.


85 http://journals.cihanuniversity.edu.iq/index.php/cuesj CUESJ 2019, 3 (2): 85-91

ReseaRch aRticle

A Multiband Biconical Log-periodic Antenna for Swarm 
Communications
Bessam Al Jewad*

Department of Computer and Communication Engineering, Cihan University-Erbil, Kurdistan Region, Iraq

ABSTRACT

In this paper, we present a specific multiband antenna design that addresses the problem of communication with unmanned aerial 
vehicles (UAVs). We consider a scenario where multiband single-antenna UAV communicates with the rest of the swarm members that 
are equipped with similar antennas. The key point in the design is that the communication does not require high or low elevation angles 
in most of the cases. The suggested design has a sufficient degree of freedom to select the desired features for the field pattern while 
keeping other features such as antenna impedance and gain relatively stable or at least in the acceptable operation region.

Keywords: Biconical antenna, broadband antenna, component, drone-to-drone, drone-to-infrastructure, frequency-independent 
antennas, log-periodic antenna

INTRODUCTION

In recent years, the use of unmanned aerial vehicles (UAVs), also known as drones, has witnessed an unprecedented increase for both military and civilian applications. From 
airborne traffic surveillance to the more recent mail package 
delivery, the list of interesting applications for UAV swarms 
keeps growing.[1-3] However, the introduction of the swarm 
concept, communications have always been a challenge.[4,5] In 
UAV swarms, there are two types of communications: Drone-
to-drone (D2D) in which drones can communicate important 
navigational information between each other, and drone-to-
infrastructure (D2I) in which drones can communicate and 
take general commands from the ground station (GS). While 
the former can be relatively simple, the latter is much more 
complicated and challenging for many reasons. First, in most 
applications, the UAV is equipped with a high-resolution 
camera sending images and video. Therefore, each UAV 
requires a high-speed low-latency communication link in the 
order of tens of Mbps of bandwidth and few tens of milliseconds 
of latency.[6] That is, of course if such images and videos are 
to be used for any reliable form of navigation or interaction. 
Second due to the dynamic nature of the UAV movement in 
three-dimensional at speeds ranging from 20 m/s to 50 m/s,[6] 
the communication channel with the GS becomes time varying 
with non-stationary noise. It is further hampered by the 
constant loss of the line-of-sight and the change in antenna 
characteristics (radiation pattern, polarization, etc.) as well as 
orientation.

Currently, existing wireless technologies, such as wireless 
fidelity, ZigBee, and XBee-Pro as well as massive multiple-input 
multiple-output (MIMO) and ultra-wideband communication 

were devised for communication with UAVs.[6] However, none 
of these techniques was designed for this particular application 
making them highly unreliable for many practical situations.[7] 
In recent artificial intelligence AI studies, it was suggested 
that navigational information and low-latency interaction or 
decision-making between the UAV and GS can be minimized 
if some form of AI algorithm like swarm guidance algorithm 
was implemented locally on each UAV causing the group 
to have a massive collective processing power.[8] In such an 
application, the general heading command can be sent by 
the GS and the swarm can follow a stochastic general path in 
which each UAV can communicate the obstacles, constraints 
and locally-optimized path solution to the rest of the group.[9] 
Collectively, the group will perform a distributed cost-function 
minimization and will find the optimal path that minimizes 
the time and energy for the swarm.[10] In such an application, 
the design of a special low-cost and ergonomically efficient 
antenna for D2D communication is highly desirable.

At a basic level, a drone swarm is a floating dynamic 
wireless network, commonly known as a wireless mesh 

Corresponding Author: 
Bessam Al Jewad, Cihan University-Erbil, Kurdistan Region, Iraq. 
E-mail: bassam.jawad@cihanuniversity.edu.iq.test-google-a.com

Received: Apr 17, 2019 
Accepted: Apr 19, 2019 
Published: Aug 20, 2019

DOI: 10.24086/cuesj.v3n2y2019.pp85-91

Copyright © 2019 Bessam Al Jewad. This is an open-access article distributed 
under the Creative Commons Attribution License.

Cihan University-Erbil Scientific Journal (CUESJ)



Al Jewad: A multiband biconical log-periodic antenna for swarm communications

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network. A mesh network is a network topology in which each 
node relays data for the network. All nodes cooperate in the 
distribution of data in the network. A mesh network whose 
nodes are all connected to each other is a fully connected 
network. Many studies suggested the use of multi-carrier, 
ultra-wideband or multi-band communication. However, one 
of the limiting factors for such an approach is the antenna.

