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
Link To Document :
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