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Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1017/S0001924000004978
AuthorSearch for: 1; Search for: 2; Search for: 2; Search for: 2
Affiliation
  1. Carleton University
  2. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
Publication date
In
  • The Aeronautical Journal 108, no. 1079: 35–42.
LanguageEnglish
Peer reviewedYes
NRC numberSMPL-2002-0244
NPARC number8928308
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Record identifier9f2daa2b-b33a-4174-abe8-b1df6d5f237f
Record created2009-04-23
Record modified2020-04-17
Date modified: