<!DOCTYPE article PUBLIC "-//NLM//DTD JATS (Z39.96) Journal Archiving and Interchange DTD v1.0 20120330//EN" "JATS-archivearticle1.dtd">
<article xmlns:xlink="http://www.w3.org/1999/xlink">
  <front>
    <journal-meta />
    <article-meta>
      <article-id pub-id-type="doi">10.3390/electronics9040668</article-id>
      <title-group>
        <article-title>Optimal Configuration and Typical Size of Images Received by Unmanned Aerial Vehicles during Monitoring</article-title>
      </title-group>
      <contrib-group>
        <aff id="aff0">
          <label>0</label>
          <institution>National Aviation University</institution>
          ,
          <addr-line>Kyiv</addr-line>
          ,
          <country country="UA">Ukraine</country>
        </aff>
      </contrib-group>
      <pub-date>
        <year>2018</year>
      </pub-date>
      <volume>9</volume>
      <issue>3</issue>
      <fpage>22</fpage>
      <lpage>24</lpage>
      <abstract>
        <p>This article is devoted to develop a fundamentally different method of forming the image structure during the UAV`s monitoring. The mechanism of solving the problems of constructing optimal configurations and standard sizes of raster elements or pixels on displays in the process of processing or correcting images at the present stage of science development is an actual problem. New methods proposed to improve the quality and reliability of environmental pollution. These studies dedicated to reducing the weight of an unmanned aerial vehicle visualization system, as well as increasing the number of color shades of the environment to improve image quality. The first developed method for forming the raster elements of the UAVs based on a research algorithm, which considers a ratio of the golden section with the scale of light perception.</p>
      </abstract>
      <kwd-group>
        <kwd>raster elements</kwd>
        <kwd>unmanned aerial vehicle</kwd>
        <kwd>geographic information systems</kwd>
        <kwd>monitoring process</kwd>
        <kwd>golden section</kwd>
        <kwd>light perception scale</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>Under the conditions of increasing high and anthropogenic influence on the nature the
existing ecological reserve of the biosphere should be used with special attention.</p>
      <p>The regimes of the limited cost of this reserve, the regulation of the state of the
environment which ensure the preservation of high-quality biosphere and the ability
of nature to reproduce must be scientifically defined. Hence, at the time, there are
various exhaust devices and knowledge of monitoring the factors affecting the
environment and the state of the environment.</p>
      <p>Active inspection of large land and water surfaces, including for environmental
monitoring, is made using aviation complexes based on airplanes, helicopters or
probes, as presented in (Fig. 1). In the world directions for the use of aircraft on
artificial intelligence unmanned aerial vehicles (UAV) are intensively developed for
several years.
Active inspection of large land and water surfaces, including for environmental
monitoring, is made using aviation complexes based on airplanes, helicopters or
probes, as presented in (Fig. 2). In the world directions for the use of aircraft on
artificial intelligence (unmanned aerial vehicles) are intensively developed for several
years. These technologies have a number of advantages, do not require specially
prepared platforms and launch complexes, they are relatively cheap, relative to large
air complexes, and are not risky for humans.</p>
      <p>The largest development and, as a result, the distribution in the world received
UAVs of the winged or airplane type.
2</p>
    </sec>
    <sec id="sec-2">
      <title>Literature Analysis and Problem Statement</title>
      <p>The monitoring of air and ground conditions by the UAV is connected with the
review of a certain region and the reception of high-quality and reliable visual
information by means of photo, television and video systems, and preserving it on an
on-board drive. During the flight in a given region, the UAV tracks environmental
pollution and other types of consequences of environmental disasters with a view to
transmitting environmental information images on a real-time radio channel. The
UAV`s video system recognizes visual information and identifies its individual details
using various methods, and transmits it to the ground module of the communication,
control, processing and correction of visual information system.</p>
      <p>The localization and liquidation on land and inland areas of oil and oil spills were
considered in the study. The work is carried out by a professional emergency rescue
unit, which has all kinds of modern equipment and worked-out quick reaction
algorithms (Fig. 3 a, b), but does not have a modern restore (correction) system of the
received image.</p>
      <p>a b
Fig. 3 (a, b). Localization and liquidation of oil and petroleum products spills on land
and inner harbor in Ukraine.</p>
      <p>Diminutiveness and manufacturability of information visualization electronics allows
to create both miniature and quite large aircraft complexes with a wide range of
possibilities, from simple photo and video monitoring in the visible spectrum and
ending with the equipment of thermal imaging and laser devices. The small unmanned
systems in terms of quality comply with the highest standards. The works carried out
with application of small unmanned systems allow them to be recommended for
obtaining scientific data - remote environmental monitoring using ultralight aircraft
for the needs of the national economy of Ukraine, but the quality of the images
received does not correspond to the current requirements.</p>
      <p>
        Literature analysis [
        <xref ref-type="bibr" rid="ref1 ref2 ref3">1-3</xref>
        ] that global development experience in the field of remote
environmental monitoring is based either on space data and on the use of large
aviation, or on the use of small-scale unmanned systems. Satellite observing systems
allow monitoring of large areas based on the processing of multispectral images using
Geographic Information Systems (GIS) technologies. But to obtaining new
information products in the form that specific users are dealing with (for example, the
volume of biomass in forest, agriculture and other ecosystems at the moment of
exposure) is necessary.
