Quantity Requirement Analysis of Stratospheric Airship-Carried GPS Jammer

Conference paper
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 207)

Abstract

In order to react to the development of “Air-Sea Battle” and Global Positioning System (GPS) precision-guided weapons and enhance anti-intervened combat capabilities, a combat mode that obstructs the GPS receivers which utilizes stratospheric airships as the jammer carrier is put forward. A mathematical model about the relationship with the jammer height, transmitted power and the effective interference distance is derived, and the capacity of the jammer is simulated and analyzed. According to the quantitative measurement of the lethality of cruise missiles, the requirement of the effective interference distance is also put forward. And it calculates the required number of jammer that protect point target by using the irregular region Hexagonal grid filling algorithm.

Keywords

Suppressible jamming Disposition Boundary-fill algorithm Stratospheric airship Global positioning system (GPS) Point target protection 

Notes

Acknowledgments

The authors would like to thank Ma S.Z. and He C. for their valuable comments and suggestions which have significantly enhanced the quality of this manuscript.

References

  1. 1.
    Liang K (2004) The design of interference transmitter of GPS receiver, vol 87. Wuhan University, pp 112–143Google Scholar
  2. 2.
    Ding J, Hu LY, Li RG (2004) Study and realization of surface to air radar counter measure simulation system. Ship Board Electron Countermeasure 06:39–40Google Scholar
  3. 3.
    Zou ZN, Yang ZQ, Zhou Y (2003) Feasibility analysis of electronic interference on GPS. Electro-optic Technol Appl 4:4–5Google Scholar
  4. 4.
    Lambert JR, Balanis CA, DeCarlo D (2009) Spherical cap adaptive antennas for GPS. IEEE Trans Antennas Propag 2:406–414CrossRefGoogle Scholar
  5. 5.
    Zhou KF, Zhou XR, LI DW (2005) Exploration for GPS jamming to GPS/INS guided cruise missile. Avionics Technol 3:1–6Google Scholar
  6. 6.
    Zhao XL, Zhang C, Zhang WD (2003) Study on jamming of GPS system and its air defense application. Chinese society of aeronautics and astronautics electronic professional board 2003 exchange meeting, vol 3, pp 36–40Google Scholar
  7. 7.
    Shu SH, Chen L, Zheng Z (2008) Analysis of the turbulent channels for near-space free-space laser communication. Electron Opt Contr 2:19–23Google Scholar
  8. 8.
    Cao K, John B (2010) Multimode heat transfer in a near-space environment. Heat Transfer Eng 1:7–13Google Scholar
  9. 9.
    Khandu JL, Awange JL, Wickert J (2011) GNSS remote sensing of the Australian tropopause. Climatic Change 105:0597–0618CrossRefGoogle Scholar
  10. 10.
    Shifrin DM, Yushkov VA, Lykov AD (2010) An experience of participation of russian specialists in international programs on atmospheric balloon investigations. Russ Meteorol Hydrol 8:0571–0600CrossRefGoogle Scholar
  11. 11.
    Liu YK (2002) The basic algorithm for computer graphics, vol 37. Science Press, Beijing, pp 250–325Google Scholar

Copyright information

© Springer-Verlag London 2013

Authors and Affiliations

  1. 1.The Missile Institute of Air Force Engineering UniversitySanyuanChina
  2. 2.The Research Ministry of Air Force Engineering UniversityXi’anChina

Personalised recommendations