Many conventional antennas are highly resonant and only 
operate over a bandwidth that represents a few percent’s of 
their center frequency. These narrow bandwidth antennas may 
be entirely satisfactory or even desirable for single-frequency 
or narrowband applications where high gain is required. Wider 
bandwidths are required in D2D communication applications, 
especially as the level of the swarm intelligence and its 
processing power increase. The more sophisticated the applied 
AI algorithm gets, the more it becomes necessary to exchange 
high bandwidth or latency dependent data between swarm 
members. Conventionally, there has been a broad range of 
work on wideband antennas[11-13] for various airborne vehicle 
applications. However, D2D rarely will need to communicate 
at high (or low) elevation angles, especially while flying in 
a swarm. Therefore, a wideband, omnidirectional antenna, 
with low beam-width is proposed as a solution for such an 
application. This antenna needs to be effectively small to 
maintain the weight constraints of the drone design. In 
addition, it needs to be a broadband antenna to facilitate 
exchanging high-bandwidth data.

In this paper, we present a specific antenna design that 
addresses the problem of multi-band communications and has 
a higher degree of freedom in its design to select the desired 
features of the field pattern while keeping other features such 
as antenna impedance and gain relatively stable or at least 
within the acceptable operation region.

WIDEBAND FREQUENCY INDEPENDENT 
ANTENNA

The proposed design is a biconical log-periodic spiral antenna 
whose conceptual image is shown in Figure 1. The goal is to 
create a broadband antenna with center frequencies of 3.9 and 
5.9 GHz and a frequency range of 3.4–10 GHz. The objective 
radiation pattern is a one with high gain at the horizon and 
less gain toward the sky or ground. The reason why an array 
antenna would not work is that arrays are typically narrow 
band. Conventionally, several broadband antennas were 
utilized in the past. However, biconical log-periodic spiral 
antennas have an advantage in that they can operate in two 
main modes: The end-fire axial mode with circular polarization 
and the broadside normal mode with linear polarization. 
Thus, depending on the operating frequency, they can serve 
the dual purpose of D2D and D2I communications. This design 
draws from a range of common antennas including dipoles, 
arrays, spirals, loops, log-periodic, and conical. The aspects of 
these antennas and the amount they are used in the design 
are dependent on the frequency range of operation. In this 
particular design, the cones are actually present just to support 
the wire.[14] However, a multi-layered ferrite material can be 
used inside these cones to adjust the center frequency and 
change the polarization. As will be shown later each part of 
a loop will have a different center frequency, and since Ferrite 

material is narrow band, in general, a multi-layer stack of 
ferrite materials can be utilized depending on the desired 
characteristics from the antenna. The material around the core 
can be filled with dielectrics to enhance the capacitive effect of 
the antenna impedance to adjust the performance.

In general, a broadband antenna is defined by two factors: 
Percentage of center frequency and ratio of operation. The 
percentage of the center frequency is defined by

 

− −
= × = ×100% 100%

*
u l u l

p
cl u

f f f f
F

ff f  (1a) 

while the frequency ratio of operation is defined as the 
ratio of the upper and lower frequencies of operation f

u
 and f

l
.

  
= u

l

f
F

f  (1b)

If the impedance and the pattern do not change 
significantly over about an octave (𝐹=2) or more, we classify 
the antenna as a broadband antenna. To meet the frequency 
independence requirements in a finite structure, the current 
must attenuate along with the structure and be negligible at 
the point of the truncation. For radiation and attenuation to 
occur the charge must be accelerated (or decelerated) and this 
happens when the conductor is curved or bent normally to the 
direction, in which the charge is traveling. Thus, the curvature 
of the spiral provides a frequency-independent operation over 
a wide bandwidth.[12]

Broadly speaking, each arm of this antenna can be 
designed independently and placed strategically to provide a 
set of electrically small loop antenna array elements spaced 
by half wavelength, and excited at the center. Starting from 
one arm the logarithmic (log) spiral is defined in cylindrical 
coordinates by r=αθ or ln(r)=θ ln(α) and is shown in detail 
in Figure 2. The radial distance to a point p on the spiral is 𝑟, 
the angle with respect to the X-axis is 𝜃, and 𝛼 is a constant 
representing the apex angle. The relationship between 𝜃 and 𝑟 
can alternatively be given by θ=tan(β) ln (r).

In both relations, the z is not specified. An important 
control for a log-periodic spiral angle is the relationship for 
the spacing between each loop.[15] To achieve the broadband 
nature, the ratio between the 𝑖th loop spacing 𝑠 and the 
subsequent loop must stay constant. The log-periodic loop 
array seems a reasonable approximation to the spirally 
wrapped wire in our design. The loop diameters increase 
along with the antenna so that the included angle α is a 
constant and the spacings s of adjacent elements are scaled. 
This can also be translated in terms of the height of the loop 
z, which gives:

  

+ +

−

−
= =

−
1 1

1

i i i

i i i

S z z
k

S z z  (2)

where k is some constant. From this equation, it can be 
easily seen that z follows a simple difference equation.

