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Contact

Niclas Bähr
M.Sc.
Institute of Flight System Dynamics
Technische Universität München
Boltzmannstr. 15
85748 Garching bei München
Germany
Room:MW3601 (floor plan)
Phone:+49 89 289 16034
Fax:+49 89 289 16058
E-mail:niclas.baehr@tum.de

Research Interests

  • Fligth Physics
  • eVTOL Modeling and Simulation
  • Uncertainty Modeling, Quantification and Propagation

Teaching

  • UAV Lab

Publications

[5] M. Söpper, J. Zhang, N. Bähr, F. Holzapfel, "Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models", MDPI Applied Sciences, vol. 11, no. 8, 2021. [doi]
[4] C. Mishra, F. Schwaiger, N. Bähr, F. Sax, M. A. Kleser, P. Nagarajan, F. Holzapfel, "Efficient Verification and Validation of Performance-Based Safety Requirements using Subset Simulation", in AIAA SciTech 2021 Forum. [doi]
[3] N. Bähr, M. Söpper and F. Holzapfel, "Stochastic Lookup Tables - A Method for the Integration of Parametric Uncertainties in Non-Linear Simulation Models", in AIAA SciTech 2021 Forum. [doi]
[2] N. Bähr, "Modeling of the Rotor Blade Flapping Motion of a Transition Aircraft​", Thesis, Technische Universität München, Garching, 2018.
[1] N. Bähr, "Controlled Flight Into Terrain Analyses In Flight Data Monitoring", Thesis, Technische Universität München, Garching, 2017.

Supervised Student Work

[10] Y. Jamanka, "Development of a battery-hydrogen hybrid powertrain system architecture for a novel short take-off and landing aircraft", Thesis, Technische Universität München, Garching, 2022.
[9] O. M. Gonzalez Mota, "Modeling of a Proton-Exchange Membrane Fuel Cell and its Auxiliary Components", Thesis, Technische Universität München, Garching, 2022.
[8] O. M. Gonzalez Mota, "Modeling of a Proton-Exchange Membrane Fuel Cell and its Auxiliary Components", Thesis, Technische Universität München, Garching, 2022.
[7] K. Buck, "Entwicklung eines Hochauftriebssystems für neuartige Flugsysteme mit Kurzstart- und Kurzlandeeigenschaften", Thesis, Technische Universität München, Garching, 2022.
[6] G. Biechel, "Distributed Electric Propulsion - Low Parametric Models for Blown Flaps and Wingtip Propellers", Thesis, Technische Universität München, Garching, 2022.
[5] H. Gartner, "Development of a Tool for Mission-Based Design and Optimization of an eVTOL UAV", Thesis, Technische Universität München, Garching, 2021.
[4] J. Schüürmann, "Automatic Evaluation of Basic Flight Dynamic Parameters from Non-Linear Simulation Models", Thesis, Technische Universität München, Garching, 2020.
[3] T. Coulon, "Implementation of a Rotor Model with Dynamic Inflow in MATLAB/Simulink", Thesis, Technische Universität München, Garching, 2020.
[2] K. P. Rajput, "Modeling and Investigation of the Airframe Influence on the Rotor Dynamics of Transition Aircraft", Thesis, Technische Universität München, Garching, 2019.
[1] R. Karpstein, "Assessment of a novel Flight Propulsion Unit for VTOL applications based on a preliminary aircraft design", Thesis, Technische Universität München, Garching, 2019.