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