• Aucun résultat trouvé

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

N/A
N/A
Protected

Academic year: 2021

Partager "Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System"

Copied!
10
0
0

Texte intégral

(1)

HAL Id: hal-01466097

https://hal-ensta-bretagne.archives-ouvertes.fr/hal-01466097

Submitted on 28 May 2021

HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers.

L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés.

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

Hugo Seuté, Cyrille Enderli, Jean-François Grandin, Ali Khenchaf, Jean-Christophe Cexus

To cite this version:

Hugo Seuté, Cyrille Enderli, Jean-François Grandin, Ali Khenchaf, Jean-Christophe Cexus. In- fluence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System.

Journal of Electrical Engineering, Politehnica Publishing House, 2017, 5, pp.1-9. �10.17265/2328-

2223/2017.01.001�. �hal-01466097�

(2)

Journal of Electrical Engineering 5 (2017) 1-9 doi: 10.17265/2328-2223/2017.01.001

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

Hugo Seuté

1

, Cyrille Enderli

1

, Jean-François Grandin

1

, Ali Khenchaf

2

and Jean-Christophe Cexus

2

1. Thales Airborne Systems, 2 Avenue Gay Lussac, 78990 Elancourt, FRANCE

2. Lab-STICC, UMR CNRS 6285, ENSTA Bretagne, 2 Rue François Verny, 29806 Brest, FRANCE

Abstract: In Electronic Warfare, and more specifically in the domain of passive localization, accurate time synchronization between platforms is decisive, especially on systems relying on TDOA (time difference of arrival) and FDOA (frequency difference of arrival). This paper investigates this issue by presenting an analysis in terms of final localization performance of an experimental passive localization system based on off-the-shelf components. This system is detailed, as well as the methodology used to carry out the acquisition of real data. This experiment has been realized with two different kinds of clock. The results are analyzed by calculating the Allan deviation and time deviation. The choice of these metrics is explained and their properties are discussed in the scope of an airborne bi-platform passive localization context. Conclusions are drawn regarding the overall localization performance of the system.

Key words: Synchronization, Allan variance, time deviation, TDOA, FDOA, passive localization, USRP (universal software radio peripheral).

1. Introduction

Historically, most passive localization systems based on electromagnetic radiation have been developed in the context of EW (electronic warfare), and were denoted as ESM (electronic support measures). Various military applications have emerged, where ESM devices are mounted onboard different kinds of platforms: airborne [1], naval [2] or even spatial [3].

Passive localization systems use the properties of a signal received at different positions and/or dates in order to compute an estimate of the position of the radiating source. These systems differ from communication systems in that the source does not cooperate with the receiver, thus the waveform is unknown a priori and cannot be used to improve an estimator of the position of the source.

Traditionally, these localization systems have relied on interferometry to obtain AOA (angle of arrival)

Corresponding author: Ali KHENCHAF, professor, research fields: radar, sea clutter, radar cross section, sea EM scattering, complex targets EM scattering, signal processing and remote sensing.

measurements in order to triangulate the position of the source. But these measurements only have an accuracy of a few degrees and the acquisition time can be long before the location is estimated with the desired accuracy. This is why other types of measurements have been introduced. Many modern techniques used in passive localization now rely on time and frequency based measurements on different platforms. For example, many techniques are based on the calculation of T/FDOA (time/frequency difference of arrival) [1-5], and scan-based localization techniques use the dates of interception of the main lobe of a rotating emitter [6].

Since the measurements depend on the time on two or more remote platforms, several clocks are needed. All clocks have imperfections which make them drift, yet a single time base must be maintained all along the measurement time, hence the need to synchronize the devices [5].

Synchronization can be done in practice by exchanging a signal in different configurations:

one-way, two-ways, common view [7]. It is also possible to dispense with a sync signal if beacons of known positions can be seen by the receivers [8].