      </p>
      <p>Negative factors in the use of UAVs and their visualization systems were also
analyzed:</p>
      <p>1. At the moment, the development of the civilian UAVs market, including UAVs
for aerial photography, is hampered by the lack of a regulatory framework for the
integration of UAVs into a single airspace. The problem of correction of visualization
of the environment on the basis of modern theory is also not been solved completely
in any country in the world.</p>
      <p>2. Increased UAV`s accidents. At the moment, the UAVs are not equipped by a
system for identifying obstacles and collision avoidance, in addition, many models are
equipped with imperfect autopilots (to reduce the cost and the weight of on-board
equipment). The risk of loss of craft and equipment leads to the fact that many
companies may want to buy not UAVs, but flight hours from organizations that
specialize in unmanned launches.</p>
      <p>3. The high cost of UAV, which is associated with the development of flight
systems and high-tech concept providing a "meaningful flight", i.e. similarity to
artificial intelligence.
3</p>
    </sec>
    <sec id="sec-3">
      <title>Setting objectives</title>
      <p>
        Performance of the main study material with a full substantiation of the scientific
results obtained is done in [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ]. It is known [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] that for the simultaneous establishment
of a gyrostabilized photoplatform for aerial photography by the UAV in two spectra
(visible - 0,4-0,8 μm and infrared - 0,8-1,1 μm), result is the poor image quality that
does not correspond to the criteria for comfort perception by the human eye. The
received visual information can not be used for cartography and further application in
geodetic and topographical works. Fixing the corners and coordinates of shooting
UAV`s drift, its adjustment for the windshift are built in the abilities of platform, but
there are such distortions like moiry when printing on a paper or film. The capabilities
of the UAV`s camera allow the exploration of thermal maps of the earth and water
surface up to 0.05°C, but economically it is not profitable.
      </p>
      <p>
        Small-scale aerial photography, as a kind of remote ground sensing by UAV, is not
a compromise between the ideal technical and financially available aerial
photography because the quality of the images (Fig. 4) does not correspond the
criteria for comfortable perception by the human eye. It is known [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ] that there are
three types of aerial photography available.
      </p>
      <p>For the first time, has been developed a method to facilitate solving an issue. The
results of experiments show that vertical UAV`s images are generally better for
measuring and compiling the characteristics of regions, because the geometry of
vertical images can be calculated in the form of mathematical models of images.
However, this type of shooting of the UAV is difficult to perceive and interpret for
people who are not familiar with the region itself, and with the subtleties of
processing. The shooting of the UAV is made with a significant angle to the horizon
(Fig. 5), that is, the view aerial photography, gives a good overview and is easily
perceived by most people. However, there is a significant disadvantage - a significant
distortion in geometry, which will result in inaccurate measurements and unreliability
of information. As a result of shooting the UAV (Fig. 5), we get the output:</p>
      <p>The UAV`s control system and its image visualization and correction system
should include a ground and airborne equipment. The ground equipment includes a
personal computer with specialized software installed, observing, analyzing,
processing and synthesizing images blocks and GSM/GPRS modem for receiving
telemetry and transmitting control information. The on-board equipment consists of a
GPS/GLONASS receiver, an inertial system, an integrated system, an onboard
computer MC26, GSM/GPRS modem and special equipment for monitoring, analysis,
processing, synthesis, identification and correction of images obtained using UAV.</p>
      <p>
        The latest researches analysis, which initiated the resolution of image quality
problems [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ] of the environmental monitoring of the UAV, the separation of
previously unsettled parts of the general problem, as established, is based on the
secrets of antiquity. It is known [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ] that Flemish artist Rubens wrote about the
repetition of the triangular shape in parts of the human body.
