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  <front>
    <journal-meta>
      <issn pub-type="ppub">1613-0073</issn>
    </journal-meta>
    <article-meta>
      <title-group>
        <article-title>Methods for Time Synchronization in Distributed Radar Systems</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>Damodarin Udhaya Mugil</string-name>
          <email>Udhaya.Mugil.Damodarin@uniroma2.it</email>
          <xref ref-type="aff" rid="aff0">0</xref>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Federico Di Girolamo</string-name>
          <email>federico.digirolamo@alumni.uniroma2.eu</email>
          <xref ref-type="aff" rid="aff0">0</xref>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Samuele Tanzini</string-name>
          <email>samuele.tanzini@alumni.uniroma2.eu</email>
          <xref ref-type="aff" rid="aff0">0</xref>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Department of Electronic Engineering, Tor Vergata University of Rome</institution>
          ,
          <addr-line>00133 Rome</addr-line>
          ,
          <country country="IT">Italy</country>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>Informatics</institution>
          ,
          <addr-line>Mathematics, and Engineering. Catania</addr-line>
        </aff>
      </contrib-group>
      <fpage>47</fpage>
      <lpage>52</lpage>
      <abstract>
        <p>Recently, the push to develop high-performance antenna arrays for space applications has underscored the economic and technical constraints associated with satellite missions. One cost-reducing strategy involves deploying a swarm of smaller, lighter satellites, though this approach introduces synchronization complexities. This paper evaluates two time synchronization techniques for distributed radar systems: the Two Way Time Transfer (TWTT) based Inter-Satellite Link (ISL) method and a Phase-Locked Loop (PLL) based method. The TWTT method utilizes Time Division Multiple Access (TDMA) for signal exchange among satellites, ensuring time alignment via delay filters. Conversely, the PLL method involves a primary satellite transmitting a reference signal to secondary satellites, which then recover the clock signal. Both techniques are analyzed for their implementation feasibility and efectiveness in maintaining synchronization, with simulation results demonstrating their potential in improving satellite communication performance. Time synchronization, distributed radar systems, satellite swarm, Two Way Time Transfer (TWTT), Inter-Satellite Link (ISL), ICYRIME 2024: 9th International Conference of Yearly Reports on</p>
      </abstract>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>CEUR
ceur-ws.org</p>
    </sec>
    <sec id="sec-2">
      <title>1. Introduction</title>
    </sec>
    <sec id="sec-3">
      <title>2. TWTT Based ISL Link Method</title>
      <p>
        In recent years, a new technical trend has been spread- The TWTT Based ISL Link is a Method used to reach the
ing throughout the world. The objective is to develop
time synchronization between sensors in a multistatic
increasingly high-performance antenna arrays for space
system. The basic idea is to broadcast signal flight times
applications from both a technological and an
applicaand ofset delays among various local oscillators
informational point of view. The greatest economic impact of
tion between nodes and exploit this information to align
each mission is established by the weight of the launcher
the flow of transmitted or received data with true delay
and the payload; therefore, implementation constraints
iflters. The ISL is performed using a Time Division
Multiare often also established to find the optimal compromise
ple Access (TDMA) method: to each node is assigned the
between weight and technology [
        <xref ref-type="bibr" rid="ref1">1</xref>
        ] used to perform the
time intervals to listen to and transmit data within the
satellite or to improve its performance [
        <xref ref-type="bibr" rid="ref2">2</xref>
        ]. A possible
formationas as reported in [
        <xref ref-type="bibr" rid="ref11">11</xref>
        ] and [
        <xref ref-type="bibr" rid="ref12">12</xref>
        ], for which the
solution to reduce satellite launch costs is to use a satel- implemented software has been refactored accordignly
lite swarm [
        <xref ref-type="bibr" rid="ref3 ref4">3, 4</xref>
        ] composed of many smaller and lighter
[
        <xref ref-type="bibr" rid="ref13">13</xref>
        ]. In order to carry out the TDMA technique and to
satellites [
        <xref ref-type="bibr" rid="ref5">5</xref>
        ]. Although the implementation of these
sysensure that the time intervals will be respected, all nodes
tems has the advantage of decreasing launch costs, they
must first achieve coarse synchronization. This can be
have the disadvantage of complexity of synchronization
achieved by using a highly stable frequency source and
− 2 ( −  + , )

 ,
err
[
        <xref ref-type="bibr" rid="ref10 ref6 ref7 ref8 ref9">6, 7, 8, 9, 10</xref>
        ]. In this paper, two diferent synchronization
techniques are analyzed. The first one is based on a direct
Inter-Satellite link (ISL) using Two Way Time Transfer
(TWTT), and the second is based on the transmission
of a reference signal from a primary to one or multiple
secondary that recover the clock with a PLL.
