Items where Author is "Pashilkar, AA"

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Number of items: 55.

Conference or Workshop Item

Lathasree, P and Shaik , Ismil and Pashilkar, AA (2014) Design of Nonlinear Flight Controller for Fighter Aircraft. In: ACODS2014, 13 Mar 2014, IIT Kanpur.

Pashilkar, AA and Ismail, Shaik and Ayyagari, Ramakalyan and Sundararajan, N (2013) Design of a nonlinear dynamic inversion controller for trajectory following and maneuvering for fixed wing aircraft. In: IEEE Symposium Series on Computational Intelligence, 16 Apr 2013, Singapore.

Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan and Sundararajan, N (2013) Improved autolanding controller for aircraft encountering unknown actuator failures. In: IEEE Symposium Series on Computational Intelligence, 16 Apr 2013, Singapore.

Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan (2011) Adaptive control of micro air vehicles. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Goyal, Anup and Saraf, Amitabh and Pashilkar, AA and Patel, Ambalal V. (2011) Analysis of effect of wake vortices on air data sensors. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Lathasree, P and Pashilkar, AA (2011) Digital Simulation Model for Turboprop Engine. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Pashilkar, AA and Haijun, Rong and Sundararajan, N and Saratchandran, P (2011) Fault toleranat neuro/neuro-fuzzy controllers for aircraft auto landing with actuator failures and severe winds. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Pashilkar, AA (2009) Model Based Design of Aerospace Control Systems. In: International Symposium on Opportunities and Challenges Facing Aviation inustry in Indian Subcontinent, 18-20, 2009, Sreenidhi Institute of Science and Technology, Hyderabad.

Pashilkar, AA and Kamali, C and Raol, JR (2007) Direct estimation of nonlinear aerodynamic coefficients. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 20-23 Aug 2007, Soutli Carolina, USA.

Pashilkar, AA (2007) Development of Saras Autopilot. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.

Raja, D and Sreedeep, R and Pashilkar, AA and Kamesh, JV (2005) Active flutter suppression of a composite plate with PZT multilayered benders using LQG control. In: International Conference on Smart Materials Structures and Systems, 28-30 Jul 2005, Bangalore, India.

Yadav, R and Kapadi, Yogesh and Pashilkar, AA (2005) Aero-thermodynamic model for digital simulation of turbofan engine. In: ASME Turbo Expo 2005: Power for Land, Sea, and Air (GT2005) , June 6–9, 2005 , Reno, Nevada, USA.

Yadav, R and Jugseniya, Chandrakant B and Pashilkar, AA (2005) Thermodynamic analysis of turbofan engine. In: ASME Turbo Expo 2005: Power for Land, Sea, and Air (GT2005) , June 6–9, 2005, Reno, Nevada, USA .

Pashilkar, AA (2002) Flight dynamic analysis of the flow incidence rate model AIAA Paper 2002-0098. In: 40th AIAA Aerospace Sciences Meeting amp; Exhibit, 14-17 January 2002, Reno, NV.

Pashilkar, AA (2002) Global response surface model for unsteady surface pressures on delta wing aircraft AIAA Paper 2002-0711. In: 40th AIAA Aerospace Sciences Meeting amp; Exhibit, 14-17 January 2002, Reno, NV.

Pashilkar, AA (2001) Unsteady aerodynamic modeling at high incidence for flight dynamic analysis. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 6-9 Aug 2001, Canada, United States.

Pashilkar, AA (2001) Flow incidence rate model for unsteady aerodynamics at high angles of attack AIAA Paper 2001-2469. In: 19th Applied Aerodynamics Conference, 11-14 June 2001, Anaheim, CA.

Pashilkar, AA (2001) Surface pressure model for simple delta wings at high angles of attack AIAA Paper 2001-2415. In: 19th Applied Aerodynamics Conference, 11-14 June 2001, Anaheim, CA.

Pashilkar, AA (1999) Computation of flight mechanics parameters using continuation techniques. AIAA Paper 99-4318. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Aug. 9-11, 1999, Portland, OR.

Pashilkar, AA (1999) Unsteady aerodynamic modelling using multivariate orthogonal polynomials AIAA Paper 99-4014. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Aug. 9-11, 1999, Portland, OR.

Pashilkar, AA (1996) Algorithms for aircraft trim analysis on ground 13; AIAA-96-350513;. In: AIAA flight simulation technologies conference.

Journal Article

Srikanth, K P and Kamali, C and Pashilkar, AA (2014) Terrain Integrity Monitoring Studies using Kalman Filter for SVS. International Journal of Advanced Research in Electrical, Electronics and Instrumentation Engineering . pp. 534-539. ISSN 2278 - 8875

Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan and Sundararajan, N (2014) Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds. Aeronautical Journal, 118 (1207). pp. 1-28. ISSN 0001-9240

Lathasree, P and Pashilkar, AA (2014) Efficient numerical integration and table lookup techniques for real time flight simulation. International Journal of Computer Science and Business Informatics, 10 (1). pp. 8-24. ISSN 1694-2108

Ismail, Shaik and Pashilkar, AA and Ramakalyan, Ayyagari and Narasimhan, Sundararajan (2014) Improved neural-aided sliding mode controller for autolanding under actuator failures and severe winds. Aerospace Science and Technology, 33 . pp. 55-64. ISSN 1270-9638

Pashilkar, AA (2014) Trends in Simulation Technologies for Aircraft Design. Journal of Aerospace Science and Technology, 22 (1). pp. 1-10.

