IDENTIFICATION OF DAMAGE IN PLATE-LIKE STRUCTURES USING TWO STAGE ALGORITHM COMBINES NON- MODEL BASED AND MODEL BASED TECHNIQUES | ||
| International Conference on Aerospace Sciences and Aviation Technology | ||
| Article 119, Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Pages 1-21 PDF (226.98 K) | ||
| Document Type: Original Article | ||
| DOI: 10.21608/asat.2007.24375 | ||
| Authors | ||
| Abdelkhalik, M.1; Amin, M. S.2; Zidan, M. K.3 | ||
| 1Msc, Civil Eng. Department, Military Technical College, Egyptian Armed Forces, Egypt. | ||
| 2Ph.D, Civil Eng. Department, Military Technical College, Egyptian Armed Forces, Egypt. | ||
| 3Professor, Civil Eng. Department, Faculty of Engineering, Ain Shams University, Cairo, Egypt. | ||
| Abstract | ||
| The regular structural integrity monitoring of major engineering structures such as space structures, orbiting spacecrafts, and civil infrastructures have become an urgent necessity to prevent potential catastrophic failures. The evolution of Vibration Based Damage Identification methods (VBDI) introduced an alternative techniques to the conventional methods. These methods relate changes in the vibration signature (natural frequencies and mode shapes) to changes in structural physical parameters (mass and stiffness) and thus is used to identify damage. The present research focus on developing a combined algorithm includes a model-based method (optimal matrix update) and a Non model-based method (frequency response functions difference), to enhance the reliability of the VBDI techniques. The algorithm presented robust sequential scheme of VBDI techniques and has proven a reasonable success when tested through numerical simulation on a large complex space frame. Since, the FEM of the monitored structure considered as a major constitute of the identification procedure, in the present paper, the ability of the proposed combined algorithm to identify damage in plate-like structure is investigated. A numerical simulation is carried out by introducing several damage scenarios to steel plate and predictions were compared to the known damage. Regardless the assumptions made in the FEM and the introduced simulated random errors introduced at different steps in the algorithm procedures, the algorithm is found to be reliable in identifying damage in plate-like structures. | ||
| Keywords | ||
| Vibration-based damage detection; structural health monitoring; identification of damage in plate-like structures; frequency response function; optimal matrix update; Optimization | ||
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