D

DAVID PUBLISHING

(3)

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

2

This article focuses on a system designed for combined TDOA/FDOA localization in a short-base airborne ESM context. This is a challenging scenario for a synchronized system because the measured time and frequency differences are small, thus the synchronization error must be kept as low as possible in order to have good precision [5]. In the scope of this article we will try to determine what performance in sync error we can expect in real-life situations via implementation and analysis of a full synchronization system, comprised of hardware (clocks, digital receivers) and software (delay estimation algorithm) processing. Then this will be translated in terms of localization error, in a simple scenario.

The paper is organized as follows: Section 2 presents some theoretical background on clock impairments and how to characterize sync error; Section 3 describes the methodology and the experimental process of the measurements which were carried out; in Section 4 the results for two different types of embedded clocks are shown and analyzed from an operational point of view;

Section 5 establishes the link between sync error and localization performances; finally global conclusions and perspectives are presented in Section 6.

2. Timekeeping Issues

A clock can be modeled as a device producing a sine wave output of the form [9]:

sin 2 (1)

where is nominal peak output voltage, amplitude noise, nominal frequencyand phase fluctuation (noise). In the case of time and frequency analysis, we can usually ignore the term. From there we can identify two parameters of interest [9]:

Time fluctuation:

(2) Fractional frequency, derived from the latter:

(3) Due to the non-stationary nature of , these quantities cannot be analyzed through traditional

statistics, the standard variance estimator will not converge as the number of samples increases [10]. In order to have a way to evaluate the amount of fluctuation of fractional frequency , the Allan variance was introduced [9, 11]. It measures the variance of the difference of two values of spaced by a time . An efficient estimator for the Allan variance can be expressed in terms of time data:

∑ 2 (4)

where is the time horizon on which the variance is calculated, the sample of a dataset containing

values of sampled every , and / the number of samples of contained in the time horizon ( must be an integer such as 1).

Other types of variances similar to the Allan variance were developed, like the modified Allan variance, which is capable to distinguish between more types of noise [9, 12]. The expression of its estimate in terms of time data is:

1

2 3 1

∑ ∑ 2 (5)

The time Allan variance is based on the modified (frequency) Allan variance and characterizes the time error of a clock [13]. It can be expressed as:

/3 (6)

All the considerations stated above refer to the characterization of a single clock. But in practice it is not possible to measure the absolute fluctuations of a clock ( and ) without having another clock to use as a time reference for . Therefore and do not represent the absolute fluctuation of a single clock but the fluctuations of a clock relative to another reference clock. 0 s and 0 means that at a date the two clocks are perfectly aligned with each other and their frequency is exactly the same.

can be interpreted as the standard deviation of

the time error between the clocks considering an

integration time of . For example, considering that the

(4)

Influ

time error simulation i 1/√ [13] ( lowest stand

∞, so t correction of values of

On the co a white frequ we have situation, th

when 0

synchroniza highest frequ correct the ti

In the cas the sum of d white phase function example is g synchronize

(which sliding wind means as a c Similarly, deviation of considering being directl of al white freque and for rand calculation o the best inte value of

Now we analysis and data that cou system.

3. Method

In this se

uence of Syn

is a white p illustrated on (as shown on dard deviation the synchroni ffset correspo as possibl ontrary, if the uency noise (

√ [ he lowest sta

0 i.e.

tion strategy uency and us ime base, wit se of a compl different noise e noise and may reac given in Fig. 3 d time base m is sampled e dow of width correction.

, can b f the relative f

an integratio ly linked to t lso reflects d ency noise, w om walk freq of also egration time

.

will try to d identify the

uld have bee

dology and

ection will be

nchronization

phase noise n Fig. 1a), w n Fig. 1b). I n of the error ization proce onding to the

le.

time error ca (like the simu

[13] (see Fi andard devia 0 . In this y is to sam se the vector thout any ave lex noise mo e types (for e white frequ ch a minimu 3. There, a go may be to com every with and use t

be interpreted frequency bet on time of that of ,

different typ we would hav quency noise

o makes it po in order to

o apply the e noise type o en obtained in

Measurem

e described t

n Impairments

(such as in we have

It means that r is attained w ess must app

mean of as m

an be modele ulation in Fig.

ig. 2b). In ation is achie case, the mple at of time error eraging.

odel compose xample in Fi ency noise), um . Again ood way to ha mpute the mea

h )

the series of th

d as the stand tween the clo

. Its expres , a representa pes of noise:

ve 1

√ . ossible to cho o have the low

e same type of real time e n an actual E

ments

the experime

s on an Expe

the

t the when ply a many

d by 2a), this eved best the rs to

ed of g. 3, the n, an ave a an of on a hese

dard ocks, ssion ation for 1/√

The oose west

e of error ESM

ental Fig.

(Fig time proc

Fig.

(Fig simu

Fig.

(Fig time of b

rimental TDO

. 1 Represent g. 1a, top) and

e (Fig. 1b, bo cess.

. 2 Represent g. 2a, top) an

ulated white fr

. 3 Represent g. 3a, top) and

e (Fig. 3b, botto both white phas

OA/FDOA Loc

tation of time time deviation ottom) of a si

tation of time d time deviat requency noise

tation of time time deviation om) of a simula se noise and w

calization Sys

error as a fun n as a function

imulated whit

error as a fu tion (Fig. 2b, e process.

error as a fu n as a function

ated noise proc white frequency

stem 3

nction of time of integration e phase noise

nction of time bottom) of a

nction of time of integration cess composed y noise.

3

e n e

e a

e

n

d

(5)

Influ

4

protocol use passive bi-p to evaluate h time error) o performance two remote r and softwa synchroniza

The recei two SDR (so USRP B210 card, linked This setup developmen frequencies and is availa TDOA have such as Ref.

synchroniza Here, in o time error b

Fig. 4 Diagr

Fig. 5 Diagr

uence of Syn

ed to acquire latform local here is not jus of the clocks o e of a whole receivers, inc are processin

tion protocol ivers used fo oftware defin 0 (receiver # d to a laptop

was chosen nt and expe

from 70 MH able off-the-s e already been f. [14] but the

tion error.

order to have between two

ram of the exp

ram of the dela

nchronization

e time fluctu ization system st the perform of the receive

passive syste cluding their i ng, their c l.

or this experim ed radio) plat 1) and a B2 computer to n because erimentation Hz to 6 GHz,

shelf. Experim n carried out o ey did not an

e an accurate receivers, a

erimental set-u

ay estimation p

n Impairments

uation data o m. What we w mance (in term

rs, but the ov em, compose internal hardw clock and t

mental study tforms based 200 (receiver record the d it allows q

tasks on r it is quite ch mental studie

on USRP dev nalyze thorou

e way to mea a synchroniza

up.

process.

s on an Expe

on a want ms of erall ed of ware their

y are on a r #2)

data.

quick radio heap es on vices ghly

asure ation

syst emi sign B21 loca dela dela can

T

 dete reco stam hav step

 reco accu T [15 Fig

rimental TDO

tem has bee ission of a pe nal is actually 10 card. In ated close to ay can be neg ay cannot be ncelled if the p The sync sign

 When it i ector on the ording a fix mped file. Th ve a huge amo

ps.

 The comp orded by th urately obtain This delay es

] and [16]. It . 5: First the c

OA/FDOA Loc

en developed eriodic sync s y collocated w this experim o each other glected. In the

neglected, bu platform posi nal is used for is detected e signal’s ba xed number his avoids to r ount of data to

lex envelop he two rece

n the time dif timation proc t is done in fo complex enve

calization Sys

d (Fig. 4), b signal. The em with receiver #

ment two p so that the e case of a rea

ut it can be e itions are kno r two things:

(via a simp and), the re of samples record perman

o process in t

es of the s eivers are p fference betw cess is descri our steps, as i elopes are cro

stem

based on the mitter of this

#1, inside the platforms are propagation al system this estimated and own [15].

