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  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Development of a Helical and Pigtail-Based Range Extension System for Campus Surveilance Quadcopter</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>M. Saidu</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Elizabeth N. Onwuka</string-name>
          <email>onwukaliz@futminna.edu.ng</email>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>A. M. Aibinu</string-name>
          <email>maibinu@gmail.com</email>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>H. Bello Salau</string-name>
          <email>habeeb.salau@futminna.edu.ng</email>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>F.O. Saliu</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>X. Shemang</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>M. N. Mohammed</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Federal University of Technology</institution>
          ,
          <addr-line>Minna</addr-line>
          ,
          <country country="NG">Nigeria</country>
        </aff>
      </contrib-group>
      <pub-date>
        <year>2016</year>
      </pub-date>
      <fpage>227</fpage>
      <lpage>231</lpage>
      <abstract>
        <p>-A Quadcopter commonly known as a drone is a type of Unmanned Aerial Vehicle (UAV) that is lifted and propelled by four (4) rotors. They usually come with a control pad and LCD screen receiver that receives videos and photographs from the quadcopter while aloft. The major problem faced by UAVs is the communication range limitation between the drone and its ground control station. Generally, the longer the range, the larger the UAV coverage, and in turn, the more productive. In this work, a range extender system was constructed and used to extend the communication and control range of a campus surveillance drone. To achieve this, the quadcopter was coupled and many field trials were conducted for the purpose of understanding its flight mechanism and to empirically measure its range. However the average communications range between the quadcopter and its control pad was 108 meters. In order to increase this range, range extender system was constructed. It consists of a pigtail antenna for extending the control and video transmission range, and a helical motorized antenna for extension of the flight range. Flight trails and empirical measurements at the Federal University of Technology Minna campus showed that the communication range of the UAV was extended by 200 meters.</p>
      </abstract>
      <kwd-group>
        <kwd>-surveillance quadcopter</kwd>
        <kwd>communication range</kwd>
        <kwd>control station</kwd>
        <kwd>pigtail antenna</kwd>
        <kwd>helical antenna</kwd>
        <kwd>range extender</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>INTRODUCTION</p>
      <p>
        An Unmanned Aerial Vehicle (UAV), known commonly
as a drone is an airplane without a human pilot on board. Its
flight is controlled either autonomously by computers in the
vehicle, or under the remote control of a pilot on ground or
in another vehicle [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ]. The vehicles are developed purposely
to operate in regions where the presence of an on-board
human pilots is either unnecessary or too dangerous. UAVs
have prospective applications in military for recognition,
environmental observation, and maritime surveillance. Other
non-military applications of UAVs are environmental and
infrastructure surveillance among others [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ]. A quadcopter is
a type of UAV with four (4) rotors which pushes air
downwards, thus, creating a thrust force keeping the vehicle
on air. It usually has a control pad with LCD screen which is
used to control its speed, direction, and flip motion. The
LCD screen receiver receives aerial videos and photographs
which were taken by the camera mounted on the Quadcopter.
This camera has a pigtail antenna mounted on it which
transmits videos and photographs captured to the LCD
screen receiver at the ground control station.
      </p>
      <p>
        One of the serious challenges of any UAV, especially in
surveillance applications, is the short communication range
between the Quadcopter (transmitter) and the LCD screen
(receiver). The longer the communication range between
devices and their controls, the more efficient the output and
also more conveniently they can be remotely operated [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ].
This challenge can be overcome by a variety of techniques,
which include the use of a Wi-Fi repeater, and increment of
the strength of the transmitter antenna among others. Wi-Fi
repeater, which could also be called a wireless range
extender/booster, is a wireless repeater that extracts signal
that already exist from a wireless router and rebroadcasts it
to create a second network. On the other hand an antenna is
an electrical device that converts electric power to radio
waves and coverts radio waves back to electrical power.
