DocumentCode
1795193
Title
Modeling method for gliding reentry vehicle via model migration
Author
Haoliang Wang ; Qingdong Li ; Zhang Ren ; Zixuan Liang
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
1739
Lastpage
1743
Abstract
The development of gliding reentry vehicle is a process of small-batch and multi-batch. In order to reduce the cost of experiments and shorten the cycle of modeling of gliding reentry vehicles with similar shapes, the new method based on model migration is presented in this paper. Specifically, a method of assessing the similarity degree of the gliding reentry vehicles is explained; whether the model migration theory can be applied in the vehicle modeling depends on the degree. The aerodynamic coefficients of the base gliding reentry vehicle are partitioned by the linearity of itself, and the cluster centers of the intervals are obtained. The migration equations are given through the analysis of the relation of the cluster centers of aerodynamic coefficients of the base vehicle to the ones of the new vehicle. The advantage of the new method is verified by the simulation.
Keywords
entry, descent and landing (spacecraft); vehicle dynamics; aerodynamic coefficients; base gliding reentry vehicle modeling method; cost reduction; interval cluster centers; model migration theory; multibatch process; small-batch process; Aerodynamics; Atmospheric modeling; Linearity; Mathematical model; Numerical models; Shape; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007445
Filename
7007445
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