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
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;
Conference_Titel :
Computer Science and Electronics Engineering (ICCSEE), 2012 International Conference on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-4673-0689-8
DOI :
10.1109/ICCSEE.2012.252
