Proposal of Hardware-in-the-loop control platform for small fixed-wing UAVs

被引：0

作者：

Abdulhamid, Rauhe ^{[1
]}

de Oliveira, Neusa M. F. ^{[1
]}

d'Amore, Roberto ^{[1
]}

机构：

[1] Inst Tecnol Aeronaut, Dept Engn Eletron & Comp, Sao Jose Dos Campos, SP, Brazil

来源：

2016 ANNUAL IEEE SYSTEMS CONFERENCE (SYSCON) | 2016年

关键词：

Hardware-In-the-Loop systems; UAVs; Measurement of airplane control deflections;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Unmanned Aerial Vehicles (UAVs) have received considerable attention from the academic community and technology solutions companies, given their civilian and military applications. The autopilot system shall be thoroughly tested in lab because an accident may cause irreversible damage to the UAV. This article presents a proposal of a Hardware-In-the-Loop platform for testing and validation of a small fixed-wing aircraft. Besides a communication system, it was developed a deflection measurement platform of the aircraft control surfaces. This measurement platform was validated, enabling future work on implementing embedded control algorithms.

引用

页码：808 / 813

页数：6

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