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Contact

Tuğba Akman
M.Sc.
Institute of Flight System Dynamics
Technische Universität München
Boltzmannstr. 15
85748 Garching bei München
Germany
Room:MW3617 (floor plan)
Phone:+49 89 289 16056
Fax:+49 89 289 16058
E-mail:tugba.akman@tum.de

Publications

C. Krammer, F. Schweighofer, D. Gierszewski, S. Scherer, T. Akman, H. Hong, F. Holzapfel, "Requirements-based Generation of Optimal Vertical Takeoff and Landing Trajectories for Electric Aircraft", in 33rd Congress of the International Council of the Aeronautical Sciences (ICAS), 2022.
T. Akman, S. Hosseini, J. Diepolder, B. Grüter, R. J. M. Afonso, M. Gerdts, F. Holzapfel, "Efficient Sensitivity Calculation for Robust Optimal Control​", in DGLR, Deutscher Luft- und Raumfahrtkongress, 2020. [doi]
F. Teschner, T. Akman, C. Mundt, F. Holzapfel, "Aerodynamic and Trajectory Studies on Optimal Earth Reentry of a Capsule", in International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions and Engineering, 2019.
B. Grüter, J. Diepolder, P. Piprek, T. Akman, F. Holzapfel, "NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING", in ICAS 31st Congress of the International Council of the Aeronautical Science, 2018.
T. Akman, J. Diepolder, B. Grüter, F. Holzapfel, "Using Sensitivity Penalties to Robustify the Optimal Reentry Trajectory of a Hypersonic Vehicle", in ICAS 31st Congress of the International Council of the Aeronautical Science, 2018.
B. Grüter, J. Diepolder, T. Akman, F. Holzapfel, "Integrated Bi-level Arrival and Departure Time Assignment for Optimal Trajectories", in ENRI Int. Workshop on ATM/CNS 2017 (EIWAC 2017).
J. Diepolder, P. Piprek, B. Grüter, T. Akman, F. Holzapfel, "Aircraft Safety Analysis using Generalized Polynomial Chaos", in ENRI Int. Workshop on ATM/CNS 2017 (EIWAC 2017).
J. Diepolder, C. Göttlicher, B. Grüter, T. Akman, F. Holzapfel, J. Z. Ben-Asher, "Optimal Control Based Flight Control Law Testing with Parameter Uncertainties", in IEEE Conference on Control Technology and Applications (CCTA), 2017.

Supervised Student Theses

F. Höhne, "Numerical Optimization of Combined Ascent and Landing Trajectories for a Reusable Orbital Launch Vehicle", Thesis, Technische Universität München, Garching, 2022.
M. Bischoff, "Numerical Trajectory Optimization for Airborne Wind Energy Systems with Passively Moving Ground Stations", Thesis, Technische Universität München, Garching, 2021.
F. Bayer, "Analysis of Orbital Launcher Guidance Schemes based on Optimal Ascent Trajectories", Thesis, Technische Universität München, Garching, 2021.
N. Schlautmann, "Maneuver Optimization for Transition-UAV​", Thesis, Technische Universität München, Garching, 2020.
K. Najorka, "Berechnung des Wärmeminimalen Wiedereintritts der HL-20 durch Optimale Steuerung", Thesis, Technische Universität München, Garching, 2019.
F. Höhne, "Development of a Simulation Framework for a Generic Exoatmospheric Kinetic Energy Effector​", Thesis, Technische Universität München, Garching, 2019.