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