Helical antenna is a passive radio frequency signal booster
that uses the principle of convergence of RF signals at the
focal point of reflective parabolic object, which increases the
transmission and reception signal range. Pigtail antenna
usually has a high frequency coupling device called
PIGTAIL that enables the antenna to be mounted to the
circuit [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ].
      </p>
      <p>In this work, we used both helical and pigtail antennas to
extend the communication range between the quadcopter and
its control pad at the ground station. Firstly, various parts of
the quadcopter were coupled together and tested several
times in the field to understand its principle of operation and
also to determine its maximum average communication
range. The antenna inside the control pad and the LCD
screen of the quadcopter were then extended using a pigtail
antenna. Helical antenna was also constructed and the cable
from the antenna was then connected to the pigtail antennas
on the control pad and the LCD with the aid of connectors.</p>
      <p>The rest of the paper is organized as follows: Literature
review is presented in section 2. Methodology of the work is
described in section 3. Test and Result is presented in
section 4, while, section 5 concludes the paper.</p>
      <p>II.</p>
      <p>LITERATURE REVIEW</p>
      <p>
        In recent years, development of UAVs has become a
significant growing segment of global aviation industry.
These vehicles are purposely developed to operate in various
applications where human intervention is dangerous or
considered difficult [
        <xref ref-type="bibr" rid="ref3">3</xref>
        ]. The first flying quadcopter was
invented by Etienne Oehmichen in 1922 in order to run
“Wireless Control Quadcopter with Stereo Camera and Self
Balancing System” research. Several theory and techniques
were reviewed from previous related research report. The
reviews includes the technological development and control
methods used in the development of the quadcopter. The
inputs are usually the desired values of the height, roll, pitch
and yaw. While the outputs are the power of each of the four
rotors that is necessary to reach the specifications. The first
recorded construction of a quadcopter was in the same year
when Georges De Bothezat and Ivan Jerome fabricated and
flew the Quadcopter. The quadcopter was to a certain extent
large and used variable-pitch propellers for control. This
project sponsored by the United State army was cancelled
when the quadcopter proved difficult to fly and the military
became more interested in autogiros. Later in 1956, another
more successful quadcopter was built and flown by designer
D. H. Kaplan [
        <xref ref-type="bibr" rid="ref4">4</xref>
        ][
        <xref ref-type="bibr" rid="ref5">5</xref>
        ].
      </p>
      <p>Quadcopter exists in different sizes ranging from as small
as size of a compact disc (CD) up to something big as one
(1) meter in width. Larger quadcopters need larger motors
which, in turn, have larger inertias and cannot be controlled
as quickly as smaller motors. As the size increases to a
certain level, the quadcopter can no longer be stabilized
through RPM control alone because the torque required to
quickly change the rotational velocity of the motor exceeds
the capacity of the motor. Therefore, variable-pitch blades
become essential for larger quadcopters merely for
stabilization purposes</p>
      <p>
        The longer the communication range between devices
and their controls, the more efficient the output and also the
more conveniently it can be remotely operated. The
communication range between quadcopter and its control
pad could be extended through the use of Wi-Fi repeater and
increment of the length of the transmitter antenna [
        <xref ref-type="bibr" rid="ref6">6</xref>
        ]. A
WiFi repeater which could also be called a wireless range
extender or wireless range booster is a wireless repeater that
extracts signal that already exists from a wireless router and
rebroadcasts it to create a second network. When two or
more hosts have to be connected with one another and the
distance is too long for a direct connection to be established,
a wireless repeater is used to bridge the gap. Wi-Fi repeater
has been used to extend the range of communication between
the quadcopter and its control station by taking a signal that
already exists and rebroadcasting that same signal thereby
creating a second network. [
        <xref ref-type="bibr" rid="ref6">6</xref>
        ].
      </p>
      <p>Radio repeater is a type of wireless repeater used to
extend the range of coverage of a radio signal. It usually
consists of a radio receiver connected to a radio transmitter.