      </p>
      <p>To achieve fine synchronization, the i-th node must first
ulated on a carrier of frequency  and phase  :
broadcast a chirp signal, denoted as ( ), which is
mod( ) = ( ) · − 2 ( )</p>
      <p>·  
We can represent the signal received by the j-th sensor
at a certain distance and sampled at  as:
, [] =   −    −   +
,</p>
      <p>︂)]
To compute the time of arrival (and thus the delay time)
during reception, it is necessary to perform the following
correlation:
, ( ) = , ( ) * * (−  )</p>
      <p>The maximum of this convolution correspond to the delay
value associated with the clock temporal delays and the
time of flight (TOF).</p>
      <p>
        In this study, the classic Quadratic Least Squares method
was used because it was found to have acceptable
performance as shown in [
        <xref ref-type="bibr" rid="ref14">14</xref>
        ]:
:, =   |, ( )|
      </p>
      <p>=   −   +  ,
Once the time corresponding to the peak of the
correlation has been found, the sample corresponding to this
time can be determined using the sampling frequency :</p>
      <p>:, =  · ,</p>
      <sec id="sec-3-1">
        <title>2.1. Simulation model</title>
        <p>˜ =  −
2 − 0
20 − 41 + 22</p>
      </sec>
      <sec id="sec-3-2">
        <title>2.2. Simulation results</title>
        <p>During the simulation, the correlation peaks initially
appear separated because the average value of the
pretransmission shift has not yet been processed. These
peak separations indicate the delay of diferent
transmission epochs (Fig. 3). This delay prevents synchronous
transmission, making the system unusable. Subsequently,
synchronization epochs will be performed to observe
how the peaks’ distances converge, as shown in Fig. 2.2.</p>
        <p>This algorithm is continuously iterated so that the chirps
overlap as much as possible. Only in this way can we
compensate for delays caused by temporal clock drifts
among the various nodes.</p>
        <p>The core issue is not the implementation of BPSK or
QPSK encoding, but the conversion of arrival times into
information suitable for use as a modulating signal for
transmission. The chosen method involves converting
these temporal values into voltage levels, which could be
utilized with an encoder before transmission.</p>
        <p>The proposed Rx architecture is shown in Fig. 1. Fol- In Fig. 2, the iteration of the algorithm throughout the
enlowing the correlation using the matched filter, there is a tire working period is shown; it is clear that it is possible
comparison process aimed at resetting a set/reset counter to correct a few tenths of a sample.
in free-counting mode. The counter continues to count
indefinitely until reset by an external signal
corresponding to the correlation peak. The conversion to amplitude 3. PLL Based ISL Method
was achieved by implementing a memory that contains
various delay values in terms of samples. This memory The second method analyzed is an implementation of
is scanned by the previously introduced counter, and a PLL based architecture [15, 16, 17]. This architecture
through the "hit" signal generated by the counter itself, has a primary sensor and  secondary sensors; each
secit becomes possible to sample the time value as ampli- ondary sensor receives a wave from the primary and
tude. While in Simulink the transmission and reception synchronizes its clock on it. When all clocks are
synprocess was simulated, in Matlab the iterative true peak chronized each node will be in phase depending on the
detection algorithm was employed. This iterative process distance from the primary sensor [18, 19].
generates ˆ at each step, which will be applied to
different chirps before transmission. The goal is to achieve 3.1. Simulation model
perfect synchronization by aligning all signals ideally;
where:
The simulated PLL transfer function, responsible for
engaging the phase of the signal transmitted by the primary
sensor, is:
ˆ =
1 ∑︁ Φ ˆ ,


0() = 5.78
1 + 8.1 · 10− 3 107</p>
        <p>2</p>
        <p>After a period of synchronization, the primary and
secondary nodes have the same clock time. In this work,
we used a carrier wave of 1  modulated with a 1.5
  sinusoidal wave.</p>
        <p>After clock synchronization, the next step is to
synchronize the phases of the waveforms. This is important
because in relation to the distance from the primary sensor,
all nodes must create a beam with constructive
interference on the target. The formula used to adjust the phase
contribution is [15]:
 ( ) = 2</p>
        <p />
        <p>[1 − sin( )]
The simulated system is composed by 2 nodes, a block
that simulates an instantaneous phase noise, and the
phase shift blocks, which are controlled by a high
precision ranging system [18]. In fig.7 the PLL structure is
shown while the complete system is shown in fig.8.</p>
      </sec>
      <sec id="sec-3-3">
        <title>3.2. Simulation results</title>
        <p>In the final step, we assessed the nodes’ performance
by comparing the outputs of the phase shifters with the
inputs. In Fig.9 and 10 we note that the system converges
across all distances tested and remains resistant to small
phase disturbances.</p>
      </sec>
    </sec>
    <sec id="sec-4">
      <title>4. Conclusions</title>
      <p>In this work, two diferent methods have been analyzed;
after the implementation study and the simulation results
we are able to determinate the advantages and
disadvantages for both paths taken. The "TWTT Based ISL Link
Method" we have the opportunity to develop both
software, to face any implementation challenges, and
hardware, to speed up algorithm processing. This algorithm
convergence is ensured mathematically, indeed, it is
wellknown that the arithmetic mean can influence a set of
data, improving its precision as well. A problem could
be the rising of complexity in defining a communication
protocol with increasingly large system. For the "PLL
Based ISL Method" we are able to perform beamforming
without DSP, which is an worth implementation
semplification, but we need an high precision measurement
system in  or  band which could be dificult in ISL
systems.</p>
      <p>In future works, new optimization methods based on
neural approaches will be explored [20, 21, 22]</p>
    </sec>
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