Contact

Stefan Raab
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 16162
Fax:+49 89 289 16058
E-mail:stefan.raab@tum.de

Publications

[7] 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]
[6] 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]
[5] 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]
[4] 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]
[3] 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]
[2] 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]
[1] 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

[7] T. Lausenhammer, "Design of a Nonlinear Flight Control System for a Guided Research Missile", Thesis, Technische Universität München, Garching, 2020.
[6] J. Holfelner, "Development of a Flight controller for an Ultralight Helicopter", Thesis, Technische Universität München, Garching, 2020.
[5] J. Bachler, "Comparison of Nominal and Incremental Dynamic Inversion for Helicopter Flight Control", Thesis, Technische Universität München, Garching, 2020.
[4] N. Michel, "Incremental Nonlinear Dynamic Inversion of the Longitudinal Dynamics of a Transition Vehicle Including Nonlinear Coupling Effects​", Thesis, Technische Universität München, Garching, 2019.
[3] C. Ibel, "Control Effector Identification for the Control of a Tricopter Using Incremental Nonlinear Dynamic Inversion", Thesis, Technische Universität München, Garching, 2019.
[2] M. Söpper, "Model Filtering for an INDI Controlled UAV", Thesis, Technische Universität München, Garching, 2018.
[1] B. Hab, "Comparative Analysis and Application within INDI Control of a Tricopter Airframe", Thesis, Technische Universität München, Garching, 2018.