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Dynamic Active Noise Control of Broadband Noise in Fighter Aircraft Pilot Helmet

Y. K. Bharath1,*, S. Veena2

1 Malnad College of Engineering, Hassan, 573202, India
2 National Aerospace Laboratories, Bengaluru, 560017, India

* Corresponding Author: Y. K. Bharath. Email: email

Sound & Vibration 2022, 56(4), 319-331. https://doi.org/10.32604/sv.2022.015634

Abstract

This paper presents the development of a dynamic Active Noise Control (ANC) algorithm aimed towards reducing the broadband noise inside the helmet earcups of a fighter aircraft pilot helmet. The dynamic ANC involves a Variable Step-Size Griffiths (VSSG) FxLMS algorithm to attenuate noise entering directly through helmet, a LMS based adaptive noise canceller to attenuate noise entering through the pilot microphone, and energy detectors for failure protection and optimized battery power usage. The algorithms are implemented on Texas Instruments’ TMS320C6748 processor and are tested in a helmet ANC experimental setup.

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Bharath, Y. K., Veena, S. (2022). Dynamic Active Noise Control of Broadband Noise in Fighter Aircraft Pilot Helmet. Sound & Vibration, 56(4), 319–331.



cc This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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