ple threshold eceivers start into a time nently and to the following

sync signals processed to ween them.

ibed in Refs.

illustrated on ss-correlated, e s e e n s d

d t e o g

s o

. n

,

(6)

Influ

Fig. 6 A rep Table 1 Val

P. V

1 1 2 1 3 5 next the p cross-correla then interpo the parabola final estimat our experim next to each signal betw Thus the va chain direct the tim Due to th requirement

 When envelope of cross-correla there must b interval of p periodic w maximum t records—the that could co

uence of Syn

presentation of ues of the para Value

10 s 143 ns 200 ms 1 kHz 3 MHz 5 GHz points aroun

ation function lated by a par a is compute te of the dela ment, the two h other so the een the two alue at the ou tly correspo me error betwe hese different s on this sign cross-correla f the signals c

ation peak be a single p possible delay with a short time offset ere will be se orrespond to

nchronization

f the envelope o ameters of inte

D S S D F F N nd the main

n are selected rabola, and fi ed, which co ay between th o receivers a difference of platforms c utput of the nds to an een each rece t purposes, th nal:

ation is com contained in t must be peak which ys. Indeed, if t period—sh

expected be everal cross-c a consistent d

n Impairments

of the sync sign erest.

Description Sync signal peri Sampling period Duration of the r Frequency of the Frequency of the Nominal frequen n peak of d, these points

inally the ape orresponds to he two signal are situated r

f path of the s an be neglec delay estima estimate iver.

here are diffe

mputed from the two files unambigu occurs inside the sync sign horter than etween the correlation p delay estimat

s on an Expe

nal with

od of emission d

record of the sy e first modulati e second modul ncy of the local

the s are ex of o the

s. In right sync cted.

ation of

erent

the , the uous:

e an nal is

the two eaks ion.

 imp it is esti mea sign

whe Hen freq esti

A bee com and first

whe sign T grou

rimental TDO

and

ync signal on of the sync s lation of the syn l oscillators on t

 This cross-c prove the accu s stated that th imation is pro

an square rad nals, defined

ere is nce the synch quency comp imation.

A signal com en chosen arb mposed of a c d a high frequ t and second

ere and nals and The settings

uped on Tabl

OA/FDOA Loc

, sam

signal nc signal the receivers an correlation pe uracy of dela he standard d oportional to dian frequenc

by 2 s the signal hronization s ponents to

mplying with bitrarily (repr arrier modula ency signal (s requirement)

sin 2 s

are the freq is the carrier used during le 1.

calization Sys

mpled every

nd emitter eak needs to ay estimation.

deviation of th 1/ , where cy” of the cro

∞∞

power densi signal needs provide acc

h these requi resented on ated in amplit satisfying res ).

sin 2

quencies of th r frequency.

g the measu

stem 5

.

be narrow to . In Ref. [16]

he time offset is the “root oss-correlated

/

(7) ity spectrum.

to have high curate delay

irements has Fig. 6). It is tude by a low spectively the

(8) he modulated

urements are 5

o ] t t d

) . h y

s s w e

) d

e

(7)

Influ

6

Now that fluctuations next step is t consistent w

4. Measur

Two exp featuring a d clock type experiment.

compensated GPSDO (GP actually bas internal cont signal from

Fig. 7 re measuremen the reception clocks type computed fr and (5). Fig.

data, using experiments limited to

for relevant (les interval is t acquisition t behavior of a it appears u the system e What we c is that the fre term time st for a long proportional random walk clocks reach minimum is period

Clocks typ

uence of Syn

we have a s measuremen to produce th with operation

rement Ana

periments ha different type is mounted Clocks type d crystal osci PS disciplined sed on the sa trol loop usin a GPS receiv epresents two nts betw n system fitte e B. Fig. 8 rom the latter 9 shows the A (X). The s was 1 hour

