DocumentCode :
2984423
Title :
The Precision Analysis and Simulation Based on SLAM
Author :
Yang, Ping ; Bin Zhang ; Dong, Guo-fang ; Kuang, Shen-Qing
Author_Institution :
Dept. of Commanding, Commanding Commun. Acad., Wuhan, China
fYear :
2010
fDate :
25-27 June 2010
Firstpage :
5810
Lastpage :
5813
Abstract :
Precision analysis is one of the key factors which must be considered in the process of Anti-air missile guidance system design . In this paper, a homing guidance system of anti-aircraft missile systems is analyzed, and finally statistical linearization adjoint method (SLAM) is chosen. Considering the system with disturbance of target maneuver, glint, atmosphere nois s and so on, a typical proportional navigation engagement simulation model is stablished. The simulation results show that the SLAM can not only get the root mean square miss distance, but also the total impact of the miss distance due to the different random input signal of the system, which results into a higher accuracy of guidance system in practice.
Keywords :
linearisation techniques; mean square error methods; missile guidance; statistical analysis; anti-air missile guidance system; homing guidance system; precision analysis; root mean square miss distance; statistical linearization adjoint method; Aerospace control; Atmospheric modeling; Missiles; Monte Carlo methods; Physics; Publishing; Simultaneous localization and mapping; adjoint method(SLAM); homing guidance system; precision analysis; statistical linearization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-6880-5
Type :
conf
DOI :
10.1109/iCECE.2010.1458
Filename :
5630106
Link To Document :
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