DocumentCode
512426
Title
The application of linear adjoint method in rocket ballistic error analysis
Author
Zhao, Dunhui ; Chen, Jiabin ; Xu, Jun ; Liu, Zhide ; Han, Yongqiang
Author_Institution
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
Volume
1
fYear
2009
fDate
28-29 Nov. 2009
Firstpage
146
Lastpage
149
Abstract
This paper established a linear dynamic model of the rocket using segmental ballistic linearization methodology based on small turbulence theory. Based on the model, the application of linear adjoint method in rocket is studied. Ballistic error is deduced and analyzed. Finally the feasibility of applying linear adjoint method to rocket error is testified through computer simulation.
Keywords
ballistics; error analysis; linearisation techniques; rockets; computer simulation; linear adjoint method; rocket ballistic error analysis; segmental ballistic linearization methodology; Aerodynamics; Aerospace engineering; Aerospace industry; Automation; Computational intelligence; Computer industry; Equations; Error analysis; Paper technology; Rockets; adjoint method; error analysis; linearization; rocket;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Industrial Applications, 2009. PACIIA 2009. Asia-Pacific Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-4606-3
Type
conf
DOI
10.1109/PACIIA.2009.5406471
Filename
5406471
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