[ieee 2012 international symposium on telecommunication technologies (istt) - kuala lumpur, malaysia...
TRANSCRIPT
Performance Prediction of Future V-band
Earth-space Link in the Tropics
1A.F. Ismail
#,
1N.W. Md Saad,
1K. Badron,
2W. Hashim and
1K. Abdullah
1Dept. of ECE, Faculty of Engineering, International Islamic University Malaysia, Kuala Lumpur, Malaysia.
2MIMOS Berhad, Technology Park Malaysia, Kuala Lumpur, Malaysia.
[email protected], [email protected], [email protected], [email protected] and
Abstract—Higher capacity systems demand for increased of
bandwidths. Higher bandwidth can be achieved by means of
increasing the frequency, and hence greater the capacity of a
channel to carry information. The Ka-band satellite rollouts in
the tropics are still growing. However, the higher frequencies
such as V-band do present a more substantial potential for
increased system capacity and are now starting to draw
attention. Although the bandwidths are theoretically higher at V-
band links, there are many aspects that are harder to achieve
than of those of at lower frequencies. V-band frequencies
certainly have higher RF losses, higher atmospheric propagation
losses and certainly much higher losses due to precipitation.
While the required V-band technological advancements are being
pursued, it is would be in the interest of the satellite designers
and engineers alike to evaluate the viability of such links
especially in the tropics where heavy rains are copious
Keywords—rain attenuation; V-band; tropical region;
impairment
I. INTRODUCTION
A quarter century ago, the operating frequencies of most
available satellites in the tropics were C-band or S-band.
During those days, Ku-band and Ka-band satellite links were
initially confined mainly to temperate regions [1]. Recently
however, there has been significant proliferation of bandwidth-
intensive High Definition Television (HDTV) broadcasting
worldwide including the tropical regions. What lies just beyond
the horizon is the next generation HDTV, a more bandwidth
hungry service; the Ultra High Definition Television
(UHDTV). The 8K UHDTV will at least have 16 times the
number of pixels of the existing 1080p HDTV. In the future,
new satellites in the tropical and equatorial regions will also
have no alternative but to operate at higher than Ku-band
frequencies due to spectrum limitations. Contrary to popular
belief that the future in TV broadcasting will be Internet
Protocol Television (IPTV), one must admit that bandwidth of
fibre optic networks is not unlimited or infinity. Hence, super
high frequency satellite broadcasts might be a more workable
option. The fibre network that have been used for decades to
transmit large volumes of traffic across the country will one
day come to a halt when the number of its users reached
maximum [2].
Performance predictions are an essential step in the design
of all new satellite links. Performance is usually defined as the
expected quality of the channel for a very high percentage of
time (at least a month and usually a year). For satellite
systems, it is usually that level achieved in what is called “clear
sky”. It is very critical to be able to predict accurately the likely
impairment to be encountered on a given link in order to plan
the services economically. The predicted value of signal loss
and fading are used to determine the design parameters [3].
Examples of design parameter are the power requirements of
the equipment, the antenna characteristics and the service range
or the hop length. These design parameters can be determined
and from them the performance of a service is specified for a
particular percentage of the time. The performance can be
specified for example, at availability of 99% of time at a given
receiving location or at a specified percentage of locations
within a reception area. Availability is the ratio typically
associated with the percentage of the total time a service is
capable of being used, or is available to be used during a given
interval to the length of the interval.
Fig. 1. Basic segment of a satellite broadcast link
In satellite communication terms, the link availability is
usually expressed as a percentage of a year when the link will
perform as per the required Bit Error Rate (BER). As an
example, 99% availability for a year, states that the link will be
available for 867.24 hours and unavailable for 87.6 hours
(8760 – 87.6 hours / 8760 hours x 100). Equally important,
other attribution such as the level of interfering signals
exceeded for some small percentage of the time, for instance at
0.1%, also need to be predicted, again at the reception point or
1st IEEE International Symposium on Telecommunication Technologies
978-1-4673-4786-0/12/$31.00 ©2012 IEEE 187
area of concern. Predictions are employed in order to know
whether a satisfactory service will be provided at the required
reception point or area and also for planning to avoid mutual
interference with other systems sharing the same frequency
band.
