ACT/FHS EC135 System Identification Data at Hover and 60 knots forward flight - Sweeps and Multistep Responses -

Kurzfassung

This document summarizes flight test data of the ACT/FHS at hover and 60 knots forward flight. Sweeps may be used for parameter identification, modeling, and validation in the frequency domain. Multistep inputs may be used to validate the model in the time domain. These flight test data are a subset of the overall ACT/FHS EC135 system identification data and is shared through the NATO AVT-RTG 296 on Rotorcraft Flight Simulation Model Fidelity Improvement and Assessment (2018-2020).