Drones 2017, 1(1), 3; https://doi.org/10.3390/drones1010003
Hardware Design of a Small UAS Helicopter for Remote Sensing Operations
Pablo Royo 1,*
, Enric Pastor 1
, Cristina Barrado 1, Raul Cuadrado 1, Felix Barrao 2 and Antonio Garcia 2
, Cristina Barrado 1, Raul Cuadrado 1, Felix Barrao 2 and Antonio Garcia 21
Department of Computer Science, Polytechnic University of Catalonia, Castelldefels, 08860 Barcelona, Spain
2
MAGline Composites y Sistemas SL, 50197 Zaragoza, Spain
*
Author to whom correspondence should be addressed.
Received: 21 July 2017 / Revised: 30 August 2017 / Accepted: 31 August 2017 / Published: 10 September 2017
Abstract
This paper presents the hardware design and integration process employed to develop an Unmanned Aircraft System (UAS) helicopter. The design process evolves from the bare airframe (without any electronics), to become a complete and advanced UAS platform for remote sensing applications. The improvements, design decisions and justifications are described throughout the paper. Two airframes have been used during the design and integration process: the AF25B model and the more advanced AF30 model, from the Copterworks company. The airframe engine reliability and fuel economy have been improved by adding an Electronic Fuel Injection (EFI) and Capacitor Discharge Ignition (CDI), both managed by an Engine Control Unit (ECU). On-board power supply generation and regulation have also been designed and validated. Finally, the integration process incorporates on-board mission computation to improve the concept of operation in remote sensing applications. Several flight tests have been performed to verify the reliability of the whole system. The flight test results demonstrate the correct process of integration and the feasibility of the UAS. View Full-TextKeywords:
UAS; design helicopter; remote sensing
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MDPI and ACS Style
Royo, P.; Pastor, E.; Barrado, C.; Cuadrado, R.; Barrao, F.; Garcia, A. Hardware Design of a Small UAS Helicopter for Remote Sensing Operations. Drones 2017, 1, 3.
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