A. K. Ghosh Email: This email address is being protected from spambots. You need JavaScript enabled to view it.

Professor of Aerospace Engineering

Office Phone: 91(512)2597716

Fax : +91-512-2597561
   

 Research Interests


Flight Mechanics, 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

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+ - Awards & Honors Click to collapse

  • Recipient of DRDO Technology Award, 1993.
  • Best paper award - Inhouse Journal "Shastra Shakti" ARDE, Pune

+ - Primary Teaching Area Click to collapse
Aerospace Engineering
+ - Positions & Employment Click to collapse

Teaching at IIT Kanpur


Taught several courses at the undergraduate and graduate level. These include:-

1. Introduction to Flight Mechanics
2. Airplane performance
3. Stability and Control
4. Introduction to Experiments in Flights
5. Aircraft Design
6. Flight Dynamics 

Research Experience
 
AT DRDO:

1. Scientist, DRDO, Ministry of Defense, India (1982 -1994): Aerodynamic Design and Development of
 


a. Unguided Rocket-PINAKA
b. Mortar Bomb
c. High Speed low drag Bomb, 250Kg, 450Kg
d. Anti-tank ammunition for ARJUN tank and T-72 tank
 
AT IIT Kanpur:

2. Design and Development of:
 


a. Five degrees of Freedom Dynamic Test Rig
b. Parafoil
c. Guided Bomb
d. Lattice Fin
e. FAE Bomb
f. Glider based Torpedo delivery system
g. Parafoil based delivery system
h. Akashdeep Aerostat
i. Stratospheric Airship

3. Parameter estimation using neural network from flight data of light combat aircraft.

4. Estimation of aerodynamic parameter through wind tunnel testing

5. Post flight analysis of flight data of unguided rocket and anti-tank ammunition.

6. Research work on development of supercavitating vehicle

7. Development of control laws using Non linear Dynamic Inversion Technique

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Professor Aerospace Engineering Department & Faculty Incharge-Flight Labortory

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+ - Books & Publication Click to collapse
Conferences

