About
My active research areas are Application of Real time system Identification for online fault diagnosis of an aircraft under distress, Online system identification of aircraft undergoing icing condition, Application of parameter estimation for UAV certification, and Adaptive Control using Realtime System Identification.
Assistant Professor
Department of Aerospace Engineering
- Website: https://home.iitk.ac.in/~saderlas/
- Phone: +91-512-259-2009
- Degree: PhD (IIT Kanpur, IN)
- E-mail: saderlas@iitk.ac.in
Course taught:
Fight stability and control (AE648A),(2019,2020,2022)
Flight dynamics (AE647A), (2019,2020,2022)
Experiments in flight mechanics (AE421A), (2020,2021,2022)
Aircraft design (AE461A), (2019,2020,2022)
NPTEL Courses taught:
Design of fixed wing Unmanned Aerial Vehicles
UAV design Part II
New courses introduced:
Development
UAV Lab
Bio
Personal and Professional Information
Summary
Subrahmanyam Saderla
5+ years of teaching experience.
- UAV Laboratory, Department of Aerospace Engineering, IIT Kanpur, India
- +91-512-259-2009
- saderlas@iitk.ac.in
Education
Doctor of Philosophy
2016
Thesis Title:Parameter Estimation using Flight Data of Unmanned Flight Vehicles at Low and Moderately High Angles of Attack Using Conventional Methods
Indian Institute of Technology Kanpur, India
Master of Technology
2010
Thesis Title: Aerodynamic Characterizatin and Trajectory estimation of guided projectiles.
Indian Institute of Technology Kanpur, India
Bachelor of Technology
2008
Institute of Aeronautical Engineering
Hyderabad, India
Professional Experience
Assistant Professor
Jan, 2018 - Present
Department of Aerospace Engineering, IIT Kanpur, India
Postdoctoral Researcher
Sep, 2016 - Dec, 2017
Gyeongsang National University, Jinju, South Korea
Chief Technical Officer (CTO)
Oct, 2015 - Aug, 2016
Srashta Automation Labs Pvt. Ltd., India
Project Scientist, Flight Dynamics
Jul, 2015 - Sep, 2015
Indian Institute of Technology Kanpur, India
Collaborations
VU-Dynamics Private Limited
Start-up incubated at IITK-FIRST under Faculty Entrepreneurship Program
Role: Director
Since 2022
LAB Facilities
Useful in developing the cutting-edge unmanned systems
UAV Testing and Prototyping Facilities
- Dynamic thrust calibration test bench for microjet engines, mini IC engines, Electric Ducted Fans and Brushless Motor
- Static Coaxial Thrust bench for BLDC motors
- UAV rapid prototyping setup using 3D printing
- Ground control Station for UAV communication and flight testing
- Drone battery pack testing and development setup (Lithium Ion and Lithium Polymer)
- Composite curing ovens with vacuum bagging facility (4m x 2m x 2m)
- UAV mold fabrication facility using 3axis CNC router (2.8m x 1.5m x 0.25m)
- Non-metallic template machining facility using laser cutting (1.5m x 1 m x 0.012m)
- Miniature calibration dynamic test rig facility for drone UAV ground station
Developed Technologies
- Real time crowd monitoring/surveillance solution using Aerostat
- Remote pilot training module for UAVs
- Software in the loop simulator for Kamikaze drone
- Tandem wing catapult/canister launched Kamikaze drone
- Hand launch flying wing drone for surveillance
- Pneumatic Catapult Launcher for UAVs
- Pneumatic Canister Launcher for foldable fixed wing UAVs
Publications
Published Articles
Kumar, N., Kishore, G., Saderla, S., and Kim, Y., 2023. An adaptive law based online system identification of cropped delta unmanned aerial vehicles from flight tests, Aerospace Science and Technology, Volume 141. 108526, ISSN 1270-9638, https://doi.org/10.1016/j.ast.2023.108526
Kumar, N., Saderla, S., and Kim, Y., 2023. Aerodynamic characterisation of delta wing unmanned aerial vehicle using non-gradient-based estimator. The Aeronautical Journal, 127(1314), 1435-1451. https://doi.org/10.1017/aer.2023.2
Samuel J, J., Kumar, N., Saderla, S., and Kim, Y., 2023. Parametric model identification of delta wing UAVs using filter error method augmented with particle swarm optimisation. The Aeronautical Journal, 127(1312), 982-1008. https://doi.org/10.1017/aer.2022.100
Kumar, N., Saderla, S., and Kim, Y., 2023. System identification of cropped delta UAVs from flight test methods using particle Swarm-Optimisation-based estimation. The Aeronautical Journal, 127(1307), 76-96. https://doi.org/10.1017/aer.2022.46
S. Saderla, Dhayalan R, Kirtiman Singh, Neetesh Kumar and Ghosh, A.K., 2019. Longitudinal and lateral directional aerodynamic characterization of reflex wing UAV from flight tests using ML, LS and NGN methods. The Aeronautical Journal, 123 (1269), 1807-1839.
