Evaluation of Structural Behaviour of INS Device Installation Design on Unmanned Aerial Vehicle Using Finite Element Method and Modal Testing

Author:

GÜNGÖR Erkin Barış,ÇELİK Bilgin

Publisher

Journal of Aviation Research, Maltepe University

Subject

General Medicine

Reference13 articles.

1. Baker, A., Dutton, S., & Kelly, D. (2004). Composite Materials for Aircraft Structures - 2nd ed. Virginia: American Institute of Aeronautics and Astronautics.

2. Ersoy, K. (2017). Operational Modal Analysis in Helicopter Structures Containing Harmonic Excitations. AIAC. Ankara.

3. Inertial Reference System (IRS). (2020). Retrieved from skybrary.aero: https://www.skybrary.aero/index.php/Inertial_Reference_System_(IRS)

4. Irvine, M. (1986). Structural Dynamics for the Practising Engineer. Oxon: Taylor & Francis.

5. Kurowski, P. M. (2004). Finite Element Analysis for Design Engineers. Warrendale,PA: SAE International.

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