All Stories

  1. Linear Model Identification for a Coaxial Rotorcraft in Hover

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

    Lukas Maier, Seyedbarzin Hosseini

  2. 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

  3. Conversion of a Coaxial Rotorcraft to a UAV

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

    Seyedbarzin Hosseini, Hannes Hofsaess, Lukas Maier

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

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

    Seyedbarzin Hosseini

  5. Center of Gravity Estimation Using Multiple Accelerometers

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

    Seyedbarzin Hosseini, Xiang Fang, Lukas Maier

  6. 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

  7. 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

  8. 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

  9. 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

  10. 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

  11. 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