Aircraft Structure Strain-Gage Loads Monitoring Method Study

来源 :The 2nd International Conference on Structural Health Monito | 被引量 : 0次 | 上传用户:bao21987
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  A method of aircraft structurc load monitoring based on strain gages has been developed by taking the composite materials box as the object of study.In order to obtain load equation,the mechanics model of composite materials box was established,sensor network layout and load test was designed,using the multiple liner regression method to process,optimize and inspection experimental data,finally conduct the structural load calibration measurement.The validation test result indicates the error of the real load value and the calculated loads is less than 10%.
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