The preliminary results of theoretical and experimental range estimations for Multifunctional X-ray Navigation System (MXNS) at a precipitation and other conditions are presented. The most difficult case is the complex X-ray attenuation (up to 98%) by atmosphere, heavy rain, “brownout” or “whiteout”, an aircraft skin and icing up. Derived from analysis of the precipitation and other conditions information the some phantoms have been designed for test-bench experiments. The experimental test-bench results were confirmed calculations of X-ray attenuation in the propagation medium. The experimental results obtained lead to the following MXNS's researches in real conditions.
REFERENCES
1.
“
Rotary-Wing Brownout Mitigation: Technologies and Training
”. A Technical Report by NATO Research and Technology Organization, North Atlantic Treaty Organization
(2012
).2.
Robert
Cheung
, “Spatial Orientation – Nonvisual Spatial Orientation Mechanisms” // F.
Previc
, W.
Ercoline
(Eds.) Spatial Disorientation in Aviation. Progress in Astronautics and Aeronautics
Volume 203
. American Institute of Aeronautics and Astronautics, Inc
. Restin, VA, USA
. (2004
), pp. 37
–94
.3.
Safety analysis of the Russian civil aviation at the first half year 2014
. Inspection Safety Fly Department of the Federal Aviation Agency Russian Federation
(2014
).4.
V. N.
Poshjdaev
, Reduction and back-scattering of the millimeter's radio waves at fog, rainfall, snowstorm, IV Russian conference «Radar engineering and radio communication»
– Institute Radio Electronics RAS
, 29 Nov-3 Dec 2010, pp. 744
–748
.5.
6.
G. B.
Brilev
et al, Radar features of clouds and precipitations
, Leningrad
1986
, 233
p.7.
R. P.
Bistrov
et al, Estimation of the radar potential abilities and immunity features at radio intercept mode
, Inst. Radio Electronics, Radio electronic journal
№ 8
2015
, ISSN .8.
S.
Orlovsky
et al, Dangerous and very dangerous sandy storms at the Middle Asia, Sectoral Problems for Dry lands Development
, Arid Eco-systems
, 2013
19, № 4
(57
), p.p. 49
–58
.9.
The values ratio and volume weight of building sand
, Builder Manual, Leningrad
1986
, 320
p.10.
A. L.
Jeleznjakova
et al, Aerodynamic calculation of two type models of the landing spacecraft, Institute mechanic problem RAS Moscow, Physical-Chemical gas dynamic kinetics
, www.chemphys.edu.ru/pdf/2010-01-12-025.pdf.11.
A. A.
Kuchurkin
et al, Cheljabinsk State University, Ultra-high frequency diagnostic for the gas-discharge plasma
, Radio Electronics & Radio Physics, Moscow Radio Technology Institute
, 2010
v. 2
, № 3
, p.p. 122
–125
.12.
I. A.
Shevjakov
, About the radio transparency of the hypersonic aircraft's plasma skin, South-Ural State University Messenger, Series
: «Mathematics. Mechanics. Physics»
, 2014
, v. 6
, № 2
p.p. 80
–84
.13.
Helicopter Mi-8MT
, Manual on Technical Operation, 8АМТ-0007-00MTO, Book II, Part 1
, Plane, June 26, 1995
, 324
p.14.
G. A.
Timofeev
, N. N.
Potrakhov
, A. I.
Nechaev
, Experimental researches of the X-ray communication channel, V Russian science-practice conference for X-ray producers, Conference Thesis's
, Saint Petersburg State Electrotechnique University “LETI”
, 2019
p. 97
.
This content is only available via PDF.
© 2020 Author(s).
2020
Author(s)
You do not currently have access to this content.