Limit Cycle Oscillation Amplitude Tailorng Based on Describing Functions and $$\mu $$ Analysis-Reference-Cited by-同舟云学术

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Limit Cycle Oscillation Amplitude Tailorng Based on Describing Functions and $$\mu $$ Analysis

Published:2017-12-15 Issue: Volume: Page:101-119
ISSN:
Container-title:Advances in Aerospace Guidance, Navigation and Control
language:
Short-container-title:

Author:

Iannelli Andrea,Marcos Andrés,Lowenberg Mark

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-65283-2_6

Reference25 articles.

1. Allemang RJ, Brown DL (1982) A correlation coefficient for modal vector analysis. In: 1st International modal analysis conference

2. Anderson MR (1998) Pilot-induced oscillations involving multiple nonlinearities. J Guid Control Dyn 21(5):786–791

3. Baldelli DH, Lind RC, Brenner M (2005) Robust aeroservoelastic match-point solutions using describing function method. J Aircr 42(6):1597–1605

4. Bisplinghoff RL, Ashley H (1962) Principles of aeroelasticity. Wiley, New York

5. Borglund D (2004) The $$\mu $$ -k method for robust flutter solutions. J Aircr 41(5):1209–1216

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