• Ghosh, A. K., Misra, A., and Rakesh Kumar, "Parameter Estimation from Flight Data of Hansa-3 Aircraft using Quasi-steady Stall Modeling", Journal of Aerospace Engineering, ASCE, USA, Vol. 26, No. 3,July, 2013.

• 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.

Office

Office Phone: 0512-259-7716 (O) / 0512-259-8221 (R)
0512-259-7729 / 7807 (Flight Lab)

Fax: 0512-259-7561

Email: akg[AT]iitk.ac.in