Items where Author is "Pashilkar, A. A"

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Number of items: 11.

Conference or Workshop Item

Pashilkar, A. A 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, A. A (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, A. A (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, A. A (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, A. A (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, A. A (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.

Proj.Doc/Technical Report

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

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

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

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

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

This list was generated on Mon Sep 1 01:55:00 2014 IST.