Since the arrangement is logarithmic, it is more convenient 
to let z=mθ. Now to find the height of each loop z

i
 we will 

assume that completes one full rotation for each discrete loop 
and is therefore an integer i times 2π. Thus, the height of the 



Al Jewad: A multiband biconical log-periodic antenna for swarm communications

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ith loop can be written as z
i
 = mi. Therefore, z

i+1
=m(i+1)=mz

i
 

in the same way z
i+1

=m2 z
i-1

. Substituting this in (2) and 
solving for m, we find that m=k for a non-trivial solution and 
therefore z=kθ.

It is fairly reasonable to assume that only a single loop (or 
part of the loop) from the spiral will contribute to the major far-
field component and will have the major current distribution 
according to the frequency of interest. This assumption was 
validated by several simulations. In this sense, the diameter 
for any element n+1 is approximately kn greater than the first 
element, or

   

+ = ≈1
1

nnD F k
D  (3)

where 𝐹 is the frequency ratio from Equation (1); the 
smallest loop in the antenna has a circumference equal to a 
tenth of a wavelength to quantify for the small loop antenna 
definition which gives the constraint for the diameter of the 
first loop. Therefore, the geometric representation for one arm 
of the biconical antenna is given by

   
q q q= =/ tan    , r e z k  (4)

Equations (3) and (4) constitute the design equations 
for one arm of the antenna. Each antenna arm can be placed 
in either a frequency selective biconical construct shown in 
Figure 1 or stacked in a broadband uni-conical construct.

MULTI-BAND ANTENNA MATCHING

In the previous section, the antenna was designed to meet 
several broadband requirements. In general, most self-
complementary broadband antennas have almost constant 
impedance. The problem with most wire antennas (like our 
design) is that the antenna impedance is highly frequency 
dependent. Thus, even though the antenna arm in the previous 
section may have broadband properties, it can only be used 
with a single frequency dictated by the matching network. The 
alternative would be to utilize a broadband matching network 
and in this case, the matching would not be perfect or easy. In 
addition, broadband matching in general means a compromise 
on the antenna gain due to the constant gain-bandwidth 
product constraint.

Using the design equations of the previous section, the 
parameters selected for our design are shown in Table 1. The 
simulation results for the antenna impedance assuming a 
wire gauge of AWG33 are shown in Figure 3 for an input port 
impedance of 50 Ohm.

The approach that was adopted in our matching is the 
dual-band impedance matching where the antenna is matched 
at 3.9 GHz and 5.9 GHz. The same approach can be expanded 
to match any set of frequencies within the band. In this section, 
the approach is introduced. Analyzing the actual antenna 
response on the Smith Chart (from a vector network analyzer) 
is also performed.

The antenna’s frequency response (that is, the reflection 
coefficient Γ) is plotted as a function of frequency on the Smith 
Chart, as shown in Figure 4. The blue curve in this Figure 4 
represents the antenna impedance, plotted on the Smith Chart 

continuously from 3.4 GHz to 6.2 GHz since the rest of the 
frequency response is not required for the matching. The black 
circles indicate the locations on the curve corresponding to 3.9 
GHz–5.9 GHz.

The corresponding VSWR plot for the same impedance 
above is given in Figure 5.

The target is to bring both of the above impedance 
locations to the center of the smith chart with a single 
matching network. To do this, the low band is matched first. 
For this step, use is made of only series capacitors and parallel 
inductors. This is because series capacitors affect lower 

Figure 1: Proposed antenna concept

Table 1: Design parameters for the initial antenna matching circuit

Parameters Values

Circumference ≤λ/10

Low frequency 3.481 Ghz

Large frequency 10 Ghz

β 1.54 radians

Κ 1.235

Radius of wire 0.0899 mm

Number of turns 5

Figure 2: Log-periodic loop array structure



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frequencies more than higher frequencies. Similarly, parallel 
inductors affect low frequencies more than high frequencies. 
As a result, if only those components are used, the low band 
can be matched with minimal effect on the high band. The 
matching is done by calculating the required series and 
parallel impedances by moving on a constant X circle on the 
immittance Smith Chart.

For the lower band matching a series, capacitor will move 
the impedance to intersect the Re[y]=1 circle. By inspection, 
we find that a 0.738 pF series capacitor will move the 3.9 
GHz impedance to intersect the Re[y]=1 circle. From there, 
we complete the low band match with a parallel inductor of 
approximately a 0.692 nH. The resulting impedance curve for 
the group (the antenna, the 0.738 pF series capacitor and then 
the parallel 0.692 nH inductor) is shown in Figure 6.

