journal of guidance, control, and dynamics 30 (3), 835-847, 2007
252007
Improved neural-aided sliding mode controller for autolanding under actuator failures and severe winds
S Ismail, AA Pashilkar, R Ayyagari, N Sundararajan
Aerospace Science and Technology 33 (1), 55-64, 2014
232014
Computation of flight mechanics parameters using continuation techniques
AA Pashilkar, S Pradeep
Journal of Guidance, Control, and Dynamics 24 (2), 324-329, 2001
212001
Design of a nonlinear dynamic inversion controller for trajectory following and maneuvering for fixed wing aircraft
AA Pashilkar, S Ismail, R Ayyagari, N Sundararajan
2013 IEEE symposium on computational intelligence for security and defense …, 2013
152013
Correlation between physiological and performance-based metrics to estimate pilots' cognitive workload
PA Hebbar, K Bhattacharya, G Prabhakar, AA Pashilkar, P Biswas
Frontiers in psychology 12, 555446, 2021
132021
Surface pressure model for simple delta wings at high angles of attack
AA Pashilkar
Sadhana 26, 495-515, 2001
132001
Design of nonlinear flight controller for fighter aircraft
P Lathasree, S Ismail, AA Pashilkar
IFAC Proceedings Volumes 47 (1), 711-718, 2014
102014
Aero-thermodynamic model for digital simulation of turbofan engine
R Yadav, Y Kapadi, A Pashilkar
Turbo expo: power for land, sea, and air 46997, 63-70, 2005
102005
Real-time Parameter Estimation for ReconfigurableControl of Unstable Aircraft
C Kamali, AA Pashilkar, JR Raol
Defence Science Journal 57 (4), 381, 2007
92007
Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds
S Ismail, AA Pashilkar, R Ayyagari, N Sundararajan
The Aeronautical Journal 118 (1207), 1009-1038, 2014
82014
Improved autolanding controller for aircraft encountering unknown actuator failures
S Ismail, AA Pashilkar, R Ayyagari, N Sundararajan
2013 IEEE Symposium on Computational Intelligence for Security and Defense …, 2013
82013
Neuro controller for aircraft auto landing under severe winds and control surface failures
A Pashilkar, N Sundararajan, P Saratchandran
43rd AIAA Aerospace Sciences Meeting and Exhibit, 914, 2005
82005
Thermodynamic Analysis of Turbofan Engine
R Yadav, CB Jugseniya, AA Pashilkar
Turbo Expo: Power for Land, Sea, and Air 46997, 55-62, 2005
82005
Guaranteed stability and improved performance against actuator failures using neural-aided sliding mode controller for autolanding task
S Ismail, AA Pashilkar, R Ayyagari
IFAC Proceedings Volumes 45 (1), 7-12, 2012
72012
Pilot performance evaluation of simulated flight approach and landing manoeuvres using quantitative assessment tools
PA Hebbar, AA Pashilkar
Sādhanā 42, 405-415, 2017
62017
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