II. PERFORMANCE PREDICTION
Radiowave propagation plays a very significant part in
the design and eventually dictates performance of space
communication systems. The IEEE defines V-band as between
40 to 75 GHz, but for communications satellites this frequently
means transmit (down-link) signals in the range of 40-46 GHz
and receive (up-link) signals in the range of 48-56 GHz. The
challenge in operating at such high frequencies for
communication purposes is that there exist stronger
electromagnetic interaction between the radio signals and
atmospheric hydrometeors [4]. These instances will without
doubt distort the performance of such high frequency satellite
communication systems. Several procedures have been
proposed for predicting rain induced attenuation statistics.
Among currently available prediction methods are the models
recommended by the radiocommunications sector of the
International Telecommunication Union (ITU-R) [5], the
Dissanayake, Allnutt and Haidara (DAH) rain induced
attenuation model [6], the Crane-Global model [7] and the
Crane-Two Component model [8].
Fig. 2. World climate map [9]
In this paper, performance prediction of a future V-band
Earth-space link for Malaysia, operating in tropical climate
environment was produced using the latest ITU-R model in
force, published in October 2009. This is the most up-to-date
published ITU-R method to predict attenuation due to
precipitation along a slant propagation path, identified as
Recommendation ITU-R P.618-10 - ‘Propagation Data and
Prediction Methods Required for the Design of Earth-Space
Telecommunication Systems’. The procedure currently
adopted in ITU-R prediction model is based on the estimation
of the attenuation exceeded at 0.01% of the time A0.01, which
is derived from the rainfall rate exceeded at the same time
exceedance percentage, R0.01. From a theoretical point of view,
the concept of equiprobable analysis is not consistent with
meteorological information and not entirely satisfying.
Nonetheless, the accuracy obtained in previous cases when
using the prediction method is somewhat consistent with the
quality and variability of available rain intensity data [10].
For a given value of rainfall rate at 0.01 time exceedance
percentage R0.01, the specific attenuation R is calculated. When
multiplied with the effective path length LE, the corresponding
attenuation value at 0.01% time exceedance A0.01 is produced.
The schematic presentation of an Earth-space path outlining the
parameters to be included into the attenuation prediction
procedures is portrayed in Fig. 3.
Fig. 3. Schematic presentation. A: frozen precipitation, B: rain height, C:
liquid precipitation, D: Earth-space path, LG: horizontal projection, LS: slant-
path length, hr: rain height, hs: station height, : elevation angle [2]
The set expression for the estimation of A0.01 is based on
two assumptions. With reference to the above figure, the first
assumption is that the spatial structure of rain can be modelled
by equivalent rain cell; with a rectangular cross-section of
equivalent length LG and effective height hR-hS in the plane of
the path. The subsequent assumption is that the equivalent rain
cell can assume any position with respect to the path with
equal probability.
III. PREDICTION OF PROPAGATION
A variety of propagation parameters needed in planning
Earth-space systems operating in either the Earth-to-space or
space-to-Earth direction, have to be predicted reliably. For a
likely future satellite-Earth link to be operating in Johor
Bahru, Malaysia, the estimations of its performance were
calculated methodically through the following procedures.
