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Simultaneous Vibration Reduction and Performance Improvement of Helicopter Rotor Using Individual Blade Pitch Control with Multiple Harmonic Inputs

Published Online: 2024-05-10

Published Print: 2024-10

Authors

Park, Jae-Sang https://orcid.org/0000-0002-7621-9565
Funding

Funding for this research was provided by:

Korea Research Institute for defense Technology Planning and advancement (KRIT-CT-21-020)

National Research Foundation of Korea (2020R1I1A3071793)

Ministry of Science and ICT (2021R1A5A1031868)
License Information

Text and Data Mining valid from 2024-05-10

Version of Record valid from 2024-05-10
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Article History

Received: 1 January 2024

Revised: 18 April 2024

Accepted: 19 April 2024

First Online: 10 May 2024

Declarations

:

: The authors declare that there is no conflict of interest regarding the publication of this paper.

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