DocumentCode :
232452
Title :
Sensitivity analysis based model validation for Hypersonic Vehicle model
Author :
Zeng Fanlin ; Zong Qun ; Zhang Xibin ; You Ming
Author_Institution :
Sch. of Autom. & Electr. Eng., Tianjin Univ. of Technol. & Educ., Tianjin, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
6287
Lastpage :
6292
Abstract :
This paper presents a novel model validation methodology based on sensitivity analysis method. Uncertain parameters of the Hypersonic Vehicle model are considered as risk factors. Validation method is composed of parameter sensitivity analysis and uncertainty quantification. Quantitative evaluation of the accuracy and reliability of model are given from the user´s point of view with validation metrics. The new model validation method was then used to evaluate the quality of the Hypersonic Vehicle model. Simulation results are provided to demonstrate that the new model validation method provides a highly efficient and powerful new method for Hypersonic Vehicle model validation.
Keywords :
aircraft control; risk analysis; sensitivity analysis; hypersonic vehicle model; parameter sensitivity analysis; quantitative evaluation; reliability; risk factors; sensitivity analysis based model validation method; uncertain parameters; uncertainty quantification; Analytical models; Computational modeling; Predictive models; Sensitivity analysis; Uncertainty; Vehicles; Hypersonic vehicle; Model validation; Risk factor; Security metrics; Sensitivity analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6896022
Filename :
6896022
Link To Document :
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