PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
Article 2018

Characteristic helicopter flight mechanics and motion cueing integration into the sivor robotic flight simulator: An objective approach

Authors

Hidalgo, Diego F.
Rodamilans, Guilherme B.

31st Congress of the International Council of the Aeronautical Sciences Icas 2018

2
Citations
3
Authors

Abstract

© 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. All rights reserved.The following paper will depict the process followed to build a baseline motion cueing setting specific for VTOL and helicopter applications for the SIVOR flight simulator at ITA. This effort is built around three elements: a pilot model, an identified model of the robotic platform and a set of surrogate flight dynamic models representative of helicopter motion. Initially, a description of the platform and simulation environment is presented, followed by the tuning strategy based on numerical optimization and a test case which will serve as a validation for the optimization strategy. A brief description of the SIVOR system identification process is presented along with the structural-pilot-model used to explore a set of three main manoeuvres which are used for washout filter tuning. Optimization results included in the test maneuvers show good agreement with published experimental observations.

Keywords

Flight Simulation Robotics Motion Cueing

Electrical and Electronic Engineering (ENGI) Control and Systems Engineering (ENGI) Materials Science (all) (MATE) Aerospace Engineering (ENGI)
: Scopus
Last Update: 2026-06-25
: 2-s2.0-85060463480