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COBEM 2017
24th ABCM International Congress of Mechanical Engineering
HIL system with 3-axis Gimbal for UAV’s autopilot tests
Submission Author:
Diogo Costa , DF
Co-Authors:
Neusa Maria Franco Oliveira, Roberto d'Amore, Diogo Costa
Presenter: Diogo Costa
doi://10.26678/ABCM.COBEM2017.COB17-2229
Abstract
This paper describes the development of a system to speed up UAV's Autopilot development in general, and specifically test inertial measurement unit (IMU). The system is composed of a three axis Gimbal, controlled by an embedded control board. To realize the communication between the simulated aircraft and the Gimbal control board it was developed data conversion software. Results acquired with the Gimbal being automatically positioned with the simulated aircraft attitude is presented.
Keywords
unmanned aircraft systems, Hardware-in-the-Loop, airspace control