S. No Author(s) Year Title Name and Place of Conference
  1. 1.
 Subrahmanyam Saderla,Sunil Sharma, A K Ghosh 2011 Analytical Modeling Trajectory Simulation and Control of Guided Projectiles Annual International Conference on Control, Automation and Robotics, CAR 2011 28th February- 1st March 2011, Hotel Fort Canning, Singapore
  1. 2.
 Sunil Sharma, A K Ghosh 2011 Simulation and control of highly maneuverable aircraft under turbulent atmosphere using Nonlinear Dynamic Inversion Technique CHAOS 2011, 4th Chaotic Modeling and Simulation International Conference, May 31 - June 3, 2011 Agios Nikolaos, Crete, Greece
  1. 3.
 Anuj Kumar Garg, Santosh Kumar Burnwal, Asish Pallapothu, Rohit Singh Alawa & A K Ghosh 2011 Solar Panel Area Estimation and Optimization for Geostationary Stratospheric Airships 11th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, 20-22 September 2011, Virginia Beach, Virginia, USA
  1. 4.
 Anuj Kumar Garg, Santosh Kumar Burnwal, Asish Pallapothu, Rohit Singh Alawa & A K Ghosh 2011 Impact of Helium Permeability and Altitude Control of Geostationary Stratospheric Airship – A Mathematical Model 11th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, 20-22 September 2011, Virginia Beach, Virginia, USA
  1. 5.
 Asish Pallapothu, Anuj Kumar Garg, Rohit Singh Alawa, Santosh Kumar Burnwal & A K Ghosh 2011 Modeling and Simulation of possible Controlled and Uncontrolled modes of launch of Stratospheric Airship The 4th Chaotic Modeling and Simulation International Conference, 31 May - 3 June 2011 Agios Nikolaos Crete Greece.
  1. 6.
 Anuj Kumar Garg, Asish Pallapothu, Rohit Singh Alawa, Santosh Kumar Burnwal, Ridhi Bhatia, Gaurav Singh & A K Ghosh 2011 Design Analysis and Optimization of Geostationary Stratospheric Airship Hull and Fins International Seminar Aero India 2011, 7-9 Feb 2011, Bangalore, India
  1. 7.
 Asish Pallapothu, Subramanyam Saderla & A K Ghosh 2011 Design Analysis and Fabrication of a scaled down Radio Controlled Variable Stability Aircraft International Seminar Aero India 2011, 7-9 Feb 2011, Bangalore, India
  1. 8.
 Balraj Gupta, S C Upadhyaya, Vipin Kumar, Ravi Krishna & A K Ghosh   Aerodynamic characteristics of 15-cell Ram Air Parachute Designed for Precision Delivery 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, USA
  1. 9.
 Balraj Gupta, S C Upadhyaya, Vipin Kumar, Ravi Krishna & A K Ghosh   Trajectory Simulation of Large Ram Air Parachute Using 9-DOF Model 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, USA
  1. 10.
 Balraj Gupta, S C Upadhyaya, Vipin Kumar, Ravi Krishna & A K Ghosh December 10-12, 2009 Mathematical and Experimental methods of Load estimation on Control Lines of Ram Air Parachute Proceeding of Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), , Bangalore, India
  1. 11.
 Peyada, N. K., Ghosh, A. K., and Go, T. H.,   Mathematical Modeling, Simulation and Estimation of Aircraft Parameters using 5 DOF Dynamic Test Rig IMech E, Part G: J. Aerospace Engineering
  1. 12.
 G.G. Dutta, Ankur Singhal and A.K. Ghosh, 07- 09 Sept. 2009. Estimation of Drag Coefficient from Free Flight Data of an Artillery Rocket using Neural Networks IASTED International Conference on Applied Simulation and Modeling (ASM), Palma de Mallorca, Spain,
  1. 13.
 Peyada, N. K. and Ghosh, A. K. Aug 10-13, 2009 Aircraft Parameter Estimation using Neural Network based Algorithm INCPAA- 2008, AIAA Atmospheric Flight Mechanics Conference, Chicago, Illinois, USA
  1. 14.
 Peyada, N. K., Sen, A., Dutta, G. G., Singhal, A., Rajan, K. M., Raj, A. and Ghosh, A. K. Nov. 20-22, 2008 Effect of Mach Number on Supersonic Wrap Around Fin Aerodynamics National Conference on Advances in Armament Technology, ARDE, Pashan, Pune, India,.
  1. 15.