360 s, bec close to ac ss samples a too large). I time is often a clock, but in unlikely that t

exceeds sever can see from ee running cl tability but w

time, time lly to

/

, k frequency m h a minimum s reached wh

40 s (4 mea pe B have a w

nchronization

system capab nts between tw hese data in co nal contexts.

alysis

ave been ca e of clock (A d on both r

e A are TCX illator) and c d oscillator), ame TCXO ng the 1-PPS ( ver as a refere o series of ween the two ed either with 8 shows the r measuremen Allan deviati

acquisition r. The Allan cause values cquisition tim are averaged In other app used to analy n our context the synchron ral minutes.

the time devi ocks (type A) when it is left e deviation which is ch modulation no

time deviatio hen is av asurements).

worse short te

n Impairments

le of giving t wo receivers onditions tha

arried out, e A or B). The s

receivers on XO (tempera clocks type B which are clo but joined to (pulse per sec ence.

time fluctua o platforms, w h clocks type A e time devia

nts using Eqs on from the s time for th deviation plo s of

me may not d, the confide plications, lon yze the long t

of airborne E nization perio

iation plot (F ) have good s ft unsynchron incre haracteristic o

oise [13]. Typ on of 2.5 ns.

veraged durin

erm time stabi

s on an Expe

time , the t are

each same n an

ature B are ocks o an cond)

ation with A or ation . (4) same

hese ot is and t be ence nger term ESM, od of

ig. 8) short nized eases of a pe A

This ng a

ility, Fig.

the

Fig.

plat

Fig.

plat

y()

rimental TDO

. 7 Measured two experimen

. 8 Exper tforms.

. 9 Experim tforms.

101 10-10 10-9

-1

OA/FDOA Loc

d time error nts.

rimental time

mental Allan

0

calization Sys

between p

e deviation

deviation

102

 (s)

-1

1/2

stem

platforms, for

between

between

Clock A Clock B

r

n

n

(8)

Influ

probably bec introduce so Time deviat representativ [13]. But the by flicker p showing a t which is coh [17].

The Allan about the flu the platform decreases p minimum o 130 s.

time minimi that minimiz clocks (typ approximate then it starts If we ex minimum tim clock A for fractional fre A appears synchroniza sync signal best choice.

datalink pro receivers is purposes or short period standard TC

5. Localiza

In the prev considered s by exchangi with the op attain a time frequency d

uence of Syn

cause of an in ome high fre tion increases ve of a flicke en it becomes phase modula time deviatio herent with ti

n deviation p uctuations of ms. For clock proportionally

f 1.2 10 It is interesti izing the Alla zing time dev pe B), th ely constant s decreasing p

xtrapolate th me deviation r 430 s equency devi to be better tion period

exchanged), . Typically, oviding synch s restricted because of ja d synchroniz CXO seems to

ation Perfo

vious section synchronizati ing a synchro ptimal integra e deviation of

deviation of

nchronization

nternal contro equency nois s proportiona er frequency m

constant (i.e.

ation noise) a on of

me accuracy

lot (Fig. 9) g f fractional fre ks type A the

y to 1/ un for an int ing to note th an deviation viation. For t he Allan at 1.5 10 proportionally he results, w n would be ac and clock B iation (Allan r for 60

is high (or a GPSDO a this case ca hronization c or unavaila amming). On zation signal o be a better o

ormances

ns we have sho ion system, u onization sign ation time it f 2.5 ns

f 1.2

n Impairments

ol loop which se in the sys ally to , whic

modulation n . is affe after 60 seco 50 s 40 for a GPS si

gives informa equency betw e Allan devia ntil it reache tegration tim hat the integra

is different f the other type deviation s

until y to 1/ . we see that

chieved by u B otherwise.

deviation), c 00 s . So if even infinite appears to be an happen if apabilities to able (for ste the contrary, l is availabl option.

own that with using TCXOs

nal every 10 was possibl s and a fracti 10 . Fo

s on an Expe

may tem.

ch is noise ected onds, 0 ns, gnal

ation ween ation es a me of ation from es of stays 50 s

the using For lock f the e: no e the f the o the ealth , if a e, a

h the and sec, le to ional or a

TD of t

whe erro con syn inst on repr imp look of l

T

RF The sou bas

Fig.

rimental TDO

OA/FDOA s the measurem

ere and or for time an nstant over nchronization trumental erro

TDOA and resents the c perfect synch king for how ocalization p This scenario

following ea emissions fr e receivers ar urce is at a di

e (Fig. 10).

