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Contact

Pranav Bhardwaj
M. Sc.
Institute of Flight System Dynamics
Technische Universität München
Boltzmannstr. 15
85748 Garching bei München
Germany
Room:MW3609 (floor plan)
Phone:+49 89 289 16113
Fax:+49 89 289 16058
E-mail:pranav.bhardwaj@tum.de

Publications

P. Panchal, S. Myschik, K. Dmitriev, P. Bhardwaj, F. Holzapfel, "Handling Complex System Architectures with a DO-178C/DO-331 Process-Oriented Build Tool", in 2022 IEEE/AIAA 41st Digital Avionics Systems Conference (DASC). [doi]
P. Piprek, M. M. Marb, P. Bhardwaj, F. Holzapfel, "Trajectory/Path-Following Controller Based on Nonlinear Jerk-Level Error Dynamics", Applied Sciences, vol. 10, no. 23, 2020, pp. 8760. [pdf] [doi]
J. Zhang, P. Bhardwaj, S. Raab, F. Holzapfel, "Control Allocation Framework with SVD-based Protection for a Tilt-rotor VTOL Transition Air Vehicle", in AIAA Aviation 2019 Forum. [doi]
S. Raab, J. Zhang, P. Bhardwaj, F. Holzapfel, "Consideration of Control Effector Dynamics and Saturations in an Extended INDI Approach", in AIAA Aviation 2019 Forum. [doi]
P. Bhardwaj, V. S. Akkinapalli, J. Zhang, S. Saboo, F. Holzapfel, "Adaptive Augmentation of Incremental Nonlinear Dynamic Inversion Controller for an Extended F-16 Model", in AIAA Scitech 2019 Forum.
P. Bhardwaj, S. Raab, J. Zhang, F. Holzapfel, "​​​Thrust command based Integrated Reference Model with Envelope Protections for Tilt-rotor VTOL Transition UAV", in AIAA Aviation 2019 Forum. [doi]
J. Zhang, P. Bhardwaj, S. Raab, S. Saboo, F. Holzapfel, "Control Allocation Framework for a Tilt-rotor Vertical Take-off and Landing Transition Aircraft Configuration", in 2018 AIAA Applied Aerodynamics Conference. [doi]
S. Raab, J. Zhang, P. Bhardwaj, F. Holzapfel, "Proposal of a Unified Control Strategy for Vertical Take-off and Landing Transition Aircraft Configurations​", in 2018 AIAA Applied Aerodynamics Conference. [doi]
P. Bhardwaj, S. Raab, J. Zhang, F. Holzapfel, "Integrated Reference Model for a Tilt-rotor Vertical Takeoff and Landing Transition UAV", in AIAA AVIATION 2018. [doi]
J. Diepolder, S. Saboo, V. S. Akkinapalli, S. Raab, J. Zhang, P. Bhardwaj, M. Krenmayr, B. Grüter, F. Holzapfel, "Flight Control Law Testing using Optimal Control and Postoptimal Sensitivity Analysis", in CEAS EuroGNC, 2017.

Supervised Student Theses

A. Ramesh, "Augmentation of an Incremental Non-Linear Dynamic Inversion Controller with a Modified Linear Extended State Observer", Thesis, Technische Universität München, Garching, 2021.
C. Racke, "Generation of Required Control Phase Planes from Desired Response Models​", Thesis, Technische Universität München, Garching, 2021.
P. J. Müller, "Adaptive Higher Order Reference Models for Extended Incremental Nonlinear Dynamic Inversion​", Thesis, Technische Universität München, Garching, 2021.
M. Marb, "Development and Testing of a Path-Following Controller Employing Full Nonlinear Kinematics Based on Jerk-Level Dynamics", Thesis, Technische Universität München, Garching, 2020.
V. Meidinger, "Model-in-the-Loop Based Requirement Evaluation of an eVTOL Aircraft​", Thesis, Technische Universität München, Garching, 2018.