Agnes Steinert

Dr. Agnes Steinert serves as Deputy Head of the Institute of Flight System Dynamics at the Technical University of Munich (TUM), where she holds the rank of Professor. Her work centers on advancing aerospace control systems through theoretical innovation and practical implementation in flight vehicles.

Her research spans Flight Control, Flight Guidance, Nonlinear and Adaptive Control, Trajectory Optimization, Navigation Systems, and Flight Safety. She pioneers Incremental Nonlinear Dynamic Inversion (INDI) methodologies for robust aircraft control, with recent focus on electric vertical take-off and landing (eVTOL) systems, trajectory generation under dynamic constraints, and sensor-actuator synchronization challenges.

Analysis of her 15 most recent publications (2022-2025) reveals a consistent trajectory toward safety-critical autonomous flight systems. Key themes include real-time trajectory optimization for eVTOLs, stability analysis of nonlinear controllers with actuator dynamics, and robustness enhancement through multiobjective parameter tuning—bridging theoretical control frameworks with aerospace operational requirements.

No scientific awards were documented in the provided materials.

Dr. Steinert actively mentors graduate researchers, having supervised over 20 theses covering airship/hydrofoil control, flight envelope protection, and adaptive controller design. Her leadership extends to experimental validation through TUM's flight test infrastructure, including collaborations on electric aircraft autonomy projects.

The Institute of Flight System Dynamics maintains comprehensive research facilities including manned/unmanned aircraft, flight simulators, and GNC subsystems. Current infrastructure supports experimental work on trajectory optimization, sensor fusion, and safety-critical flight control validation for next-generation aviation systems.