TABLE I. EARTH STATION AND SATELLITE INFORMATION
Possible Earth station Potential Satellite Location
longitude (degree),
les : 103.38 E
longitude (degree),
lst : 91.5 E
latitude (degree),
: 1.33 N
frequency (GHz),
f : 38
station height above mean sea level of the (km),
hs : 0.018
polarisation: vertical
188
The below transcript involves and includes adaptations of
the ITU-R P.618-10 for the sake of readability and clarity. In
the latest version of ITU-R prediction procedure, the vertical
structure of rain is taken into account by the use of an
effective rain height hR, derived from experimental data, in the
expression of LS. For vertical paths, the effective path length
coincides with the effective rain height, which at any latitude
may differ from the 00
C isotherm height hFR, as specified in
ITU-R Recommendation, P.839-3 - ‘Rain Height Model for
Prediction Methods’ [11]. Varying techniques have been
proposed by researchers in order to include the vertical
structure of rain into account. Some of techniques can be
considered as an extension of those previously developed for
terrestrial paths [12]. Whereas others proposed rain height
derivation based on extensive studies on the rain structure
itself [13].Malaysian investigators did carry out elementary
studies at various local locations using the TRRM and
meteorology radars in the hope to uncover the actual effective
rain height. [14, 15]. The rainfall rates R0.01 at time
exceedance of 0.01% from the new climatic zone map of ITU-
R Recommendation P.837-6 [16] that equals to 100 mm hr-1
was used in calculating predicted attenuation values.
1) Calculation of the elevation angle , for the earth-space
link:
)cos()(cos1
45.0)cos()cos(tan
2
1
esst
esst
ll
ll (1)
2) Calculation of the polarisation angle :
tan
sintan 1 esst ll
(2)
3) The effective rain height, hR, for the latitude of the
station was determined according to ITU-R
recommendation:
kmhhR 36.00 (3)
The ITU-R Recommendation P.839-3 states that h0 for
Malaysia equals to 4.5 km
4) For 5 computation of the slant-path length Ls,
below the rain height is as follows:
(4)
5) Calculation of the horizontal projection, LG of the
slant-path length from:
(5)
6) Determination of the k and values using the
frequency-dependent coefficients, kH, kV, H, and V from
Table 1 of the ITU-R P.838-3.
Based on assumption of spherical drops, values of k and
have been calculated at various frequencies between 1 and
1000 GHz for several drop temperatures and drop size
distributions. The calculations were computed by assuming
oblate spheroidal drops, aligned with a vertical symmetry axis
and with dimensions related to equal volume spherical drops.
Values of k and coefficients based on the Laws and Parson’s
rain dropsize distribution and a drop temperature of 200 C have
also been calculated and included in Table 1 of
Recommendation ITU-R P.838-3[17]. The table also includes
values for horizontal and vertical polarisation of k and at
various frequencies.
Values of k and at frequencies other than those in the
table can be estimated by interpolation using logarithmic scale
for frequency f, a logarithmic scale for k, and a linear scale for
. For linear and circular polarisation, and for all path
geometries, the k and coefficients for the specific
attenuation equation can be calculated from using the
following equations:
(6)
(7)
where is the path elevation angle and is the
polarisation tilt angle relative to the horizontal as in (2) ( =
45 for circular polarisation).
7) The specific attenuation, R, using the frequency-
dependent coefficients calculated above and the rainfall rate,
R0.01 was obtained by using (1).
Researchers [18] have reported that the relationship
between specific attenuation ‘A’ or ‘R’ and rainfall rate R can
be approximated by using the power-law.
)( 01.0RkR (8)
8) Calculation of the horizontal reduction factor, r0.01, for
0.01% of the time:
(9)
9) Calculation of the vertical adjustment factor, v0.01, for
0.01% of the time:
sin
)( SRs
hhL
cosSG LL
2/2coscos)( 2 VHVH kkkkk
kkkkk VVHHVVHH 2/2coscos)( 2
GRG L
f
Lr
2–01.0
e–138.0–78.01
1
189
01.0
1– –tan
rL
hh
G
sR (10)
Since the > , therefore the reduced length LR was
determined according to;
(11)
In the case of Malaysia, its < 36, hence
= 36 – | | (12)
(13)
10) Calculation of the effective path length is:
01.0vLL RE (14)
11) The predicted attenuation exceeded for 0.01% of an
average year is then calculated using:
(15)
where the effective path length LE is the product of slant
path length, horizontal path reduction factor r0.01 and vertical
path reduction factor v0.01. The empirical expression of (15) is
then used for scaling the other time percentage, in order to
provide a complete prediction of rain induced attenuation
distribution.
