2005
DOI: 10.1115/1.2062829
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On the Uniqueness of Solutions for the Identification of Linear Structural Systems

Abstract: This work tackles the problem of global identifiability of an undamped, shear-type, N degrees of freedom linear structural system under forced excitation without any prior knowledge of its mass or stiffness distributions. Three actuator/sensor schemes are presented, which guarantee the existence of only one solution for the mass and stiffness identification problem while requiring a minimum amount of instrumentation (only 1 actuator and 1 or 2 sensors). Through a counterexample for a 3DOF system it is also sho… Show more

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Cited by 28 publications
(53 citation statements)
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“…Hence, for a 3-DOF shear-type system for which the 2nd row of V is known, there may exist two possible sets of 1st and 3rd rows of V, one of which will correspond to the true system, and the other to an alternative, but also physically admissible, system. An example of such non-uniqueness was also discussed in [9] where it was shown that two 3-DOF systems, System I with {m 1 , m 2 , m 3 }¼ {0.85, 1.3, 1.1} and {k 1 , k 2 , k 3 } ¼{9, 12, 11}; and System II with {m 1 , m 2 , m 3 } ¼{2.3690, 1.3000, 0.2776,} and {k 1 , k 2 , k 3 } ¼{7.5473, 16.1429, 6.8571}, will have the same response at DOF 2 for the same applied force at DOF 2, and thus will have the same eigenvalues and the same 2nd row of V. Proof of Statement 4. The proof of this statement is intuitive.…”
Section: A Procedures Of Mode Shape Expansion and Associated Uniquenesmentioning
confidence: 95%
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“…Hence, for a 3-DOF shear-type system for which the 2nd row of V is known, there may exist two possible sets of 1st and 3rd rows of V, one of which will correspond to the true system, and the other to an alternative, but also physically admissible, system. An example of such non-uniqueness was also discussed in [9] where it was shown that two 3-DOF systems, System I with {m 1 , m 2 , m 3 }¼ {0.85, 1.3, 1.1} and {k 1 , k 2 , k 3 } ¼{9, 12, 11}; and System II with {m 1 , m 2 , m 3 } ¼{2.3690, 1.3000, 0.2776,} and {k 1 , k 2 , k 3 } ¼{7.5473, 16.1429, 6.8571}, will have the same response at DOF 2 for the same applied force at DOF 2, and thus will have the same eigenvalues and the same 2nd row of V. Proof of Statement 4. The proof of this statement is intuitive.…”
Section: A Procedures Of Mode Shape Expansion and Associated Uniquenesmentioning
confidence: 95%
“…Furthermore, while the above studies provide answers to the question of minimal instrumentation, there still exists a need to develop and validate robust methods for unique mode shape expansion and consequent parametric identification using input-output data from prescribed minimal instrumentation set-ups. As Franco et al [9] clearly state: "…satisfying global identifiability does not mean that the unique solution is found. Indeed, to find this solution it is usually necessary to solve a nonlinear optimization problem that can be quite complex…", and illustrates the complexity one will encounter using a 3-DOF system at the end of their paper.…”
Section: Introductionmentioning
confidence: 95%
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