DocumentCode :
518523
Title :
INS computer design basing on subdivision technology
Author :
Liao Dan ; Yang Jian-qiang ; Zhu Yong
Author_Institution :
Coll. of Opto-Electron. Sci. & Eng., Nat. Univ. of Defence Technol., Changsha, China
Volume :
4
fYear :
2010
fDate :
16-18 April 2010
Abstract :
The inertial navigation system (INS) computer is a key part in the inertial navigation application. Traditional PC104 computer is of many disadvantages such as fixed board layout and large power dissipation, which makes the system impossible to integrate the functions of signal collecting and navigation computing for reducing the power dissipation and size of board. In this paper, a new INS computer is designed using DSP TMS320C6713 and FPGA XC3S400AN. The computer integrates the signal collecting work by employing pulse subdivision method to avoid ±1 quantization error. Experimental results show that the new INS computer gets good performance on signal collecting (RMS of 10-3) and inertial navigation computing, brings decreased power dissipation (1.5W) as well, which makes it useful in INS application.
Keywords :
aerospace computing; computerised navigation; digital signal processing chips; field programmable gate arrays; inertial navigation; DSP TMS320C6713; FPGA XC3S400AN; INS computer design; inertial navigation system; power dissipation; pulse subdivision technology; signal collection; Accelerometers; Aircraft navigation; Application software; Digital signal processing; Field programmable gate arrays; Inertial navigation; Military computing; Power dissipation; Power engineering computing; Sensor systems; INS; power dissipation; signal collecting;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6347-3
Type :
conf
DOI :
10.1109/ICCET.2010.5486367
Filename :
5486367
Link To Document :
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