Design of Tracked Model Vehicle Measurement and Control System Based on VeriStand and Simulink

Chang, Hao; Wu, Dafang; Wei, Hui; Zhang, Qi; Dong, GuangLi

doi:10.1051/matecconf/201817503047

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Hil Simulation Platform1

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2019

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“…The set of 12 equations of motion derived in Section 3 have been particularised for the prototype model and implemented in Matlab/Simulink. Simulink allows to compile the model to be run on the PXI real-time target [34,35].…”

Section: Hil Simulation Platformmentioning

confidence: 99%

Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV

et al. 2019

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This paper gathers the design and implementation of the control system that allows an unmanned Flying-wing to perform a Vertical Take-Off and Landing (VTOL) maneuver using two tilting rotors (Bi-Rotor). Unmanned Aerial Vehicles (UAVs) operating in this configuration are also categorized as Hybrid UAVs due to their ability of having a dual flight envelope: hovering like a multi-rotor and cruising like a traditional fixed-wing, providing the opportunity of facing complex missions in which these two different dynamics are required. This work exhibits the Bi-Rotor nonlinear dynamics, the attitude tracking controller design and also, the results obtained through Hardware-In-the-Loop (HIL) simulation and experimental studies that ensure the controller’s efficiency in hovering operation.

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Section: Hil Simulation Platformmentioning

confidence: 99%