The received signal is amplified and retransmitted, often on
another frequency to provide coverage beyond the initial
range, without any alteration to the signal.</p>
      <p>
        An antenna or an aerial is an electrical device that
converts electric power to radio waves and from radio waves
back to electrical power. Radio waves are electromagnetic
waves which carry signals at the speed of light through the
air or space with almost no transmission loss before getting
to its destination (the receiver). They are commonly used
with radio transmitters and radio receiver. In order to
transmit signal using an antenna, a radio transmitter supplies
an electric current oscillating at radio frequency (RF) to the
terminal of the antenna. The energy from the current
supplied by the radio transmitter is radiated as
electromagnetic waves/radio waves by the antenna and
during reception, an antenna intercepts some of the power of
an electromagnetic wave thereby produce a tiny voltage at its
terminals. This voltage produced at the terminal of the
intercepting antenna is applied to a receiver to amplify it.
Antennas can be used for a large variety of equipment that
uses radio such as radio broadcasting, television
broadcasting, telephones, radar, communications receivers,
satellite communications, wireless microphones, and
Bluetooth enabled devices among others. [
        <xref ref-type="bibr" rid="ref7">7</xref>
        ][
        <xref ref-type="bibr" rid="ref8">8</xref>
        ]
      </p>
      <p>The focus of this work is extension of communication
and flight range of a campus surveillance UAV. A range
extension system consisting of pigtail antennas, and
motorized helical antennas was developed to achieve this
purpose. The methodology used in doing this is discussed in
the next section.</p>
      <p>III.</p>
      <p>METHODOLOGY
The methodology employed in this work is in three fold,
which is described in three (3) subsections, which are;
coupling of the quadcopter parts, extension of the UAV
control and video transmission range with pigtail antennas
and the construction of the motorized helical antenna for
extension of the UAV flight range.</p>
      <p>A. Coupling of the Quadcopter Parts.</p>
      <p>The drone used in this work came as experimental
chassis parts, which were then assembled together to give a
complete quadcopter system. The snap-shot of the assembled
system is shown in plate 1. These parts include camera,
propeller guide, propeller and Quadcopter stand among
others. The control pad and LCD screen constituted the
control system at the ground station. The assembled system
was taken to the field and tested several times with the aim
of understudying the principle of its flight operation and also
to understand the control mechanism. The maximum
average communication range between the quadcopter and
its control system at the ground station was also determined
empirically during these fields.</p>
      <p>B. Extension of the UAV Control and Video Transmission</p>
      <p>Range with Pigtail Antenna.</p>
      <p>In other to extend the communication range between the
quadcopter and its control pad, the length of the antenna in
both the control pad and LCD screen pad of the system were
increased. We opened both the control board and the LCD
screen and soldered 2cm of a 2.4 GHz Pigtail antenna to the
length of the antennas found inside the two components.
This antenna is described as pigtail because it has a high
frequency coupling device called PIGTAIL, which enabled
us to mount the antenna to the circuit. The end of the pigtail
antenna in both the LCD screen and the control pad were
connected to a female connector, the snapshot of this
connection is shown in plate 2 and 3 respectively.
Plate 1. The assembled Quadcopter
Plate 2. Pigtail antenna on the control board
C. Construction of the Helical Antenna for extension of the
UAV Flight Range.</p>
      <p>A helical antenna is a spring with N turns made up of a
conducting wire wound in the form of a helix with a
reflector. Helix dimensions is determined by the wavelength
(λ) which also depend on the frequency (F) of the radio wave
used as shown in the following equations.</p>
      <p>λ = 0.3/Ϝ ………………………………. (1)
D = λ/π ………………………………… (2)
C = Dπ …………………………………. (3)
d = C/4 ……………………………….... (4)</p>
      <p>
        Where „F‟ is the operating frequency (2.4 GHz), D is the
diameter of a turn, „C‟ is the circumference of a turn and„d‟
is the approximated space distance between the turns. To
obtain a circular polarization around the axis, the
circumference (C) of a turn must be approximately one
wavelength (λ) and size of the reflector (R) is equal to C or
λ.[
        <xref ref-type="bibr" rid="ref11">11</xref>
        ][
        <xref ref-type="bibr" rid="ref12">12</xref>
        ]
      </p>
      <p>The materials we used in the construction of the helical
antenna based on the values obtained from the equations are
shown in plate 4. Two 40 cm PVC pipes were used and the
wires of a coaxial cable were wounded around the pipes
making use of 12 numbers of turns at a distance of 3.3cm to
produce the helical antenna. The wire has a colorized PVC
isolation and the slight difference in D of 42 mm as against
the calculated 39.3 mmisdue to the thickness of the isolation.