Gwang-gyo Seo , Yoonsoo Kim, S. Saderla, 2019. Kalman-filter based online system identification of fixed-wing aircraft in upset condition. Aerospace Science and Technology, 89, 307-317.
-
S. Saderla, Yoonsoo Kim, A K Ghosh, 2018. Online system Identification of mini cropped delta UAVs using flight test methods. Aerospace Science and Technology, 80, 337-353.
-
S. Saderla, Rajaram, D., Ghosh, A., 2018. Lateral directional parameter estimation of a miniature unmanned aerial vehicle using maximum likelihood and Neural Gauss-Newton methods. The Aeronautical Journal, 122 (1252), 889-912.
-
Dhayalan R., S. Saderla, Ajoy Kanti Ghosh, 2018. Parameter estimation of UAV from flight data using neural network. Aircraft Engineering and Aerospace Technology, 90 (Issue 2), 302-311.
-
S. Saderla, Dhayalan, R., Ghosh, A., 2017. Non-linear aerodynamic modelling of unmanned cropped delta configuration from experimental data. The Aeronautical Journal, 121 (1237), 320-340.
-
S. Saderla, Rajaram, Dhayalan, Ghosh, A K, 2017. Parameter Estimation of Unmanned Flight Vehicle Using Wind Tunnel Testing and Real Flight Data. Journal of Aerospace Engineering (ASCE), 30 (1), 04016078.
-
S. Saderla, R. Dhayalan, A. K. Ghosh, 2017. Parameter estimation from near stall flight data using conventional and neural-based methods. Defense Science Journal, 67 (1), 03-11.
-
S. Saderla, R. Dhayalan, A. K. Ghosh, , "Aerodynamic parameter estimation using neuro-fuzzy model based method," 2017 First International Conference on Recent Advances in Aerospace Engineering (ICRAAE), Coimbatore, India, 2017, pp. 1-5, doi: 10.1109/ICRAAE.2017.8297220
-
S. Saderla, Rajaram, Dhayalan, Ghosh, A K, 2016. Longitudinal parameter estimation from real flight data of unmanned cropped delta flat plate configuration. International Journal of Intelligent Unmanned Systems, 4(1), 2-22.
People
List of current students/staff
Ph.D. (On-going)
Neetesh Kumar
2018
“Real-time System Identification for Reconfigurable Control of Marginally Stable High-speed Aircraft.”
Gulivindala Kishore
2020
“Fault Detection, Isolation, and Reconfiguration Methods for UAV”
Sagar Ghosal
2023
“NA”
M.Tech. (On-going)
Surya M
2022 - 2024 Batch
"Terminal guidance of Fixed wing unmanned aerial vehicle in Real time estimation"
Sonam Chorol
2022 - 2024 Batch
"System Identification with software-in-loop simulation using gain tuning in PX4 algorithm for non-linear flight envelope."
Mohammad Sadeeq Shah
2022 - 2024 Batch
"Design optimisation of VTOL UAV."
