DocumentCode :
1795110
Title :
Precision analysis of exoatmospheric endgame guidance based on unscented transformation
Author :
Wenshan Su ; Weilin Wang ; Lei Chen
Author_Institution :
Coll. of Aerosp. Sci. & Eng., Nat. Univ. of Defense Technol., Changsha, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1362
Lastpage :
1367
Abstract :
Precision analysis is an important task of the exoatmospheric endgame guidance. The conventional method Monte Carlo is time-consuming. Covariance analysis description equation technique (CADET) needs to linearize the nonlinear model, which is complicated and the precision is difficult to be guaranteed. In order to overcome these problems, a new method based on the Unscented Transformation (UT) for nonlinear endgame guidance error analysis is proposed. The error transformation model and the error propagation model are deduced for the nonlinear exoatmospheric endgame guidance system. And they are testified by simulation. Simulation results are compared with that of Monte Carlo method and indicate that the guidance high precision can be guaranteed by the proposed method high at low time-cost and the process is simple.
Keywords :
covariance analysis; missile guidance; nonlinear control systems; CADET; covariance analysis description equation technique; error propagation model; error transformation model; nonlinear endgame guidance error analysis; nonlinear exoatmospheric endgame guidance system; nonlinear model; precision analysis; unscented transformation; Acceleration; Analytical models; Equations; Mathematical model; Monte Carlo methods; Standards; Vectors;
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.2014.7007395
Filename :
7007395
Link To Document :
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