On-line identification, flutter testing and adaptive notching of structural mode parameters for V-22 tiltrotor aircraft-Reference-Cited by-同舟云学术

On-line identification, flutter testing and adaptive notching of structural mode parameters for V-22 tiltrotor aircraft

Published:2000-04 Issue:2 Volume:25 Page:137-158
ISSN:0256-2499
Container-title:Sadhana
language:en
Short-container-title:Sadhana

Author:

Mehra R. K.,ARambel P. O.,Sampath A. M.,Prasanth R. K.,Parham T. C.

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Link

http://link.springer.com/content/pdf/10.1007/BF02703755.pdf

Reference12 articles.

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3. Faure P 1976 Stochastic realization algorithms. InSystem Identification: Advances and Case Studies (eds) R K Mehra, D G Larniotis (New York: Academic Press)

4. Mehra R K 1991 Identification of state space models using a stochastic realization algorithm with applications to modal identification of flexible aerospace structures.IFAC Symp. on System Identification, Budapest, June

5. Mehra R K 1994a A new unified approach to state space model structure determination and maximum likelihood identification with aerospace applications.IFAC Symp. on System Identification, Copenhagen, July

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