The calculated 132 mm of C obtained is 1.07 of λ. The two
helical antennas constructed were placed on an RC reflector
which was curved in order to focus the energy in one
direction.The Helical antenna was then placed on a Dual axis
motorized stand, which is connected to a gear box used in
controlling the direction of the Dual axis motorized stand.
The stand is powered by a 12 V D.C battery by connecting
the cable from both motors on the stand to it. The snapshot
of the constructed helical antenna on dual axis motorized
stand is shown in plate 5, while, the snapshot of the entire
UAV extender system is shown in plate 6. This antenna
extends the flight range of the quadcopter in a given
direction.</p>
      <p>Plate 3. Pigtail antenna on LCD screen receiver.</p>
      <p>Plate 4. Materials for Helical Antenna
Plate 5. The helical antenna mounted on the Dual axis motorized stand
Plate 7a. FUT Minna, Senate Building Road
Plate 6. UAV extender system
Plate 7b. FUT Minna, Research Farm
IV.</p>
      <p>RESULT AND DISCUSSION</p>
      <p>The complete project work shown in plate 6 was taken to
a field in campus for test and evaluation. The quadcopter
crash landed several times at the early stage of the test.
However, after several trails, all the commands sent to the
quadcopter from control pad, such as flipping, trimming,
hopping, taking aerial video and photographs were well
executed. Since the flight extender is a directional antenna,
while the Quadcopter is on flight, the helical antenna points
in the direction in which it flies by using the buttons on the
gear box connected to the antenna to control the Dual axis
motorized stand in the up or down, left or right directions.</p>
      <p>Plates 7 (a), (b), (c) and (d) show some of the aerial
photographs taken by the quadcopter while aloft in campus.</p>
      <p>Plate 7c. FUT Minna, Academic Publishing Center</p>
      <p>The initial average communication range between the
quadcopter and its control pad was measured after several
field trails to be 108 meters. However, with the introduction
of the Pigtail/Helical Antennas, the new average
communication range was measured after several field trails
to be 308 meters line of sight. It was observed that while a
great distance was achieved, the battery capacity reduced
from 5 minutes to 3 minutes due to the amount of power
being consumed by the antennas.</p>
      <p>V.</p>
      <p>CONCLUSION</p>
      <p>In this work an experimental chassis parts of a
UAVquadcopter was assembled. Knowing that one of the
challenges of most UAVs is inadequate communication
rangebetween the vehiclesandtheir control pad, field trials
were conducted for the purpose of studying the operating
principle and to empirically determining the range. The
averagecommunicationrange of the UAV was measured after
several field trials to be 108 meters. A range extension
system, consisting of pigtail antennas and motorized helical
antenna was developed to extend the communication and
flight range of the UAVquadcopter. Field tests with the
developed system at the Federal University of Technology
(FUT) Minna air space showed that the communication
range was successfully extended by 200 meters. This means
that the new communication range was measured to be
averagely 308 meters line of sight. The vehicle was therefore
able to gain wider coverage aloft and videoed and
transmitted very clear aerial images of the areas covered.
This shows that campus surveillance can be better achieved
with the UAV. However, considering the size of this
campus, multiple UAVs may be employed for complete
surveillance.</p>
    </sec>
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