Hardware-in-the-Loop Test Platform Design for UAV Applications

Emre Atlas; Melike Irem Erdoğan; Onur Baki Ertin; Anıl Güçlü; Yusuf Eren Saygi; Ünver Kaynak; Coşku Kasnakoğlu

doi:10.4028/www.scientific.net/AMM.789-790.681

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 789-790Hardware-in-the-Loop Test Platform Design for UAV...

Hardware-in-the-Loop Test Platform Design for UAV Applications

Abstract:

A hardware-in-the-loop (HIL) platform for unmanned air vehicle (UAV) systems is designed that demonstrates flight attitudes on yaw, pitch and roll axes. The design combines a sophisticated flight simulation software with a platform capable of moving 360 degrees on all axes. This enables the testing of the flight sensors and autopilot algorithms for all sorts of scenarios including emergency and acrobatic cases where an indefinite number of full rotations in the yaw, roll and pitch might take place.

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Periodical:

Applied Mechanics and Materials (Volumes 789-790)

Pages:

681-687

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.789-790.681

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Cite this paper

Online since:

September 2015

Authors:

Emre Atlas*, Melike Irem Erdoğan, Onur Baki Ertin, Anıl Güçlü, Yusuf Eren Saygi, Ünver Kaynak, Coşku Kasnakoğlu

Keywords:

Autopilot, Gyroscope Test Systems, Hardware-in-the-Loop, HIL, MATLAB Model, PID, PID Controller, UAV, UAV Simulation Systems, UAV Test, UAV Test Platform

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* - Corresponding Author

References

[1] Onur Baki Ertin, Halim Korkmaz, Ünver Kaynak ve Coşku Kasnakoğlu. Hardware-in-the-Loop Test Platform for a Small Fixed Wing Unmanned Aerial Vehicle Embedded Controller. The 32nd IASTED International Conference on Modelling, Identification and Control, Innsbruck, Austria, (2013).

DOI: 10.2316/p.2013.794-059

Google Scholar

[2] McManus, Iain A., Greer, Duncan G., & Walker, Rodney A. (2003) UAV Avionics Hardware in the Loop, Simulator. In 10th Australian International Aerospace Congress, 29 July – 1 August 2003, Brisbane, Queensland, Australia.

Google Scholar

[3] Dongwon Jung, Panagiotis Tsiotras, Modeling and Hardware-in-the-Loop Simulation for a Small Unmanned Aerial Vehicle, AIAA Conference, (2007).

DOI: 10.2514/6.2007-2768

Google Scholar

[4] Guowei Cai , Ben M. Chen, , Tong H. Lee , Miaobo Dong, Design and implementation of a hardware-in-the-loop simulation system for small-scale UAV helicopters.

DOI: 10.1109/ical.2008.4636114

Google Scholar

[5] McManus, Iain A., Greer, Duncan G., & Walker, Rodney A. (2003) UAV Avionics Hardware in the Loop, Simulator. In 10th Australian International Aerospace Congress, 29 July – 1 August 2003, Brisbane, Queensland, Australia.

Google Scholar

[6] Claire Tomlin, Stanford Univ., CA; Jung Jang, AIAA, Autopilot design for the Stanford DragonFly UAV - Validation through hardware-in-the-loop simulation (2001).

DOI: 10.2514/6.2001-4179

Google Scholar