Education

Phd (Aerospace Engineering) - Indian Institute of Technology Kanpur, 2016

M.Tech (Aerospace Engineering) - Indian Institute of Technology Kanpur, 2007

B.Tech (Aeronautical Engineering) - Madras Institute of Technology, Chennai, 2005

Course Offered

AE 111 - Introduction to Aerospace Engineering

AE 321 - Atmospheric Flight Mechanics

Area of Interest

Aerospace system identification, Flight Dynamics, Flight Tests, Aircraft Design

Publications

1. Dhayalan, R; Saderla, S; Ghosh, AK; “Parameter Estimation of UAV from flight data using Neural networks”, Aircraft Engineering and Aerospace Technologies, https://doi.org/10.1108/AEAT-03-2016-0050.

2. Saderla, S; Dhayalan, R; Ghosh, AK; “Lateral Directional Parameter Estimation of a small unmanned aerial vehicle using Conventional and Neural based methods”, The Aeronautical Journal, Cambridge University Press, Accepted, Dec. 2016.

3. Saderla, S; Dhayalan, R; Ghosh, AK; “Non-linear aerodynamic modelling of unmanned cropped delta configuration from experimental data”, The Aeronautical Journal, Cambridge University Press, Pages, 1-21, 2017, https://doi.org/10.1017/aer.2016.124

4. Saderla, S; Dhayalan, R; Ghosh, AK; “Parameter Estimation from Near Stall Flight Data using Conventional and Neural-based Methods”, Defence Science Journal, Vol. 67, No: 1, Pages, 03-11, 2016, 10.14429/dsj.67.9995

5. Saderla, Subrahmanyam; Rajaram, Dhayalan; Ghosh, AK; “Parameter estimation of unmanned flight vehicle using wind tunnel testing and real flight data”, Journal of Aerospace Engineering, American Society of Civil Engineers, Aug 2016, http://dx.doi.org/10.1061/(ASCE)AS.1943-5525.0000679

6. Subrahmanyam Saderla, Dhayalan R, Ajoy Kanti Ghosh, (2016),"Longitudinal parameter estimation from real flight data of unmanned cropped delta flat plate configuration", International Journal of Intelligent Unmanned Systems, Vol. 4 Iss 1, pp. 2 – 22. http://dx.doi.org/10.1108/IJIUS-07- 2015-0008.