 Sen, A., Peyada, N. K., Subrahmanyam, S., Wahi, P. and Ghosh, A. K. Nov. 20-22, 2008 5-Degree of Freedom Dynamic Rig for Wind Tunnel Tests of Aerospace Vehicles National Conference on Advances in Armament Technology, ARDE, Pashan, Pune, India.
  1. 16.
 Peyada, N. K., Sen, A. and Ghosh, A. K. April 5-6, 2008 Aerodynamic Characterization of HANSA-3 Aircraft using Equation Error, Maximum Likelihood and Filter Error Method s 2nd Joint Workshop in Mechanical, Aerospace and Industrial and Management Engineering, IIT Kanpur, Kanpur, India,.
  1. 17.
 Ghosh, A. K., Peyada, N. K. April 5-6, 2008 Aircraft Parameter Estimation from Flight Data using Neural-Gauss-Newton Method 2nd Joint Workshop in Mechanical, Aerospace and Industrial and Management Engineering, IIT Kanpur, Kanpur, India .
  1. 18.
 Peyada, N. K. and Ghosh, A. K. June 25-27, 2008 Parameter Estimation from Real Flight Data using Neural Network based Method INCPAA- 2008, Mathematical Problems in Engineering, Aerospace and Sciences, University of Genoa, Italy.
  1. 19.
 Peyada, N. K. and Ghosh, A. K. March 28-29, 2008 Aerodynamic Parameter Estimation using New Filtering Technique Based on Neural Network and Gauss-Newton Method ARMS 2008, ARDE, Pashan, Pune
  1. 20.
 Peyada, N. K., Sen, A. and Ghosh, A. K. March 19-21, 2008 Aerodynamic Characterization of HANSA-3 Aircraft using Equation Error, Maximum Likelihood and Filter Error Methods International Multiconference of Engineers and Computer Scientists, Hong Kong,.
  1. 21.
 Peyada, N. K. and Ghosh, A. K 28th to 30th November 2007 Estimation of Aerodynamic Parameters from Real Flight Data Using Filter Error Method with Typical Initial Process Noise International Conference and Exhibition on Emerging Challenges in Design and Manufacturing Technologies -2007, Sathyabama University, Chennai, India,.
  1. 22.
 Peyada, N. K. and Ghosh, A. K., 22nd& 23rd, Nov. 2007. Dynamic Stability Analysis of a Parafoil-Payload System using Analytically Derived Stability Derivative SAROD-2007,Trivandrum, India
  1. 23.
 Peyada, N. K. Sen, A. and Ghosh, A. K., 16th -17th Nov. 2007 Longitudinal Aerodynamic Characteristic of Hansa-3 Aircraft Using Real Flight Data 21st National Convention of Aerospace Engineers, IIT Kanpur, India
  1. 24.
 Peyada, N. K., Singhal, A. and Ghosh, A. K. May 2007 Trajectory Modeling of a Parafoil in Motion Using Analytically Derived Stability Derivative at High Angle of Attack 19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, Williamsburg, VA, USA
  1. 25.
 S. Singh and A.K. Ghosh 2007 Improved delta Method for Parameter Estimation from Real Flight Data of an Aircraft using Neural Networks Accepted to 17th IFAC Symposium on Automatic Control in Aerospace, Toulouse, France, 24th – 29th June 2007
  1. 26.
 N.K. Peyada, Ankur Singhal, A.K. Ghosh 2007 Trajectory Modeling of a Parafoil in Motion Using Analytically Derived at High Angle of Attack 19th AIAA Aerodynamic Decelerator Systems Technology Conference Seminar, Virginia, USA, 21-24th May, 2007
  1. 27.
 NGR Iyengar, AK Ghosh, Ankur Singhal 2007 “Concurrent approach for aviation infrastructure and manpower development” National Seminar on “Aviation Infrastructure In India”, Kochi, 18-19Feb, 2007
  1. 28.
 G.G. Dutta, Ankur Singhal, A.K. Ghosh 2006 Estimation of Drag Coefficient from Flight Data of an Artillery Shell and Rocket International Congress on Computational Mechanics and Simulation(ICCMS-06), IIT Guwahati, 8-10 Dec, 2006
  1. 29.
 Ujjwala Darvemula, Ankur Singhal and A.K. Ghosh, 2006 Application of Maximum Likelihood Method for Aerodynamic Parameter Estimation from Flight Data of a Typical Parafoil International Congress on Computational Mechanics and Simulation(ICCMS-06), IIT Guwahati, 8-10 Dec, 2006
  1. 30.
 G.G. Dutta, Ankur Singhal, A.K. Ghosh 2006 Estimation of Drag Coefficient Using Real Radar Tracked Data of an Artillery Shell Proceedings AIAA Paper No. 2006-6149, AIAA Atmospheric Flight Mechanics Conference and Exhibit-06, Keystone, Colorado21st-24th Aug,2006
