All Stories

  1. Global Model Identification for a General Aviation Aircraft

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  2. Parameter Estimation of a Multi-Point Aerodynamic Model Based on Flight Data

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  3. Automated Maneuver Injection for General Aviation Aircraft for System Identification - Lessons Learned

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  4. Optimal Input Design for Aircraft Parameter Estimation - Flight Test Results

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  5. Linear Model Identification for a Coaxial Rotorcraft in Hover

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Lukas Maier, Seyedbarzin Hosseini

  6. Real-Time Dynamic Inflow Model for a Coaxial Helicopter Configuration Using the Lattice–Boltzmann Method

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  7. Conversion of a Coaxial Rotorcraft to a UAV

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini, Hannes Hofsaess, Lukas Maier

  8. Simulation, Flight Dynamics, and Control Design for a Coaxial Rotorcraft

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  9. Center of Gravity Estimation Using Multiple Accelerometers

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini, Xiang Fang, Lukas Maier

  10. Evaluation of the Pilot Training Concept for Flying a Helicopter UAV

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Lukas Maier, Seyedbarzin Hosseini, Prof. Manfred Hajek

  11. Advancements in the Theory and Practice of Flight Vehicle System Identification

    Article • Journal of Aircraft, July 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  12. Development and Validation of an Inflow Model for a Coaxial Teetering Rotor System

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini

  13. Flight Test Campaign for Unmanned Coaxial Helicopter Development

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini, Prof. Manfred Hajek, Lukas Maier

  14. Helicopter Parameter Estimation Based on A Nonlinear Physics-Based Model

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini, Prof. Manfred Hajek

  15. Optimal input design for flight vehicle system identification via dynamic programming and the direct method for optimal control

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Seyedbarzin Hosseini