DocumentCode :
1794844
Title :
Design and implementation of GPS/INS integrated navigation simulation software
Author :
Wu Xiu-zhen ; Zhou Shao-lei ; Li Rui-tao
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
361
Lastpage :
365
Abstract :
Based on GPS/INS integrated navigation algorithm, The simulation of integrated navigation process is designed, comparing the accuracy advantages in contrast to pure inertial navigation; Based on the search model of terminal guidance radar, the hit probability calculation module of anti-ship missile is designed. The two modules form the GPS/INS integrated navigation simulation software, which can be used as a visualization platform for study of inertial navigation algorithm, integrated navigation algorithm and hit probability calculation, and also provide a powerful tool for the missile design.
Keywords :
Global Positioning System; aerospace computing; inertial navigation; military computing; military radar; missile guidance; GPS/INS integrated navigation algorithm; GPS/INS integrated navigation simulation software; antiship missile; hit probability calculation module; inertial navigation algorithm; integrated navigation process; missile design; search model; terminal guidance radar; visualization platform; Algorithm design and analysis; Global Positioning System; Inertial navigation; Missiles; Probability; Radar;
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.2014.7007256
Filename :
7007256
Link To Document :
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