Design of Airborne Strapdown Inertial Navigation System Based on DSP Structure

DOI

10.2991/iccmcee-15.2015.20How to use a DOI?

Keywords

Airborne strapdown inertial navigation system, Digital signal processor, Micro inertial measurement group, Data acquisition

Abstract

An airborne strapdown inertial navigation system based on DSP is introduced. The TMS320F28335 and TMS320C6416 DSP chips of TI Company are used as the core components of the system, and the CPLD technique combined with the dual DSP structure of strapdown control and solution are used to realize logic circuit of the system. From the analysis of the hardware, software and overall design, the scheme can match the characteristics of the strapdown inertial navigation system, such as fast speed, high accuracy and good stability.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Jing Yu
AU  - Hang Guo
PY  - 2015/11
DA  - 2015/11
TI  - Design of Airborne Strapdown Inertial Navigation System Based on DSP Structure
BT  - Proceedings of the 2015 4th International Conference on Computer, Mechatronics, Control and Electronic Engineering
PB  - Atlantis Press
SP  - 97
EP  - 101
SN  - 2352-5401
UR  - https://doi.org/10.2991/iccmcee-15.2015.20
DO  - 10.2991/iccmcee-15.2015.20
ID  - Yu2015/11
ER  -