A Method of Traction Partial Jamming on GPS/INS Integrated Navigation

DOI

10.2991/iccsee.2013.64How to use a DOI?

Keywords

Integrated navigation system, Cruise missile, Complete trajectory simulation

Abstract

To solve the GPS/INS integrated navigation countermeasure problem, a method of traction partial jamming on GPS/INS integrated navigation is proposed. Deception jamming signal produced by jamming equipment can force GPS receiver to output navigation and position data that have gradual departure from the real position. When the bias error can not be corrected by integrated navigation, the traction partial jamming occurs. The definition, signal form and simplified form of jamming method are provided in this paper. The hardware-in-the-loop simulation verifies the effectiveness of the method and analyses its jamming effects.

Copyright

© 2013, 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  - Jun Chen
AU  - Yi Liu
AU  - Yun-hong Li
AU  - Da-ming Wang
AU  - Xin-yuan An
PY  - 2013/03
DA  - 2013/03
TI  - A Method of Traction Partial Jamming on GPS/INS Integrated Navigation
BT  - Proceedings of the 2nd International Conference on Computer Science and Electronics Engineering (ICCSEE 2013)
PB  - Atlantis Press
SP  - 247
EP  - 250
SN  - 1951-6851
UR  - https://doi.org/10.2991/iccsee.2013.64
DO  - 10.2991/iccsee.2013.64
ID  - Chen2013/03
ER  -