Professor, Department of Aerospace Engineering
Flight Mechanics, Flight Testing and Parameter Estimation from flight data, Neural modeling Design of Air Borne stores: Aircraft Bombs, Artillery shells and Rockets Design of Control law of guided missiles. Design of Unmanned Air Vehicle
PhD (Aerospace Engineering),
IIT Kanpur,1998.
M.Tech (Aerospace Engineering), IIT Kanpur,1989.
B.Tech (Aerospace Engineering), IIT Kanpur,1982.
Ghosh, A. K., Misra, A., and Rakesh Kumar, "Parameter Estimation from Flight Data of Hansa-3 Aircraft using Quasi-steady Stall Modeling"
Ghosh, A. K., and Rakesh Kumar, "Nonlinear Modeling of Cascade Fin Aerodynamic using Kirchhoff's Steady-stall Model", Journal of Aircraft, AIAA, USA, Vol. 49, No. 1, Jan.-Feb. 2012, pp. 315-319.
Ghosh, A. K., and Peyada, N. K., "Aircraft Parameter Estimation using New Filtering Technique based on Neural Network and Gauss-Newton Method", Aeronautical Journal, UK, Vol. 113, No. 1142, April 2009, pp. 243-252.
Ghosh, A. K., and S. Singh, "Estimation of lateral-directional parameters from real flight data using neural networks based modified delta method", The Aeronautical Journal, UK, October 2007, Vol. 111, Paper No. 1124.
Ghosh, A. K., and Raisinghani S.C., "Parameter Estimation from Flight Data of an Unstable Aircraft using Neural Networks", Journal of Aircraft, Vol. 39,No. 5, Sept. Oct. 2002, pp. 892-894.
Recipient of DRDO Technology Award,1993.
Honored by DRDO Executive Board for successfully designed,fabricated and test flown Vertical tail less Aura scaled flight configuration.
Letter of appreciation for identifying the dynamic stability problem associated with the artillery rocket configuration –PINAKA MK-II at Mach 3.6
Letter of appreciation for design, analysis and flight testing of AEROSTAT(2000 cubic meter) at Airstrip,IIT Kanpur
Appreciation by senate IIT Kanpur for excellence in teaching on many occasions.