|
S. No
|
Author(s)
|
Year
|
Title
|
Name
and Place of Conference
|
|
1.
|
Salahudden., Kumar Praful., Giri, D. K., and A.K Ghosh
|
2020
|
Quaternion Based Optimal Controller for Momentum Biased Nadir Pointing Satellite
|
IEEE Aerospace Conference, Big Sky, MT, 7-14 March 2020
|
|
2.
|
Salahudden., Dwivedi V.S., and Ghosh , A.K
|
2020
|
Flight-States and Control Inputs Computation using Nonlinear Programming for Unmanned Air vehicle
|
AIAA Aviation Forum, Reno, Nevada, 2020
|
|
3.
|
Salahudden., and Ghosh, A.K
|
2020
|
Steady-Straight-Level Flight Study: A Mathematical Optimization Approach and Flight Test
|
AIAA Aviation Forum, Reno, Nevada, 2020
|
|
4.
|
Salahudden., Giri, D. K., and Ghosh, A.K
|
2020
|
Aircraft Stall Recovery using Sliding-Mode Based Pitch-Attitude and Altitude Control
|
International Conference on Unmanned Aircraft Systems, Athens, Greece, 9-12 June 2020
|
|
5.
|
Salahudden., Dwivedi, P.N., and Ghosh, A.K
|
2020
|
Aircraft Flat-Spin Recovery with Altitude Loss Reduction using Sliding-Mode-Based Closed-Loop Thrust Control
|
AIAA SciTech Forum, 2020
|
|
6.
|
Salahudden, Giri, D. K., Subham, D., and Mukherjee , B. K.
|
2019
|
Angular rate stabilization using fixed-time continuous sliding mode control
|
2019 Fifth Indian Control Conference (ICC), IITH, Hyderabad, 18-20 December, 2019
|
|
7.
|
Dwivedi, V.S., Salahudden., Ghosh, A.K., and Kamath, G. M
|
2019
|
Design Studies to Achieve Energy Optimal Attitude for a Solar-Powered Aircraft
|
IEEE Aerospace Conference, Big Sky, Montana, 2-9 March 2019
|
|
8.
|
Subham, D., Dwivedi, V.S., Salahudden., and Giri, D. K,
|
2019
|
Fixed-Time Attitude Control of Satellite Using Combined Magnetic and Magneto-Coulombic Actuators
|
IEEE Aerospace Conference, Big Sky, Montana, 2-9 March 2019
|
|
9.
|
Salahudden., Dwivedi V.S., and Ghosh, A.K.
|
2019
|
Roll Angle Optimization in Coordinated Level Turn Flight and its Analytical Validation for UAV
|
IEEE Aerospace Conference, Big Sky, Montana, 2- 9 March 2019
|
|
10.
|
Salahudden, Giri, D. K., and A.K Ghosh
|
2019
|
Robust Controller Design for Bank to Turn Asymmetric High-Speed Projectile with Uncertainties
|
IEEE Aerospace Conference, Big Sky, MT, 7-14 March 2019
|
|
11
|
. S. Dey, D. K. Giri, V. Laxmi, and A. K. Ghosh
|
2018
|
Time-Varying Non-Singular Terminal Sliding Mode Attitude Control of Reusable Launch Vehicle
|
15th International Conference on Control, Automation, Robotics and Vision, Singapore, 19-21 Nov., 2018
|
|
12.
|
Kumar, Ajit, and Ajoy K. Ghosh.
|
2018
|
"Data-Driven Method based Aerodynamic Parameter Estimation from Flight Data.
|
In 2018 AIAA Atmospheric Flight Mechanics Conference, p. 0768. 2018
|
|
13.
|
Kumar, Ajit, and Ajoy Kanti Ghosh.
|
2017
|
Aerodynamic Parameter Estimation using LASSO Regression Method from Flight Data
|
Proceedings of ICTACEM, IIT Kharagpur, December, 2017
|
|
14.
|
Kumar, Ajit, and Ajoy Kanti Ghosh.
|
2017
|
Lateral-Directional Aerodynamic parameter Estimation using Neuro-Fuzzy based Method
|
Proceedings of International Conference on Computational Intelligence: Theories, Applications and Future Directions, IIT Kanpur, December, 2017
|
|
15.
|
Kumar, Ajit, Subrahmanyam Saderla, and Ajoy Kanti Ghosh
|
2017
|
Aerodynamic parameter estimation using neuro-fuzzy model based method
|
International Conference on Recent Advances in Aerospace Engineering, IEEE, Coimbatore, 2017
|
|
16.
|
Srivastava, Ambuj, Ajit Kumar, and A. K. Ghosh.
|
2017
|
Estimation of lift and drag characteristics of light transport aircraft in the presence of ground effect during landing
|
International Conference on Recent Advances in Aerospace Engineering, IEEE, Coimbatore, 2017
|
|
17.
|
Subrahmanyam S, Sunil S and A. K. Ghosh
|
2011
|
Analytical Modeling Trajectory Simulation and Control of Guided Projectiles
|
presented in Control Automation and Robotics conference 2011, Singapore
|
|
18.
|
Dayalan, R., Ghosh, A. K
|
2013
|
Estimation of Nonlinear Parameters from Simulated Data of an Aircraft
|
2nd CEAS specialist conference on guidance, navigation, and control, (Netherlands) 2013
|
|
19.
