Optimal Input Design for Flight Vehicle System Identification in Frequency Domain

von Hosseini, Seyedbarzin
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Atmospheric flight mechanics ; Volume 2 of 2 (2022)

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

von Bachfischer, Michael
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Applied aerodynamics ; Volume 3 of 4 (2022)

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

von Hofmann, Rodolfo
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Atmospheric flight mechanics ; Volume 2 of 2 (2022)

Excitation Monitoring for Online Parameter Estimation

von Hafner, Simon F.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Atmospheric flight mechanics ; Volume 1 of 2 (2023)

ROBUST OPTIMAL INPUT DESIGN FOR FLIGHT VEHICLE SYSTEM IDENTIFICATION

von Hosseini, Seyedbarzin
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 1 of 2 (2020)

HELICOPTER PARAMETER ESTIMATION BASED ON A NONLINEAR PHYSICS-BASED MODEL

von Hosseini, Seyedbarzin
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Atmospheric flight mechanics ; Volume 2 of 2 (2021)

Flight Path Reconstruction for a Coaxial Helicopter Equipped with Rotational Accelerometers

von Hofmann, Rodolfo
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Flight testing (2023)

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

von Maier, Lukas
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Flight testing (2022)