Jamming Efficacy of Variable Altitude GPS Jammer against Airborne GPS Receiver, Theoretical Study and Parametric Simulation

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A. Esmaeilkhah
http://orcid.org/0000-0002-5564-2436
N. Lavasani

Abstract

Satellite-based navigation systems, as one of the key infrastructure of development in manned and unmanned guidance systems, is vulnerable against the simplest form of attack in Electronic Warfare environments. This led us to investigate the described vulnerability of an airborne GPS receiver against jammers which are located at various altitude above the targeted point. To do that and to avoid encountering with unavailability of classified information about military-class missiles, some simplification was done and the problem was investigated in “Worst Case” conditions. Finally, the flight profile and radiation pattern of the antenna of the GPS receiver were theoretically modeled. Considering some assumptions, the other parameters were derived from them. At the end, a simulation software was developed and some results were extracted. The data was represented figuratively and the dependency of efficacy of jamming operation to the jammer’s altitude and flight profile of the missile were discussed.

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How to Cite
Esmaeilkhah, A., & Lavasani, N. (2018). Jamming Efficacy of Variable Altitude GPS Jammer against Airborne GPS Receiver, Theoretical Study and Parametric Simulation. Advanced Electromagnetics, 7(1), 57–64. https://doi.org/10.7716/aem.v7i1.659
Section
Research Articles

References

A. Gulyas, British radar in WWII, Hungarian Defense Forces, 34. Special Operations Forces Battalion, Szolnok, Hungary, Vol. 7, No. 1 (2008) 175–185, Available at: www.zmne.hu/aarms/docs/Volume7/Issue1/pdf/14guly.pdf

W.L. Garfield, TACAN: a navigation system for aircraft, Proceedings of the IEE - Part B: Radio and Electronic Engineering, Volume: 105, Issue: 9, March 1958, DOI: 10.1049/pi-b-1.1958.0045

View Article

J. A . Pierce, An Introduction to Loran, The Proceedings of the IRE and Waves and Electrons.34, May. 1946. 216-234

View Article

P. B. Morris; R. R. Gupta, R. S. Warren, P. M. Creamer, Omega Navigation System Course Book. Volume 2, Technical rept. Mar 1990-Jul 1994, Analytic Sciences Corp Rrading, MA

L. Pisacane The Legacy of Transit: Guest Editor's Introduction by Vincent L. Pisacane, Johns Hopkins APL Technical Digest, Vol 19, Number 1, 1998.

J. H. REID, The SECOR Approach to Coordinate Determination for Ships and Aircraft, Navigation, Journal of Institute of navigation, Volume 11, Issue 4, Winter 1964, 393–416

L. Eldredge, GNSS Program Status, Satellite Navigation Summit, March 10, 2010, Munich, Germany.

M, Joerger, L. Gratton, B. Pervan, Analysis of Iridium-Augmented GPS for Floating Carrier Phase Positioning, NAVIGATION: Journal of The Institute of Navigation, Vol. 57, No. 2, Summer 2010, 138-160.

M. Lichtman, J. D. Poston, S. Amuru, et al., A Communications Jamming Taxonomy, IEEE Security & Privacy, Volume: 14, Issue: 1, Jan.-Feb. 2016, 47-54, DOI: 10.1109/MSP.2016.13.

View Article

D. Adamy, EW 102: A Second Course in Electronic Warfare, Artech House, 2004, 117-119, ISBN-13: 978-1580536868.

S. Hicks, Advanced Cruise Missile guidance system description, Proceedings of the IEEE National Aerospace and Electronics Conference, 24-28 May 1993. NAECON, Dayton, OH, USA.

View Article

Carlo Kopp, Tomahawk Cruise Missile Variants, BGM/ RGM/ AGM109, Tomahawk/ TASM /TLAM/ GCLM/ MRASM, Technical Report APA-TR-2005-0702, April, 2012, Available at: http://www.ausair power.net/Tomahawk-Subtypes.html

U. S. Kim, D. Akos, F. Bastide, Simulation and Validation of a GPS Antenna Array Concept for JPALS Application, ION GPS/GNSS 2003.