Kamali, C and Pashilkar, AA and Indira, N and Goyal, Anup and Premalatha, and Mudkavi, Vidyadhar Y (2013) Modeling and Simulation of Wake Encounter for a Fighter Aircraft. International Journal of Aerospace Innovations, 4 (3-4). pp. 65-74. ISSN 1757-2258

Ismail, Shaik and Pashilkar, AA and Ramakalyan, Ayyagari and Sundararajan, N (2013) Neural-Sliding Mode Augmented Robust Controller for Autolanding of Fixed Wing Aircraft. Journal of Artificial Intelligence and Soft Computing Research, 2 (4). pp. 317-330. ISSN 2083-2567

Kamali, C and Pashilkar, AA (2011) Evaluation of Recursive Least Squares algorithm for parameter estimation in aircraft real time applications. Aerospace Science and Technology, 15 (3). pp. 165-174. ISSN 1270-9638

Kamali, C and Pashilkar, AA and Raol, JR (2007) Real time parameter estimation for reconfigurable control of unstable aircraft. Defence Science Journal, 57 (4). pp. 527-537.

Pashilkar, AA and Sundararajan, N and Saratchandran, P (2007) Adaptive nonlinear neural controller for aircraft under actuator failures. Journal of Guidance, Control and Dynamics, 30 (3). pp. 835-847. ISSN 1533-3884

Kamali, C and Pashilkar, AA and Raol, JR (2007) Real time parameter estimation for reconfigurable control of unstable aircraft. Defence Science Journal . pp. 341-352.

Raja, S and Pashilkar, AA and Sreedeep, R and Kamesh, JV (2006) Flutter control of a composite plate with piezoelectric multilayered actuators13;. Aerospace Science and Technology, 10 (5). pp. 435-441.

Pashilkar, AA (2002) Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack13; 13;. Defence Science Journal, 52 (4). pp. 417-427.

Pashilkar, AA and Pradeep, S (2001) Computation of flight mechanics parameters using continuation techniques. Journal of Guidance, Control and Dynamics, 24 (2). pp. 324-329.

Kamali, C and Bhogle, JR and Pashilkar, AA (1996) Implementation of real-time parameter estimation in LabVIEW and DSP. Journal of Aerospace Science and Technologies . pp. 353-397.

Proj.Doc/Technical Report

Kamali, C and Pashilkar, AA (2009) Nonlinear aerodynamic model structure determination using statistical measures. Project Report. National Aerospace Laboratories, Bangalore.

Kamali, C and Pashilkar, AA (2007) Modeling And Estimation Of Non-Linear Aerodynamic Coefficient Dependencies For Aero Database Update Of High Performance Aircraft. Technical Report. NAL, Bangalore.

Kamali, C and Pashilkar, AA (2006) Study of RLS for Stability Margin Evaluation and Post Failure Data Analysis. Project Report. National Aerospace Laboratories, Bangalore.

Kamali, C and Pashilkar, AA (2006) Real Time Parameter Estimation For Reconfigurable Control Of Unstable Aircraft. Project Report. National Aerospace Laboratories.

Pashilkar, AA and Sundararajan, N and Saratchandran, P (2005) Adaptive backstepping neural controller for aircraft autolanding. Technical Report. National Aerospace Laboratories, Bangalore, India.

Jugseniya, Chandrakant B and Pashilkar, AA (2005) Thermodynamic Analysis of Turbofan Engine. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA (2005) Enhanced Fault-Tolerant Neural Controller for Aircraft Auto-Landing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kapadi, Yogesh and Pashilkar, AA (2005) Aero-Thermodynamic Model for Digital Simulation of Turbofan Engine. Project Report. National Aerospace Laboratories, Bangalore.

Kapadi, Yogesh and Pashilkar, AA (2005) Aero-Thermodynamic Model for13; Digital Simulation of13; Turbo of an Engine. Technical Report. National Aerospace Laboratories, Bangalore, India.

Padma, Madhuranath and Thomas, Moncy T and Lathasree, P and Pashilkar, AA and Srikanth, K P (2004) Flight Dynamic Modeling and Simulation of LCA Closing Report. Technical Report. NAL, Bangalore.

Pashilkar, AA (2003) FAST user's manual version 0.1. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA (2003) LS 1 M user's manual version 0.1. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA (2003) SARAS rigid response to turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.

Rao, Shankarnarayan TV and Aswath, C and Govindarajaswamy, E and Krishnamurthy, V and Venkatasubramanyam, DV and Pashilkar, AA (2002) 4m x 8m HAL autoclave temperature and vacuum control system design. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA and Jategaonkar, RV (1998) Some Investigations Related to Gradients for Aircraft Parameter Estimation. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA and Sara, FA (1995) Landing Gear Modelling for Flight Simulation Part I. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA (1995) Landing Gear Modelling For Flight Simulation - Part II. Technical Report. NAL, Bangalore.

Pashilkar, AA (1994) Beta-splines for Data Smoothing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kamali, C and Pashilkar, AA Real Time Parameter Estimation For Reconfigurable Control of unstable Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Wed Sep 2 03:43:50 2015 IST.