Adaptive Algorithms for Rotorcraft Active Vibration Control

VFS-F65-000319

5/27/2009

Authors
Abstract
Content

Rotorcraft vibration suppression has traditionally relied on passive devices, such as vibration isolation systems and dynamic absorbers that are effective at a single rotor speed. However, modern rotorcraft designs are moving towards variable rotor speed configurations for improved performance and reduced noise initiatives. Thus, in recent years airframe manufacturers, including Bell Helicopter Textron Inc., have been developing advanced Active Vibration Control (AVC) systems. Adaptive AVC algorithms have been developed and tested at Bell Helicopter to address the challenges of multiple rotor speeds and other aircraft changes that influence the vibration environment. These AVC algorithms are developed around the gain scheduling, automated real-time transfer function identification, and adaptive reference model methods. Laboratory testing of the algorithms using full-scale hardware has demonstrated their effectiveness and robustness. These algorithms have also been flight tested successfully on a Bell Model 430 helicopter. A summary of the algorithms and the test results is presented.

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DOI
https://doi.org/10.4050/VFS-F65-000319
Citation
Heverly, D., Singh, R., and Pappas, J., "Adaptive Algorithms for Rotorcraft Active Vibration Control," AHS 65th Annual Forum, Grapevine, Texas, May 27-29, 2009, Grapevine, Texas, May 27, 2009, https://doi.org/10.4050/VFS-F65-000319.
Additional Details
Publisher
Published
5/27/2009
Product Code
VFS-F65-000319
Content Type
Technical Paper
Language
English