. 10 Geometr

OA/FDOA Loc

ystem, the ov ments errors ca

are the var nd frequency m

time and i errors. C ors are null, d FDOA err case where er hronization of

to represent erformance f features two ach other at

rom a target re separated istance aw

ry of the scenar

calization Sys

verall standar an be modele

riances of the measurement independent Considering

we obtain a rors. This l rrors are onl f the system.

this lower bo for a simple s o mobile rece

speed and located o by a distanc way from the

rio.

stem 7

rd deviations ed by:

(9) (10) instrumental ts, considered from other that these lower bound lower bound ly due to the We are now ound in terms

cenario.

eivers and d intercepting on their side.

ce and the center of the 7

s

) ) l d r e d d e w s

d

g

.

e

e

(9)

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

8

Under the hypothesis that (the base is short relative to the distance to the source) which is realistic in an airborne context, it is possible to obtain easily the CRLB (Cramér-Rao lower bound) of a position estimator of [5]: its covariance matrix can be expressed as Σ 0 ; 0 with:

, (11)

Considering 50 km , 1 km and 300 m/s , the lower bound of a position estimator considering synchronization errors only is:

38 m, 300 m. We remark that FDOA localization is more demanding in term of synchronization accuracy.

6. Conclusion

One of the objectives of this paper was to point out that the tools developed in frequency analysis (and more particularly the Allan deviation and time deviation) are very useful to characterize the performances of distributed passive localization systems. These tools help understand the operational impact of technological decisions such as the choices concerning the type of oscillator or the synchronization period of the data link.

The main objective was to describe the influence of a realistic synchronization scheme on the output localization performance. In order to attain this objective, a simple but realistic bi-platform system has been set up and time error data have been generated using two different sets of clock. Time and Allan deviations have been computed from these data, providing estimates of synchronization performance for the optimal integration time. These time and frequency performances were used to compute a lower bound for a localization estimator, in a simple yet relevant scenario. In the end, for the case we studied it appeared that the limiting factor was the accuracy in term of fractional frequency stability.

Further work is needed to take into account the platform position error when the differential

propagation time of the sync signal cannot be neglected and must be estimated. Moreover, in this paper we only focused on time error noise, but the same principles could be extended to characterize complicated noise processes that can be present in other kinds of sensors, such as IMU (inertial measurements units).

References

[1] Arena, L., and Orlando, D. 2014. “Passive Location Developments in Elettronica SpA: System Applications.”

2014 Tyrrhenian International Workshop on Digital Communications—Enhanced Surveillance of Aircraft and Vehicles (TIWDC/ESAV), 130-4.

[2] Wooller, D. 1985. “System Considerations for Naval ESM.” In IEE Proceedings of Communications, Radar and Signal Processing, F 132 (4): 212-4.

[3] Yang, Z. B., Wang, L., Chen, P. Q., and Lu, A. N. 2013.

“Passive Satellite Localization Using TDOA/FDOA/AOA Measurements.” In Proceedings of Conference Anthology, IEEE, China, 1-5.

[4] Musicki, D., and Koch, W. 2008. “Geolocation Using TDOA and FDOA Measurements.” 2008 11th International Conference on Information Fusion, 1-8.

[5] Seute, H., Grandin, J.-F., Enderli, C., Khenchaf, A., and Cexus, J.-C. 2015. “Why Synchronization Is a Key Issue in Modern Electronic Support Measures.” 2015 16th International on Radar Symposium (IRS), 794-9.

