6 Degrees of Freedom Flight Simulator for Engineering Studies

Authors

  • Víctor Caballini Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Daniel Monserrat Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Ezequiel Crotti Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Rubén Minutella Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Eladio Fernández Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Alexis Álvarez Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina
  • Gerardo Godoy Universidad Tecnológica Nacional - Facultad Regional Haedo - Argentina

Keywords:

Simulation, Aircraft, Flight, Control

Abstract

This paper presents the main characteristics of the six degrees of freedom (6DOF) flight simulator for aeronautical engineering studies developed by the Flight Dynamics Simulation Group (GSDV) at the Flight Simulation and Control Laboratory (LSCV) of the Universidad Tecnológica Nacional, Facultad Regional Haedo. The main objectives of the simulator are to serve as a research tool to characterize models and flight qualities of the aircraft that students design during their career and to serve as a training or study platform for crews, professorships, etc. For this reason, the simulator has a generic and configurable cabin. The software that guides the different components has been specified and developed within the LSCV. The force feedback system is one of the distinctive features of the simulator and has also been developed by the GSDV. The force system, the cockpit instruments and the external scene are distributed and controlled by several computers interconnected in a network. The modules are presented here, their advantages and disadvantages. The force feedback model is particularly important for the purposes of this flight simulator. To obtain greater realism in the efforts in the controls, special care has been taken to implement hinge moment equations in the simulation software. The result is a reliable closed-loop force feedback system on all aircraft commands.

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Published

2024-04-18

How to Cite

Caballini, V., Monserrat, D., Crotti, E., Minutella, R., Fernández, E., Álvarez, A., & Godoy, G. (2024). 6 Degrees of Freedom Flight Simulator for Engineering Studies. AJEA (Proceedings of UTN Academic Conferences and Events), (AJEA 34). Retrieved from https://rtyc.utn.edu.ar/index.php/ajea/article/view/1375

Conference Proceedings Volume

Section

Proceedings - Simulation