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Institute of Flight System Dynamics

Master’s Thesis: Flight Control Law Development and Testing for a Tilt-Wing eVTOL UAV

Master’s Thesis: Flight Control Law Development and Testing for a Tilt-Wing eVTOL UAV

Posted on 25. November 202525. November 2025 by Chinmaya Mishra

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  • Home
  • News
  • Team
    • Floor Plan / Facilities
    • Alumni
  • Teaching
  • Research
    • Flight Guidance and Flight Control
      • Application Driven Flight Control
      • Manned and Robust Flight Control
      • Nonlinear and Adaptive Flight Control
    • Simulation, Parameter Identification and Flight Safety
    • Trajectory Optimization
    • Sensors, Navigation and Data Fusion
      • Geodesy
      • Inertial Navigation
      • Satellite Navigation
      • Navigation Systems
      • Data Fusion
      • Navigation Aids
    • Avionics and Safety Critical Systems
  • Infrastructure
    • Research Airplanes
    • Unmanned Systems
    • Flight Simulators
    • GNC Subsystems
    • HORYZN
  • Software
    • FALCON.m
    • Simulink® – Polarion® Connector SimPol
    • Counter Optimization Library (colibry)
    • GeoRiskNavigator QGIS Plugin
    • Test Interaction Console (tico)
    • Subset Simulation Toolbox
    • Simulation Accelerator Toolbox
  • Student Theses & HiWi
  • Job Postings
  • Forum Munich Aerospace
  • Contact
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