Abhishek M
2023 - 2025 Batch
"NA"
Vamshi Krishna R
2023 - 2025 Batch
"NA"
M.Tech. (Completed)
Pokar Monil
2019
Design Optimization of UAV Propellers for Hover Performance Using Particle Swarm Optimization.
Gaurav Kumar
2020
Attitude Stabilization and Command Tracking of a Delta Wing UAV using Adaptive Sliding Mode Control.
Tadesse Yohannes
2021
Design of Autopilot for Delta Wing UAVs.
Samuel Jenkins Paul J
2022
Controller in Loop System Identification of an Unstable Combat UAV.
Aishwarya Rani
2023
Dynamics and Control of Canard Guided Artillery Shell Projectile.
Alvin Sebastian
2023
Modelling, Simulation, and Control of Active Side Stick in Modern Combat Aircraft.
Shivam Goswami
2023
System identification with software-in-loop simulation using gain tuning in PX4 algorithm.
Challa Sai Kumar
2023
Implementation of Formation Control for a manoeuvring Swarm of Fixed-Wing UAVs.
Omkar Babasaheb Rajmane
2021 - 2023 Batch
"Obstacle detection and avoidance for a fixed wing unmanned aerial vehicle using machine learning."
M. Shiva Teja Reddy
2021 - 2023 Batch
"Real Time power-plant fault identification of an electrically powered UAV"
Lab Members
Ashish Kumar
UAV Lab
Project Associate
C. Bhushan Vishwakarma
UAV Lab
Project Associate
Jaya Suriya K
UAV Lab
Pilot
Ven Leonin K
UAV Lab
Intern
Rishi Pandya R
UAV Lab
Intern
Vishal Verma
UAV Lab
Technical Assistant
Laxmi Kant
UAV Lab
Technical Assistant
Shivam
UAV Lab
Technical Assistant
Abhishek
UAV Lab
Technical Assistant
Swati
UAV Lab
Receptionist
Projects
On-going and completed projects
On-going Projects
Real-time Flight Vehicles Distress Management using Online System Identification
Agency: Science and Engineering Research Board (SERB)
Reconfigurable control of fixed wing high speed unmanned aerial vehicles
Agency: Science and Engineering Research Board (SERB)
UAV Laboratory
Agency: IIT Kanpur
Payload dropping drones for defence applications.
Agency: Uttar Pradesh Defence Corridor
Completed Projects
Miniature pneumatic recoil management mechanism for micro-UAV
Agency: DRDO Young Scientist Laboratory (DYSL-AT)
Design optimization, prototype development and wind tunnel testing of a foldable Tandem wing UAV
Agency: Asymmetric Technologies, DRDO
Development of Crowd Monitoring Solution Using Aerostat
Agency: Govt. of UP and IITK
Development of Solar and VTOL Air Taxi
Agency: VTOL Aviation India Ltd.
Unmanned Aircraft Vehicles
Agency: Uttar Pradesh Expressways Industrial Development Authority
Flight Demonstration and Flight Data Collection For Latest Ghatak Configuration Irc 2.3 Rd
Agency: Aeronautical Development Agency (ADA)
Design, Development, and testing of Tandem Wing
Agency: DRDO Young Scientist Laboratory (DYSL-AT)
Design, Development, and testing of Aerostat
Agency: Uttar Pradesh Defence Corridor
Analytical Study Of A Supercavitating Projectile Including Stability Analysis In Different Mediums
Agency: Navel Science and Technological Laboratory (NSTL), DRDO
Modification of Conventional Artillery Rocket to A Guided Rocket With Freely Spinning Tail
Agency: ARMAMENT RESEARCH BOARD
Autonomous Flight Test of a Low RCS Aircraft Configuration with Ducted Fan for Multiple Flight Modes
Agency: Aeronautical Development Agency (ADA)
Prototype Development of Cloud Seeding Equipment
Agency: IITK and Govt. of UP
Indigenous UAV Developments
Agency: Larsen and Toubro Limited
Initiation Research Grant for System Identification
Agency: IIT Kanpur
Contact
Location:
UAV Laboratory, Department of Aerospace Engineering, IIT Kanpur, IN, 208016