Contact

Stefan Raab
M. Sc.
E-mail:stefan.raab@tum.de

Publications

R. Steffensen​, A. C. Steinert, Z. Mbikayi, S. Raab, J. Angelov, F. Holzapfel, "Filter and sensor delay synchronization in incremental flight control laws", Aerospace Systems, vol. 6, 2023. [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, 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

R. Eckfeld, "Robust Flight Control of an Over-Actuated eVTOL", Thesis, Technische Universität München, Garching, 2022.
T. Rupprecht, "Command Generation and Control of a Fly-By-Wire Equipped Helicopter Using Incremental Nonlinear Dynamic Inversion", Thesis, Technische Universität München, Garching, 2021.
S. Kellringer, "Functional Runtime Monitoring of Adaptive Controllers", Thesis, Technische Universität München, Garching, 2021.
J. Bachler, "Incremental Dynamic Inversion Control for a Fly-By-Wire EC135 Helicopter", Thesis, Technische Universität München, Garching, 2021.
S. Rieger, "Rate Based Control of Control Effectors", Thesis, Technische Universität München, Garching, 2020.
T. Lausenhammer, "Design of a Nonlinear Flight Control System for a Guided Research Missile", Thesis, Technische Universität München, Garching, 2020.
J. Holfelner, "Development of a Flight controller for an Ultralight Helicopter", Thesis, Technische Universität München, Garching, 2020.
J. Bachler, "Comparison of Nominal and Incremental Dynamic Inversion for Helicopter Flight Control", Thesis, Technische Universität München, Garching, 2020.
N. Michel, "Incremental Nonlinear Dynamic Inversion of the Longitudinal Dynamics of a Transition Vehicle Including Nonlinear Coupling Effects", Thesis, Technische Universität München, Garching, 2019.
C. Ibel, "Control Effector Identification for the Control of a Tricopter Using Incremental Nonlinear Dynamic Inversion", Thesis, Technische Universität München, Garching, 2019.
M. Söpper, "Model Filtering for an INDI Controlled UAV", Thesis, Technische Universität München, Garching, 2018.
B. Hab, "Comparative Analysis and Application within INDI Control of a Tricopter Airframe", Thesis, Technische Universität München, Garching, 2018.