|
. Kumar, R., Ghosh, A. K.
|
2013
|
Lateral Parameter Estimation using conventional and Neural based methods
|
15th Australian International Aerospace Congress (AIAC-15), (Australia) 2013
|
|
20.
|
Kumar, R., Ghosh, A. K
|
2012
|
Longitudinal Stability Analysis of an Aerostat
|
International Conference on Applications of Fluid Engineering (CAFE-12), 2012
|
|
21.
|
Kumar, R., Ghosh, A. K.
|
2012
|
The effect of Indicial Lift Function on Parameter Estimation
|
International Conference on Applications of Fluid Engineering (CAFE-12), 2012
|
|
22.
|
Sharma, S., Ghosh, A. K.,
|
2011
|
Simulation and Control of Highly Maneuverable Aircraft under Turbulent Atmosphere using Nonlinear Dynamics Inversion Technique
|
4th Chaotic Modeling and Simulation International Conference, (Greece) 2011
|
|
23.
|
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
|
|
24.
|
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
|
|
25.
|
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
|
|
26.
|
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
|
|
27.
|
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.
|
|
28.
|
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
|
|
29.
|
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
|
|
30.
|
Balraj Gupta, S C Upadhyaya, Vipin
Kumar, Ravi Krishna & A K Ghosh
|
2009
|
Aerodynamic characteristics of 15-cell
Ram Air Parachute Designed for Precision
Delivery
|
21st AIAA Aerodynamic Decelerator
Systems Technology Conference and
Seminar, USA
|
|
31.
|
Balraj Gupta, S C Upadhyaya, Vipin
Kumar, Ravi Krishna & A K Ghosh
|
2009
|
Trajectory Simulation of Large Ram Air
Parachute Using 9-DOF Model
|
21st AIAA Aerodynamic Decelerator Systems
Technology Conference and Seminar, USA
|
|
32.
|
Balraj Gupta, S C Upadhyaya, Vipin
Kumar, Ravi Krishna & A K Ghosh
|
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
|
|
33.
|
Peyada, N. K., Ghosh, A. K., and Go, T.
H.,
|
2009
|
Mathematical Modeling, Simulation and
Estimation of Aircraft Parameters using
5 DOF Dynamic Test Rig
|
IMech E, Part G: J. Aerospace
Engineering
|
|
34.
|
|
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,
|
|
35.
|
Peyada, N. K. and Ghosh, A. K.
|
2009
|
Aircraft Parameter Estimation
using Neural Network based Algorithm
|
INCPAA- 2008, AIAA Atmospheric
Flight Mechanics Conference, Chicago,
Illinois, USA
|
|
36.
|
Peyada, N. K., Sen, A., Dutta,
G. G., Singhal, A., Rajan, K. M., Raj,
A. and Ghosh, A. K.
|
2008
|
Effect of Mach Number on
Supersonic Wrap Around Fin Aerodynamics
|
National Conference on Advances
in Armament Technology, ARDE, Pashan,
Pune, India,.
|
|
37.
|
Sen, A., Peyada, N. K.,
Subrahmanyam, S., Wahi, P. and Ghosh, A.
K.
|
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.
|
|
38.
|
Peyada, N. K., Sen, A. and
Ghosh, A. K.
|
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,.
|
|
39.
|
Ghosh, A. K., Peyada, N. K.
|
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 .
|
|
40.
|
Peyada, N. K. and Ghosh, A. K.
|
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.
|
|
41.
|
Peyada, N. K. and Ghosh, A. K.
|
2008
|
Aerodynamic Parameter
Estimation using New Filtering Technique
Based on Neural Network and Gauss-Newton
Method
|
ARMS 2008, ARDE, Pashan, Pune
|
|
42.
|
Peyada, N. K., Sen, A. and
Ghosh, A. K.
|
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,.
|
|
43.
|
Peyada, N. K. and Ghosh, A. K
|
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,.
|
|
44.
|
Peyada, N. K. and Ghosh, A. K.,
|
2007.
|
Dynamic Stability Analysis of a
Parafoil-Payload System using
Analytically Derived Stability
Derivative
|
SAROD-2007,Trivandrum, India
|
|
45.
|
Peyada, N. K. Sen, A. and
Ghosh, A. K.,
|
2007
|
Longitudinal Aerodynamic
Characteristic of Hansa-3 Aircraft Using
Real Flight Data
|
21st
National Convention of Aerospace
Engineers, IIT Kanpur, India
|
|
46.
|
Peyada, N. K., Singhal, A. and
Ghosh, A. K.
|
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
|
|
47.
|
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, 24- 29th June 2007
|
|
48.
|
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
|
|
49.
|
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
|
|
50.
.
|
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
|
|
51.
|
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
|
|
52.
|
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
|
|
53.
|
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
|
|
54.
|
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
|
|
55.
|
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
|
|
56.
|
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
|
|
57.
|
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.
|
|
58.
|
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
|
|
59.
|
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
|
|
60.
|
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
|
|
61.
|
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
|
|
62.
|
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.
|
|
63.
|
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
|
|
64.
|
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
|
|
65.
|
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
|
|
66.
|
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
|
|
67.
|
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
|
|
68.
|
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
|
