摄动(天文学)
结构体系
计算机科学
数学优化
控制理论(社会学)
数学
结构工程
工程类
物理
量子力学
人工智能
控制(管理)
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:1977-08-01
卷期号:15 (8): 1095-1100
被引量:66
摘要
The objective of the effort was to investigate methodologies to reduce the cost of evaluating changes in dynamic loads when small modifications are made in the structure. A matrix perturbation technique has been developed to calculate the dynamic responses of a structural system that has been modified from the original design. The calculation is based on the results of the original design and the assumption that the structural modification is small. The advantage of the method is an update of the dynamic response due to design changes without performing an entire analysis. This procedure can be used in a design load analysis cycle in which the structural design is subject to frequent changes. A sample problem is given to demonstrate the validity of the technique.
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