Aeroelastic System Identification Using the Minimum Model Error Method-Reference-Cited by-同舟云学术

Aeroelastic System Identification Using the Minimum Model Error Method

Published:2006-07 Issue:4 Volume:29 Page:936-943
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Shiryayev Oleg V.¹,Slater Joseph C.¹

Affiliation:

1. Wright State University, Dayton, Ohio 45435

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.14966

Reference17 articles.

1. 1Juang, J.N., Applied System Identification, Prentice-Hall, Englewood Cliffs, NJ, 1994, pp.121-255.

2. Minimum model error estimation for poorly modeled dynamic systems

3. 4Stry, G. "MME Nonlinear Dynamic System Identification," Ph.D. Dissertation, School of Engineering and Applied Science,Univ. of New York, Buffalo,NY, Aug. 1991.

4. Minimum Model Error Approach for Attitude Estimation

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aeroelastic stability and nonlinear flutter analysis of viscoelastic heated panel in shock-dominated flows;Aerospace Science and Technology;2021-10

2. Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model;Acta Mechanica;2021-06-28

3. Theoretical analysis for the effect of static pressure differential on aeroelastic stability of flexible panel;Aerospace Science and Technology;2021-02

4. Analysis on location of maximum vibration amplitude in panel flutter;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-09-24

5. Effects of Shock Location on Aeroelastic Stability of Flexible Panel;AIAA Journal;2018-09