1–20 von 22 Ergebnissen
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    Optimal Input Design for Flight Vehicle System Identification in Frequency Domain

    Hosseini, Seyedbarzin / Holzapfel, Florian | AIAA | 2022

    Optimal Input Design for Flight Vehicle System Identification in Frequency Domain

    Hosseini, Seyedbarzin / Holzapfel, Florian | TIBKAT | 2022

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

    Bachfischer, Michael / Hosseini, Seyedbarzin / Holzapfel, Florian | AIAA | 2022

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

    Bachfischer, Michael / Hosseini, Seyedbarzin / Holzapfel, Florian | TIBKAT | 2022

    Flight-Test Plan Design and Evaluation in a Closed-Loop Framework for a General Aviation Aircraft

    Hofmann, Rodolfo / Hosseini, Seyedbarzin / Holzapfel, Florian | TIBKAT | 2022

    Flight-Test Plan Design and Evaluation in a Closed-Loop Framework for a General Aviation Aircraft

    Hofmann, Rodolfo / Hosseini, Seyedbarzin / Holzapfel, Florian | AIAA | 2022

    Robust optimal input design for flight vehicle system identification

    Hosseini, Seyedbarzin / Botkin, Nikolai / Diepolder, Johannes et al. | AIAA | 2020

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

    Ashok, Shreyas G. / Hosseini, Seyedbarzin / Rauleder, Juergen | AIAA | 2024

    Excitation Monitoring for Online Parameter Estimation

    Hafner, Simon F. / Hosseini, Seyedbarzin / Holzapfel, Florian | AIAA | 2023

    Excitation Monitoring for Online Parameter Estimation

    Hafner, Simon F. / Hosseini, Seyedbarzin / Holzapfel, Florian | TIBKAT | 2023

    Helicopter Parameter Estimation Based on A Nonlinear Physics-Based Model

    Hosseini, Seyedbarzin / Barth, Aaron / Hajek, Manfred et al. | AIAA | 2021

    Flight Path Reconstruction for a Coaxial Helicopter Equipped with Rotational Accelerometers

    Hofmann, Rodolfo / Hosseini, Seyedbarzin / Fang, Xiang et al. | AIAA | 2023

    HELICOPTER PARAMETER ESTIMATION BASED ON A NONLINEAR PHYSICS-BASED MODEL

    Hosseini, Seyedbarzin / Barth, Aaron / Hajek, Manfred et al. | TIBKAT | 2021

    ROBUST OPTIMAL INPUT DESIGN FOR FLIGHT VEHICLE SYSTEM IDENTIFICATION

    Hosseini, Seyedbarzin / Botkin, Nikolai / Diepolder, Johannes et al. | TIBKAT | 2020

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

    Hosseini, Seyedbarzin / Mbikayi, Zoe / Bachfischer, Michael et al. | AIAA | 2024

    On the Flight Test Campaign of a Coaxial Helicopter for the Development of an Unmanned Aerial System

    Maier, Lukas / Hosseini, Seyedbarzin / Barth, Aaron et al. | AIAA | 2022

    On the Flight Test Campaign of a Coaxial Helicopter for the Development of an Unmanned Aerial System

    Maier, Lukas / Hosseini, Seyedbarzin / Barth, Aaron et al. | TIBKAT | 2022

    Linear Model Identification for a Coaxial Rotorcraft in Hover

    Bachfischer, Michael / Hosseini, Seyedbarzin / Sax, Franz et al. | AIAA | 2024

    Evaluation of the Pilot Training Concept for Flying a Helicopter UAV

    Maier, Lukas / Hosseini, Seyedbarzin / Sax, Franz et al. | AIAA | 2024