  1. 31.
 Sanjay Singh, A.K. Ghosh, 2006 Parameter Estimation From Flight Data Using Maximum Likelihood Method And Neural Network Proceedings AIAA Paper No. 2006-5820, AIAA Atmospheric Flight Mechanics Conference and Exhibit-06, Keystone, Colorado21st-24th Aug,2006
  1. 32.
 S. K. Gupta, S. Saxena, A. K. Ghosh 2006 On Implementation of Trajectory Correction System on a Routinely Used Artillery Rocket Proceedings AIAA Paper No. 2006-6012, AIAA Atmospheric Flight Mechanics Conference and Exhibit-06, Keystone, Colorado, 21st-24th Aug,2006
  1. 33.
 K.V.Chandra Shekar, G.G. Dutta, Ankur Singhal, I.V.S. Sridhar, A.K. Ghosh 2006 Estimation of Drag Coefficient from Free Flight Trajectory Data of an Artillery Shell Proceedings of 19th Convention for Aerospace Engineer-2005, Institution of Engineers (INDIA), Rajasthan Chapter, Jaipur, INDIA
  1. 34.
 Ujjwala Darvemula, A. Singhal, A.K. Ghosh, 2006 Parameter Estimation from Flight Data of A Typical Parafoil Using Maximum Likelihood Method Proceedings of 19th Convention for Aerospace Engineer-2005, Institution of Engineers (INDIA), Rajasthan Chapter, Jaipur, INDIA
  1. 35.
 A.K.Ghosh, Ankur Singhal, Ayush Jha, 2005 Flight Path Prediction of an Artillery Shell Using Feed Forward Neural Networks Proceedings AIAA Atmospheric Flight Mechanics Conference Paper No. 2005-5820, Austin, Texas, 11 - 14 Aug 2005.
  1. 36.
 A. K. Ghosh and P. N. Dewedi 2005 Non-Linear Control Law with Application to High Angle-of-Attack of Flight Using Neural Network Conference on Non-Linear Dynamic Systems, IIT Bombay
  1. 37.
 A. Singhal, Ujjwala D. and A. K. Ghosh 2005 On application of parameter estimation methods to flight data of a typical parafoil Conference held at ADRDE, Agra, March 13
  1. 38.
 A. K. Ghosh and Om Prakash 2003 Neural Models for Predicting Trajectory Performance of an Artillery Rocket AIAA Atmospheric Flight Mechanics Conference, Austin, Texas, 11 - 14 Aug 2003
  1. 39.
 S. C. Raisinghani, and A. K. Ghosh 2002 Parameter Estimation of an Unstable Aircraft in Turbulent Atmosphere using Neural Networks AIAA Atmospheric Flight Mechanics Conference, Hyatt Regency Monterey, California, USA, Aug. 5-8, Paper No. 2002-4623
  1. 40.
 A. K. Ghosh, S. C. Raisinghani and L. K. Patnaik 2000 Parameter Estimation from Flight Data with Process and Measurement Noise Using Neural Networks AIAA Atmospheric Flight Mechanics Conference, Denver Marriott Technical Center, Colorado, USA, Aug. 14-17, 2000.
  1. 41.
 A. K. Ghosh and S. C. Raisinghani 2000 Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks AIAA Atmospheric Flight Mechanics Conference, Denver Marriott Technical Center, Colorado, USA, Aug. 14-17, 2000
  1. 42.
 S. C. Raisinghani, G. V. S. Bhaskar Reddy and A. K. Ghosh 1999 Parameters Estimation of an Augmented Aircraft using Neural Networks AIAA Atmospheric Flight Mechanics Conference, Double Tree Hayden Island, Portland, OR, USA, Aug. 9-11, 1999
  1. 43.
 S. C. Raisinghani, Ch. Srinivasa Rao and A. K. Ghosh 1999 Effects of Measurement Errors on Parameter Estimation via Neural Networks AIAA Atmospheric Flight Mechanics Conference, Double Tree Hayden Island, Portland, OR, USA, Aug. 9-11, 1999
  1. 44.
 S. C. Raisinghani, A. K. Ghosh and P. K. Kalra 1998 Aircraft Lateral-Directional Parameter Estimation via Neural Networks Proceedings of 49th AGM, The Aeronautical Society of India, pp. 6.1-6.7
  1. 45.
 A. K. Ghosh, D. K. Joshi and A. V. Rao 1995 A Simplified approach for prediction of Fire for unguided Rockets 15th International Symposium of Ballistics, Jerusalem, Israel
  1. 46.
 S. C. Raisinghani and A. K. Ghosh 1990 Parameter Estimation of an Augmented Airplane with Unsteady Aerodynamic Modelling Proceedings of the 17th International Symposium on Space Technology and Science, Tokyo, Japan, pp. 699-706

