DocumentCode
1899798
Title
Integrated Navigation System Design Based on DSP
Author
Li Guang-Hui ; Hu Jian-ming
Author_Institution
Eng. Training Center, Tianjin Univ. of Technol. & Educ., Tianjin, China
Volume
3
fYear
2012
fDate
23-25 March 2012
Firstpage
69
Lastpage
71
Abstract
Integrated navigation system has wide application prospect in the military and civilian. Navigation system directly affects the performance of direct flight control accuracy in the high-altitude unmanned flight. In this paper, micro-navigation system has been studied, based on the TMS320C6713 hardware and software design, which has a broad application prospect in field of UAV.
Keywords
accelerometers; aircraft navigation; autonomous aerial vehicles; avionics; digital signal processing chips; gyroscopes; inertial navigation; microsensors; DSP; TMS320C6713 hardware; UAV; direct flight control accuracy; high altitude unmanned flight; integrated navigation system design; micronavigation system; software design; Compass; Computers; Digital signal processing; Global Positioning System; Kalman filters; Microprocessors; GPS; Integrated navigation system; Kalman filter; TMS320C6713;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Electronics Engineering (ICCSEE), 2012 International Conference on
Conference_Location
Hangzhou
Print_ISBN
978-1-4673-0689-8
Type
conf
DOI
10.1109/ICCSEE.2012.252
Filename
6188068
Link To Document