      </p>
      <p>But for some reason, there are practically no optimal triangular configurations PE
(Fig. 4a) for UAV, although the calculation of their configurations is not complicated
and is determined by a mathematical model
(а)
(b)
(c)
(d)
(e)
(f)
(g)
circles; d </p>
      <p>2a is the square`s diagonal; p, h, m – half-perimeter, altitude of a triangle and
medial line.</p>
      <p>
        Therefore, in modern UAV`s monitoring [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ], it is proposed to use it on the basis of
rectangular, square and other RE (fig. 4a, b, c, d, e, g), while the image of the
4nvironmental state of the environment is created, then their mathematical models
have the form
      </p>
      <p>
        A mathematical model for calculating the trapezoidal [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ], parallelogram and other
PE in the general form is determined
      </p>
      <p>S  ab,</p>
      <p>S  a2 ,</p>
      <p>S  ah.</p>
      <p>Such approaches are valid for circular, irregular, mezzotint and other raster
elements (RE) (fig. 4a, b, c, d, e, f, g). But their calculation takes place without any
proportions, a priori, and it is quite impossible to determine optimal configurations,
size, area and with what optimum step of zooming should be change of the
construction of large modular screens (video wall).</p>
      <p>
        The first developed method for assessing image quality [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] of the UAV. The
effectiveness of the solution of each of the monitoring tasks estimated by the relevant
partial criterion. It is known [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] that M. Reber also found in the pyramid not only the
formula of the golden section φ = 1.618 ..., but also the value of the single wurf Δ1 =
1.309 ... and the double wurf Δ2 = 2.618. It is established that this pyramid serves as a
mapping projection on the scale 1: 43200 of the northern hemisphere of the Earth,
demonstrating through the number 2π that the pyramid is a large-scale model of the
Earth. The Egyptians [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ] explicitly used standards with the numbers of the golden
section α = 1.618, the numbers π = 3.14, the double wurf Δ2 = 2.618 and the single
wurf Δ1 = 1.309. Numerical interdependence in the construction of all pyramids, their
configuration and standard sizes is not accidental, but the optimal system of
configurations and standard sizes, connected with the development of life and the
Earth, used for the formation of RE. This determines the connection of the proportion
φ with the number π
      </p>
      <p>  
  2 cos   .</p>
      <p> 5 
(2)
(3)
(4)</p>
      <p>
        The two quantities π, φ are related by simple relations and can be expressed in
terms of the ratio of integers in the Fibonacci series [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ]. This testifies to their organic
unity and their fundamentality [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ], as established.
      </p>
      <p>
        Main study material presentation with a full substantiation of the scientific results
obtained is in [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ]. It is also known [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] that Fechner found that the ratio of the pictures
taken in European museums over 400 years does not correspond to the generally
accepted golden section that they are not equal to arbitrary numbers, but to invariant
waves α, β, γ, δ, ρ, σ and θ with an error of less than one percent. Knowledge of
psycho-physiological features of a person's view enables the introduction of the
developed criterion k as the image in the process of monitoring the ecological
situation of the UAV, to clarify the Weber-Fechner's law
B
B
      </p>
      <p>k  ,
where ψ is the relative threshold or the marginal eye contour.
4</p>
    </sec>
    <sec id="sec-4">
      <title>Problem solving hypothesis</title>
      <p>
        For the first time, was established the nature of the golden section for the
determination of images, which allows us to assess the extent to which the goal [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ]
reaches the researcher to evaluate the quality of the images, taking into account
factors that pour into the monitoring of the UAV. The results of studies are confirmed
in [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ] statistics of Fechner and the data of A. Sokolov [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ], which were used in the
work after clarification from (Table I).
