Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System-Reference-Cited by-同舟云学术

Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System

Published:2021-11-29 Issue:1 Volume:23 Page:102-114
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Hong Sung-Boo,Lee Ye-Lin,Kwon Young-Min,Park Jae-Sang^ORCID,Kim Ji-su,Kim Do-Hyung

Funder

Agency for Defense Development

Ministry of Education

Ministry of Science, ICT and Future Planning

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-021-00426-3.pdf

Reference25 articles.

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2. Ruddell AJ (1981) Advancing blade concept (ABC) technology demonstrator. USAAVRADCOM-TR-81-D-5

3. Blackwell R, Millott T (2008) Dynamics design characteristics of the sikorsky X2 TechnologyTM demonstrator aircraft. In: 64th American Helicopter Society Annual Forum

4. Walsh D, Weiner S, Arifian K, Lawrence T, Wilson M, Millott T, Blackwell R (2011) High airspeed testing of the sikorsky X2 TechnologyTM demonstrator. In: 67th American Helicopter Society Annual Forum

5. Kim D-H, Kim T-J, Jung S-U, Kwak D-I (2016) Test and simulation of an active vibration control system for helicopter applications. Int J Aeronaut Sp Sci 17(3):442–453

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