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dc.contributor.authorXixiong Wang
dc.contributor.authorYu Qi
dc.contributor.authorZhen Li
dc.contributor.authorZhaoye Qin
dc.contributor.authorTao Yu
dc.contributor.authorJifeng Ding
dc.contributor.authorFulei Chu
dc.date.accessioned2022-08-18T12:16:29Z
dc.date.available2022-08-18T12:16:29Z
dc.date.issued2022/05/27
dc.identifier.other%28ASCE%29AS.1943-5525.0001458.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4286332
dc.description.abstractLow-frequency errors are a type of testing errors commonly existing in pyroshock experiments due to the harsh mechanical environment that lead to inaccuracy and contamination of pyroshock data. It is necessary to eliminate such low-frequency errors from pyroshock data via data analysis. Two methods based on discrete wavelet transform (DWT) and ensemble empirical mode decomposition (EEMD) are proposed, respectively, in this article. Firstly, the principle and operating process of these two methods are introduced, where four correlation coefficients are defined to determine the decomposition level for quantitative correction. Then, the two methods are applied to remove the integral zero shift from a set of pyroshock test data, respectively, and the capability and effectiveness of the two methods are compared. It is revealed from the comparison studies that both methods are capable of removing integral zero shift effectively to correct the shock response spectrum and improve the accuracy of pyroshock data. The correlation coefficients constructed here can help to realize quantitative selection of key parameters for the two methods. The DWT method shows better correction performance for extracting accurate parameters, whereas the EEMD method is more concise and convenient for application.
dc.publisherASCE
dc.titleA Comparative Study of DWT and EEMD Methods for Validation and Correction of Pyroshock Data
dc.typeJournal Article
dc.journal.volume35
dc.journal.issue5
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/(ASCE)AS.1943-5525.0001458
dc.journal.fristpage04022061
dc.journal.lastpage04022061-11
dc.page11
dc.treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005
dc.contenttypeFulltext


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