SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE.

P. E. O'Donoghue; S. N. Atluri

SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE.

P. E. O'Donoghue
, S. N. Atluri

Southwest Research Institute

Research output: Contribution to a Journal (Peer & Non Peer) › Conference article › peer-review

Abstract

The topic of vibration control of large space structures which, in this instance are modeled by equivalent continua, is addressed here. A 'singular (or fundamental) solution' approach is utilized and the control algorithm is based on a fully coupled nodal system of equations which permits the effects of non-proportional damping to be monitored. Additionally, the structure will be allowed to undergo large deformations which will necessitate the implementation of a nonlinear control algorithm. In the scheme proposed here, the calculation of the feedback control forces will be based on the feedback gain matrix obtained from a solution of the linear optimal control problem. Examples will be presented to illustrate the controllability of the vibrations in both the linear and nonlinear cases.

Original language	English
Pages (from-to)	35-42
Number of pages	8
Journal	Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Issue number	pt 2
Publication status	Published - 1986
Externally published	Yes

Cite this

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title = "SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE.",

abstract = "The topic of vibration control of large space structures which, in this instance are modeled by equivalent continua, is addressed here. A 'singular (or fundamental) solution' approach is utilized and the control algorithm is based on a fully coupled nodal system of equations which permits the effects of non-proportional damping to be monitored. Additionally, the structure will be allowed to undergo large deformations which will necessitate the implementation of a nonlinear control algorithm. In the scheme proposed here, the calculation of the feedback control forces will be based on the feedback gain matrix obtained from a solution of the linear optimal control problem. Examples will be presented to illustrate the controllability of the vibrations in both the linear and nonlinear cases.",

author = "O'Donoghue, \{P. E.\} and Atluri, \{S. N.\}",

year = "1986",

language = "English",

pages = "35--42",

journal = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",

issn = "0273-4508",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "pt 2",

}

SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE. / O'Donoghue, P. E.; Atluri, S. N.
In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. pt 2, 1986, p. 35-42.

Research output: Contribution to a Journal (Peer & Non Peer) › Conference article › peer-review

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T1 - SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE.

AU - O'Donoghue, P. E.

AU - Atluri, S. N.

PY - 1986

Y1 - 1986

N2 - The topic of vibration control of large space structures which, in this instance are modeled by equivalent continua, is addressed here. A 'singular (or fundamental) solution' approach is utilized and the control algorithm is based on a fully coupled nodal system of equations which permits the effects of non-proportional damping to be monitored. Additionally, the structure will be allowed to undergo large deformations which will necessitate the implementation of a nonlinear control algorithm. In the scheme proposed here, the calculation of the feedback control forces will be based on the feedback gain matrix obtained from a solution of the linear optimal control problem. Examples will be presented to illustrate the controllability of the vibrations in both the linear and nonlinear cases.

AB - The topic of vibration control of large space structures which, in this instance are modeled by equivalent continua, is addressed here. A 'singular (or fundamental) solution' approach is utilized and the control algorithm is based on a fully coupled nodal system of equations which permits the effects of non-proportional damping to be monitored. Additionally, the structure will be allowed to undergo large deformations which will necessitate the implementation of a nonlinear control algorithm. In the scheme proposed here, the calculation of the feedback control forces will be based on the feedback gain matrix obtained from a solution of the linear optimal control problem. Examples will be presented to illustrate the controllability of the vibrations in both the linear and nonlinear cases.

UR - https://www.scopus.com/pages/publications/0022605936

M3 - Conference article

AN - SCOPUS:0022605936

SN - 0273-4508

SP - 35

EP - 42

JO - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

JF - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

IS - pt 2

ER -

SINGULAR-SOLUTION APPROACH FOR CONTROLLING THE NONLINEAR RESPONSE OF A CONTINUUM MODEL OF A LARGE SPACE STRUCTURE.

Abstract

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