Journals
S. No. Author(s) Year Title Complete reference of Journal
  1. 1.
 Rakesh Kumar and Dr. A.K. Ghosh   Parameter estimation using unsteady downwash model from real flight data of Hansa-3 aircraft Aeronautical Journal, Royal Aeronautical Society, UK
  1. 2.
 Rakesh Kumar and Dr. A.K. Ghosh   Nonlinear Longitudinal Aerodynamic Modeling using Quasi-steady Stall Model and Neural Gauss-Newton Method Journal of Aircraft AIAA, USA
  1. 3.
 Rakesh Kumar, A. K. Ghosh,S. Srivastava, Balraj Gupta and Ajit Kumar   Parametric Trend Study during Stability Analysis of a Tethered Aerostat Journal of Aerospace Sciences and Technologies, Aeronautical Society of India
  1. 4.
 Rakesh Kumar, Ajay Misra and Dr. A.K. Ghosh   Modeling of Cascade Fin Aerodynamics near Stall using Kirchhoff’s Steady-steady Stall Model Defense Science Journal
  1. 5.
 Balraj Gupta, S C Upadhyaya, Vipin Kumar, Ravi Krishna & A K Ghosh   Estimation of Load on Control Lines of Ram Air Parachute Designed for Precise Delivery using 9-DOF Model Journal of Aerospace Science and Technologies, India
  1. 6.
 Peyada, N. K., and Ghosh, A. K May 2009 Longitudinal Aerodynamic Parameter Estimation using Neural Network and Gauss-Newton Method Journal of Aerospace Science and Technology
  1. 7.
 Peyada, N. K., and Ghosh, A. K. April 2009 Aircraft Parameter Estimation using New Filtering Technique based on Neural Network and Gauss-Newton Method Aeronautical Journal, UK
  1. 8.
 Peyada, N. K., Sen, A. and Ghosh, A. K. Nov. 2008 Longitudinal Aerodynamic Characteristic of HANSA-3 Aircraft using Real Flight Data The Journal of Institution of Engineers, INDIA. Vol. 89, , pp 9-14.
  1. 9.
 S. Singh and A.K. Ghosh 2007 Modified delta Method for Parameter Estimation from Real Flight Data of an Aircraft using Neural Networks The Aeronautical Journal, UK -
  1. 10.
 S. Singh and A.K. Ghosh 2007 Longitudinal Parameter Estimation using Wind Tunnel and Simulated Flight Data of Tactical Missile Journal of Aerospace Sciences and Technologies, May 2007-
  1. 11.
 S. K. Gupta, S. Saxena, Ankur Singhal and A. K. Ghosh 2007 A Test Case on Implementation of Trajectory Correction Flight Control System Using Pulse Jet on An Artillery Rocket Defense Science Journal, INDIA-
  1. 12.
 A. K. Ghosh, G. Sagoo and A. Singhal 2006 Wind Tunnel Investigation of Typical Strategic Missiles configuration at high angle-of-attack Journal of Aerospace, Science and Technology, Vol. 58, No. 1, Feb. 2006, pp. 75-81
  1. 13.
 A. K. Ghosh, and Om Prakash 2004 Neural Model for Predicting Trajectory Performance of an Artillery Rocket JACIC, Vol. No. 2, Feb., 2004, PP. 112-115
  1. 14.
 A. K. Ghosh, IVS Sridhar and A. Singhal and OM Prakash 2004 Estimation of Drag Coefficient from Radar Tracked trajectory data of an artillery shell Journal of Aerospace Sciences and Technologies, Vol. 56, No. 1, Feb, 2004.
  1. 15.
 A. K. Ghosh, Om Prakash, IVS Sridhar and A. Singhal 2003 Trajectory modeling of an artillery shell using feed forward neural networks Journal of the Institution of Engineers (India), Vol. 84, November, 2003, pp. 47-49.
  1. 16.
 A. K. Ghosh, Aslam Khan and S. C. Raisinghani 2002 Estimation of Longitudinal Parameters from Real-Flight Data Using Neural Networks Journal of Aeronautical Society of India, Vol. 54, No. 3, pp. 16-22
  1. 17.
 A. K. Ghosh, S. C. Rainsinghani and S. K. Dehury 2002 Neural Models for Predicting Performance of an Artillery Shell Journal of Aeronautical Society of India, Vol. 54, No. 1, February, 2002, pp. 273-279
  1. 18.
 A. K. Ghosh, S. C. Raisinghani and S. K. Dehury 2002 Modeling of Performance of an Artillery Shell using Neural Networks Journal of Spacecraft and Rocket, Vol. 39, No. 3, May-June, 2002, pp. 470-472
  1. 19.
 A. K. Ghosh and S. C. Raisinghani 2002 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.
  1. 20.
 A. K. Ghosh and S. C. Raisinghani 2001 Frequency-Domain Estimation of Parameters From Flight Data using Neural Network Journal of Guidance, Control and Dynamics, Vol. 24, No. 3, pp. 525-530.
  1. 21.
 S. C. Raisinghani and A. K. Ghosh 2000 Parameter Estimation of an Aeroelastic Aircraft using Neural Networks Journal of Sadhana, Vol. 25, Part 2, pp. 181-191
  1. 22.
 S. C. Raisinghani, A. K. Ghosh and P. K. Kalra 1998 Two new Techniques for Parameter Estimation using Neural Networks The Aeronautical Journal, U.K., Vol. 102, No. 1011, pp. 25-29.
  1. 23.
 A. K. Ghosh, S. C. Raisinghani and S. Khubchandani 1998 Estimation of Aircraft Lateral-Directional Parameters using Neural Networks Journal of Aircraft, Vol. 35, No. 6, pp. 876-881
  1. 24.
 A. K. Ghosh and S. C. Raisinghani 1993 Parameter Estimation of an Aeroelastic Aircraft as Affected by Model Simplifications Journal of Aircraft, Vol. 31, No. 2, pp. 452-454