[6] Hmam, H. 2007. “Scan-Based Emitter Passive Localization.” IEEE Transactions on Aerospace and Electronic Systems 43 (1): 36-54.

[7] Cheng, L., Hailes, S., and Wilson, A. 2010. “Towards Precise Synchronisation in Wireless Sensor Networks.”

2010 IEEE/IFIP 8th International Conference on Embedded and Ubiquitous Computing (EUC), 208-15.

[8] Pelant, M., and Stejskal, V. 2011. “Multilateration System Time Synchronization via Over-determination of TDOA Measurements.” 2011 Tyrrhenian International Workshop on Digital Communications—Enhanced Surveillance of Aircraft and Vehicles (TIWDC/ESAV), 179-83.

[9] IEEE. 2009. “Standard Definitions of Physical Quantities for Fundamental Frequency and Time Metrology—Random Instabilities—Redline.” In Proceedings of IEEE Std. 1139-2008 (Revision of IEEE Std. 1139-1999)—Redline, 1-51.

[10] Allan, D. W. 1987. “Should the Classical Variance Be Used as a Basic Measure in Standards Metrology?” IEEE Transactions on Instrumentation and Measurement IM-36 (2): 646-54.

[11] Allan, D. W. 1966. “Statistics of Atomic Frequency

Standards.” In Proceedings of the IEEE 54 (2): 221-30.

(10)

Influence of Synchronization Impairments on an Experimental TDOA/FDOA Localization System

9

[12] Allan, D.W., and Barnes, J. A. 1981. “A Modified ‘Allan Variance’ with Increased Oscillator Characterization Ability.” In Thirty Fifth Annual Frequency Control Symposium, 470-5.

[13] Allan, D. W., Weiss, M. A., and Jespersen, J. L. 1991. “A Frequency-Domain View of Time-Domain Characterization of Clocks and Time and Frequency Distribution Systems.” In Proceedings of the 45th Annual Symposium on Frequency Control, 667-78.

[14] Seong, H. C., Sang, Rae, Y., Heon, H. C., Chansik, P., and Sang, J. L. 2012. “A Design of Synchronization Method

for TDOA-Based Positioning System.” In Proceedings of 2012 12th International Conference on Control, Automation and Systems (ICCAS), 1373-5.

[15] Seute, H., Grandin, J.-F., Enderli, C., Khenchaf, A., and Cexus, J.-C. 2016. “Experimental Measurement of Time Difference of Arrival.” In Proceedings of 17th International on Radar Symposium (IRS), 1-4.

[16] Stein, S. 1981. “Algorithms for Ambiguity Function Processing.” IEEE Transactions on Acoustics, Speech and Signal Processing 29 (3): 588-99.

[17] GPSDO Datasheet, Ettus Research, May 2014.

Références

Documents relatifs

Subsequent regrowth of the volcanic edi fice returned the magmatic system to conditions less favorable to basaltic magma ascent to the surface and were perhaps associated with

The goal of clock synchronization is to synchronize the time of all sensors because physical clocks of each sensor drift even if they have the same frequency, and these

Si l’adjectif ennuyeux est aujourd’hui plus fréquent que son analogue dans la presse québécoise au sens de « contrariant, fâcheux », ennuyant demeure vivant avec la

Thus, as shown in Figure 1.7, proposing an efficient localization method which is adapted to high data rate millimeter-wave communication systems (particularly at 60 GHz), is the

/ La version de cette publication peut être l’une des suivantes : la version prépublication de l’auteur, la version acceptée du manuscrit ou la version de l’éditeur. Access

We consider the (unimodular) Pisot S-adic framework introduced in [BST14], where unimodular means that the incidence matrices of the substitutions are uni- modular.. The S-adic

Our current research efforts leverage HPC resources to perform high-resolution numerical simulations with hundreds of millions to billions of unknowns to study wave breaking

C’est dans le cadre de la procédure de retour que ces quatre enfants et leur maman ont été détenus durant 54 jours avant leur rapatriement «volontaire» vers la Serbie le 9 octobre