      </p>
      <p>
        The scientific result obtained on the basis of the application of the theory of
processing PE and image pixels and the scientific-methodical apparatus of the study is
presented in [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ] is that the universal configuration and calculation of standard sizes of
PE and pixels that can be automatically scaled and transformed into rectangular,
square, triangular, and so on PE and pixels. The relative area of the PE in the given
area of the image can be determined taking into account the corrections made
(5)
(6)
(7)
(8)




where k = ctg α,  
,  
      </p>
      <p>
        are information from source [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ].
      </p>
      <p>The ways of solving the monitoring problems for the formation of the most
optimal scaling factor and its calculations in practice in the processing of images of
monitoring of the environment of the UAV are proposed.</p>
      <p> 1  i
S  k 2    Si  L2 ,</p>
      <p> n  i0
ak  al 101/ g (k 1) ,</p>
      <p>  aek ,
where kΔ2 is table transfer coefficient in step Δ2 = 2.618; Si, L, n is the area, linearity and the
number of measured REs or pixels.</p>
      <p>
        The analysis of the regularities of the change in parameters showed that their
value can be determined by the formula of geometric progression [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] and by law the
spiral
where a1, k is initial value and sequence number RE in the sequence; σ = 1 / g - indicator of
progression, which depends on the set of values, RE.
      </p>
      <p>
        In this way, as shown in [
        <xref ref-type="bibr" rid="ref5">5</xref>
        ], the progression should be not only geometric, but
also arithmetic for the calculations of PE and be similar to the Fibonacci series, but in
the form of a logarithmic spiral in polar coordinates ρ
 d   k2   L
      </p>
      <p> Rop 
M  k 2   dop  
p </p>
      <p>(9)
(10)</p>
      <p>Thus, in solving problems, we denote by φρ (n) the numerical series of Fibonacci
numbers, where n = 1, 2, 3 ... the numerical number of the series and with the number
of steps ρ = 1, 2, 3 .., then from these considerations for n&gt; p [] the following
recurrence relation follows:</p>
      <p> p (n)   p (n 1)   p (n  p 1)</p>
      <p>
        The introduction of the proposed above criterion for the quality of environmental
images for the assessment of the UAV monitoring process [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ] put forward additional
requirements regarding the minimum number of partial criteria and the completeness
of the definition of the essence of the process. This opens up one of the sides of the
problem of processing, correcting and comfortable perception of images in the
process of monitoring the UAV at the expense of optimal sizes and configurations PE
and pixels.
The above established mathematical connection is implemented as a content of the
Atlas of the sizes of RE and pixels in the fragment (Table I). To test the developed
problem solving algorithm [
        <xref ref-type="bibr" rid="ref3">3, 23-26</xref>
        ] a program has been developed that will form the
Atlas content for the calculation of, for example, 512 squares, configurations and
standard sizes of the RE or pixels of the environmental image during the monitoring
of the UAV with a change in the proportion of magnitude Δ2 = 2.618.
      </p>
    </sec>
    <sec id="sec-5">
      <title>Conclusions</title>
      <p>Investigation of the possibility and technical ways of creating an overview
information system for UAV visualization for environmental monitoring led to the
following main results:
1. The UAV expediency for ecological monitoring is shown.</p>
      <p>2. In the presence of on-board equipment of UAVs, it is expedient to use the
system of preliminary correction of images on the basis of modern theory with
environmental monitoring.</p>
      <p>3. Investigation of the features of the UAV visualization system in the ecological
monitoring zone showed that:</p>
      <p>- the research was conducted for the optimal size of the review area and from
1020x1020 to 1040x1040 elements of the resolution of the display.</p>
      <p>The conclusions and perspectives of further research in the scientific direction of
processing of environmental images are that for the first time an unconventional
approach to solving the problems of creating and calculating the ratio of areas,
configurations and standard sizes of each PE image using π, φ and the step of
changing the proportions to the value of the double warp Δ2 = 2.618. Changes in
proportions are clearly expressed in (Table 1) did not attract the attention of
researchers and specialists because the phenomenon reflected in them was not taken
into account and was not used. Now this table has found real meaning and meaning.
And Atlas's development of optimal configurations, sizes and areas of PE and pixels
will allow you to explain many of the accumulated problems in the field of
environmental image processing and solving problems in fundamental research on a
new and higher level understanding of the processes taking place in the monitoring by
the UAV.</p>
    </sec>
  </body>
  <back>
    <ref-list>
      <ref id="ref1">
        <mixed-citation>
          1.
