Radio signal distortion assessment by non directional antennas of the helicopter

Vladimir A. Ivanov; Olexandr S. Zadorozhniy

doi:10.1109/ICATT.2017.7972669

Authors

Vladimir A. Ivanov National Aviation University, Kyiv, Ukraine https://orcid.org/0000-0001-6377-0959
Olexandr S. Zadorozhniy National Aviation University, Kyiv, Ukraine https://orcid.org/0000-0002-2660-8829

DOI:

https://doi.org/10.1109/ICATT.2017.7972669

Keywords:

directivity diagram, helicopter, effective length, pulsation, antenna, bit error

Abstract

The cause-effect relations between the levels of pulsations of the antenna system, caused by main rotor rotating of the helicopter, and the probability of the bit error occurring in the digital data transmission channels were established. Graph-analytical method of error probability estimation was developed.

References

V. Ivanov and A. Zadorozhniy, “The distortion of radio signals spectra by parametric system ‘basic antenna - the fuselage of helicopter’,” Electronics and Control Systems, no. 1, pp. 35-40, 2013.

Annex 10 to the Convention on International Civil Aviation. Aeronautical Telecommunications. Tom III. Communication system, Montreal, ICAO, 2007.

D. Ivlev, Tsifrovyie Kanalyi Peredachi Dannyih. Uchebno-Metodicheskoe Posobie [in Russian]. Nizhniy Novgorod: Nizhegorodskiy Gosuniversitet, 2013.

Radio signal distortion assessment by non directional antennas of the helicopter

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