Design and Simulation of the Linear Individual Blade Control Laws for Vibratory Loads Reduction in a Medium-size Rotorcraft

Author:

Shin Sang Joon,Im Byeonguk,Kong Kunhyuk,Go Gwangin,Park Sunhoo,Kang Seung-Hoon,Cho Haeseong

Funder

Ministry of Science, ICT and Future Planning

National Research Foundation of Korea

Publisher

The Korean Society for Noise and Vibration Engineering

Subject

Linguistics and Language,Anthropology,History,Language and Linguistics,Cultural Studies

Reference12 articles.

1. Closed-Loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction

2. Closed-Loop Test of a Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction

3. Straub, F. K., Anand, V. R., Birchette, T. S. and Lau, B. H., 2009, SMART Rotor Development and Wind Tunnel Test, 35th European Rotorcraft Forum.

4. Lee, Y., Kim, D., Park, J. and Hong, S., 2019, Airframe Vibration Reduction Simulation using Active Rotor Control and Active Vibration Control System for High-speed Compound Rotorcrafts, Proceedings of the KSNVE Annual Autumn Conference, p. 166.

5. Active Vibration Control Test of High-speed Compound Unmanned Rotorcraft Using Scaled Airframe Model

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