          <string-name>
            <surname>Kharchenko</surname>
            ,
            <given-names>V.P.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Kuzmenko</surname>
            ,
            <given-names>N.S.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Ostroumov</surname>
            ,
            <given-names>I.V.</given-names>
          </string-name>
          :
          <article-title>Identification of unmanned aerial vehicle flight situation</article-title>
          .
          <source>In: 2017 IEEE 4th International Conference on Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)</source>
          , pp.
          <fpage>116</fpage>
          -
          <lpage>120</lpage>
          , Kyiv, Ukraine,
          <year>2017</year>
          .
        </mixed-citation>
      </ref>
      <ref id="ref2">
        <mixed-citation>
          2.
          <string-name>
            <surname>Hryshchenko</surname>
            ,
            <given-names>Y.</given-names>
          </string-name>
          :
          <article-title>Reliability problem of ergatic control systems in aviation</article-title>
          .
          <source>In: IEEE 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)</source>
          , Kyiv, Ukraine, pp.
          <fpage>126</fpage>
          -
          <lpage>129</lpage>
          ,
          <year>2016</year>
          .
        </mixed-citation>
      </ref>
      <ref id="ref3">
        <mixed-citation>
          3.
          <string-name>
            <surname>Solomentsev</surname>
            ,
            <given-names>O.V.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Melkumyan</surname>
            ,
            <given-names>V.H.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Zaliskyik</surname>
            <given-names>M.</given-names>
          </string-name>
          <string-name>
            <surname>Yu</surname>
          </string-name>
          .,
          <string-name>
            <surname>Asanov</surname>
            ,
            <given-names>M.M.:</given-names>
          </string-name>
          <article-title>UAV operation system designing</article-title>
          .
          <source>IEEE 3rd International Conference on Actual Problems of Unmanned Air Vehicles Developments (APUAVD)</source>
          , Kyiv, Ukraine, pp.
          <fpage>95</fpage>
          -
          <lpage>98</lpage>
          (
          <year>2015</year>
          ).
        </mixed-citation>
      </ref>
      <ref id="ref4">
        <mixed-citation>
          4.
          <string-name>
            <surname>Odarchenko</surname>
            ,
            <given-names>R.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Polihenko</surname>
            ,
            <given-names>O.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Kharlai</surname>
            ,
            <given-names>L.</given-names>
          </string-name>
          ,
          <string-name>
            <surname>Tkalich</surname>
            ,
            <given-names>O.</given-names>
          </string-name>
          :
          <article-title>Estimation of the communication range and bandwidth of UAV communication systems</article-title>
          .
          <source>In: IEEE 4th International Conference on Actual Problems of UAV Developments (APUAVD)</source>
          , pp.
          <fpage>159</fpage>
          -
          <lpage>162</lpage>
          , Kyiv,
          <year>Ukraine 2017</year>
          .
        </mixed-citation>
      </ref>
      <ref id="ref5">
        <mixed-citation>
          5.
          <string-name>
            <given-names>O.U.</given-names>
            <surname>Bondar</surname>
          </string-name>
          ,
          <string-name>
            <given-names>O.I.</given-names>
            <surname>Fedorenko</surname>
          </string-name>
          and
          <string-name>
            <given-names>A.V.</given-names>
            <surname>Kudin</surname>
          </string-name>
          . Fundamentals of Ecology: Pidruchnik, - Kyiv: Knowledge,
          <year>2006</year>
          , 543 p.
        </mixed-citation>
      </ref>
      <ref id="ref6">
        <mixed-citation>
          6.
          <string-name>
            <given-names>Le</given-names>
            <surname>Ki</surname>
          </string-name>
          <article-title>Bien. The choice of an unmanned aerial vehicle for environmental monitoring of coastal areas</article-title>
          .
          <source>Proceedings of BGTU "</source>
          <string-name>
            <surname>VOEN-MEH" D.F.Ustinova</surname>
          </string-name>
          .
          <article-title>Design issues of control systems for unmanned aerial vehicles for environmental monitoring</article-title>
          ,
          <source>St. Petersburg, BGTU</source>
          ,
          <year>2003</year>
          , pp.
          <fpage>35</fpage>
          -
          <lpage>40</lpage>
          .
        </mixed-citation>
      </ref>
    </ref-list>
  </back>
</article>