  

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  • List of M.Tech. Thesis
  • List of PhD Thesis

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+ - Contact Information Click to collapse
Prof. A. K. Ghosh
Professor
Aerospace Engineering Department
& Faculty Incharge-Flight Labortory
Indian Institute of Technology, Kanpur (U.P.) - 208016

Office
Coordinates : NL115Phone : +91-512-2597716 (O) , +91-512-2598221 (R)+91-512-2597729, +91-512-2597807 (Flight Lab)

Fax : +91-512-2597561

Email: This email address is being protected from spambots. You need JavaScript enabled to view it.
+ - Keywords Click to collapse

Flight Mechanics Mechanics of flight
  Aircraft flight mechanics
 

Bird flight mechanics 
Parameter Estimation from flight data Aerodynamic test
 

Aerospace design process 
Neural modeling Design of Air Borne stores: Aircraft Bombs Aircraft design engineering
 

Propulsion system in aircraft 
Artillery shells and Rockets Design of Control law of guided missiles Gps guided missiles
  Mortar artillery
  Aircraft missiles
  Rocket guidance and control

 

Education

  • B.Tech. (Aerospace), IIT Kanpur

  • M.Tech. (Aerospace), IIT Kanpur

  • Ph.D. (Aerospace), IIT Kanpur

Websites

CV