From this, we see that the low band (3.9 GHz) is moved to 
the center of the Smith Chart, i.e., we have impedance matched 
in this region. However, the high band (5.9 GHz) region has 
moved from its original location, even though that was not 
intentional. The next step is to try to match the 5.9 GHz point 
without undoing the 3.9 GHz match. This can be done with the 
use of parallel capacitors and series inductors (both of which 
affect high frequencies more than low frequencies). To this 
end, we want to swing the high band point in Figure 5 into the 
center of the Smith Chart. Using the concepts of the parallel 
capacitor, we can move the 5.9 GHz impedance to intersect the 
Re[z]=1 circle through a 0.483 pF parallel capacitor. Note that 
by doing so, the 3.9 GHz point is moved slightly away from the 
center but that can be tolerated. The high band is now set up to 
be matched with a series inductor. The required value can be 
found to be approximately 1.61 nH of series inductance. The 
addition of this component to the overall matching network 
produces the final impedance curve, as shown in Figure 7.

Figure 3: Un-matched antenna impedance

Figure 4: Antenna reflection coefficient frequency response

Figure 5: Original VSWR for the antenna



Al Jewad: A multiband biconical log-periodic antenna for swarm communications

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From Figure 7, the high and low bands may not appear 
exactly matched. However, Figure 8 presents the VSWR 
corresponding to the impedance plot of the above Smith chart. 
At 3.9 GHz and at 5.9 GHz, the VSWR is <2.0. This is typically 
considered a good match. If a better match was desired, the 
four component values could be further optimized to improve 
the response. The trick to optimize for the component values 
is to assume that each value has a correction factor of δ. From 
the location of each desired point, we can determine the sign 
and value of each δ. The key factor to remember if lumped 
elements are to be used is the parasitic of each element.

The final step in our matching is to convert the lumped 
elements found into short-embedded transmission lines, as 
shown in Figure 9. The reason for this step is that lumped 
passive elements rarely behave as pure elements at very high 
frequencies. For example, a simple inductor will be hampered 
by stray capacitance and by wire resistance converting it into 
a more complicated circuit element, and the same applies to 
capacitors. In addition, the values we found for the matching 
network are not very practical.

Thus, the initial lumped-element values found were 
converted to distributed elements by utilizing the theory of 
embedded short transmission line.[16] In general, a short-
embedded transmission line can approximate a shunt 
capacitance or a series inductance.

As long as the length of the transmission line is kept very 
small compared to the minimum wavelength of interest, the 
implementation is possible. Other examples exist in[16] for more 
complicated matching networks, and the selection between 
different possible matching networks depends entirely on the 
practicality of the element dimensions.

Figure 6: Matching of the lower frequency band

Figure 7: Matching of the upper frequency band

Figure 8: VSWR for the matched antenna

Figure 9: Short-embedded transmission line implementation of the 
matching network



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The resulting overall matching network was implemented 
on a Rogers 4350B substrate, as shown in Figure 10 for the 
entire frequency band.

SIMULATION RESULTS

The resulting antenna design from the previous section for 
a biconical construct is shown in Figure 11. This design had 
been simulated with Ansoft HFSS. The separation between 
the two conic sections was selected to give resonance at the 
3.9 GHz–5.9 GHz. The 𝑆

11
 or reflection coefficient is shown in 

Figure 12 and the radiation pattern for the 5.9 GHz is shown 
in Figure 13 for 5.9 GHz. The reflection coefficient response 
is <−10 dB over the entire band of interest and the center 
frequencies of 3.9 GHz–5.9 GHz have very apparent resonant 
peaks. This is due to the wideband nature of the spiral 
antennas. As was devised previously, only part of each loop 
contributed to the radiation pattern in each frequency. The rest 
of the stacked loops aided in increasing the broadside gain to 
5 dBi by working as a reflector and helping to limit the beam 
width at high and low elevation angles at the center frequency 
by working as a guide.

CONCLUSION

This paper studied a broadband biconical log-periodic antenna 
design for UAV communications. A geometrical analysis of the 
design is presented along with an HFSS simulation.

The results show that this antenna has good performance 
at the proposed frequency range with center frequencies at 
3.9 GHz and 5.9 GHz. The results show that this antenna can 
achieve a gain of 5 dBi. Further work will focus on increasing 
the gain and miniaturizing the antenna size using ferrite stacks 
and proper dielectric materials.

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Figure 11: The biconical log-periodic spiral antenna (dimensions are 
in mm)

Figure 10: Actual implementation of the matching circuit
Figure 12: Simulated reflection coefficient or S

11
 (dB)

Figure 13: Radiation pattern of antenna (dBi)



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