12) The estimated attenuation at other time percentages
of an average year, in the range from 0.001% up to 1%, is
deduced from value in step 11 above; in keeping with the
following conditions:
For p < 1% and | | < 36 and 25:
)36(005.0 (16)
and the predicted attenuation is:
(17)
Table II lists the parameters put together in accordance to
the ITU-R’s recommendations.
TABLE II. CALCULATED PARAMETERS USING ITU-R
RECOMMENDATIONS
Parameters Values
R0.01 (mm hr-1): ITU-R P.837-6 100
() 75.92
() 83.57
hR (km): ITU-R P.839-3 4.86
LS (km) 4.99
LG (km) 1.21
kH : ITU-R P.838-3 0.4001
KV : ITU-R P.838-3 0.3844
αH : ITU-R P.838-3 0.8816
αV : ITU-R P.838-3 0.8552
0.868
K 0.3919
R (dB/km) 21.34
r0.01 (mm hr-1) 0.77
() 79.07
() 34.67
v0.01 (mm hr-1) 1.3782
LR (km) 5.30
A0.01 (dB) 113.15
0.17335
IV. RESULTS AND OBSERVATIONS
In designing communications links, cumulative
distributions may be the most effective presentation format for
the long-term data. For instance, link availability or
exceedance at a point can be determined from its annual
cumulative distribution. Thus, appropriate rain induced
attenuation margins can be incorporated into the system in the
attempt to achieved the desired link performance.
Fig. 4. Plot of ITU-R predicted performance statistics
cos
01.0rLL G
R
45.0–e–131sin1
1
2
)1/(θ–
01.0
f
L RR
ER LA 01.0
)θsin)–1(–)(ln045.0–)(ln033.0655.0(–
01.001.0
01.0
pAp
p
pAA
190
TABLE III. SELECTED TIME PERCENTAGES AND PREDICTED VALUES
Time exceedance (%) ITU-R 618-6
Predicted Attenuation (dB)
1.000 14.10
0.300 41.52
0.100 67.42
0.010 113.15
0.001 128.81
Table III lists selected predicted attenuation values for the
likely future V-band satellite-Earth link in Malaysia. Initial
results of possible rain induce-attenuation impairment to be
experienced by a V-band link at Johor Bahru were generated.
The findings suggested that due to the severity of the rain
induced attenuation that will be encountered, commercial V-
band satellite operation in Malaysia and others in tropical
region may not be simply feasible to operate at 99.7%
availability (equivalent to 0.3% time exceedance) to abide the
broadcasting standard. Non realistic margin (by today’s
technological advancement) of somewhat above 41 dB has to
be incorporated into the wireless system to cope with rain
fading in such severe climate.
If V-band satellite communications is to be actually
realized, current [19] and impending researches should be
immediately focused on integrated solutions in the satellite’s
design i.e. increased transmission power level, larger reflector,
reconfigurable antennas, radiating antenna technologies, etc.
RF engineers can partake in the effort by exploring the use of
one or more countermeasure techniques to alleviate the effect
of rain induced attenuation.
V. CONCLUSION
It is not to be expected that spectrum congestion at Ku-
band will happen in the near future. The use of Ku-band
frequency band will be generalised for the next few years,
with an anticipated evolution towards Ka-band and eventually
the V-band for high data rate multimedia applications. The
main constraint will be the propagation impairment that is
expected to be quite severe in tropical climates, so standard
performances may be taxing to achieve in these regions.
Production of predicted impairment statistics as been
highlighted in this paper is therefore very important for the
future design and deployment of anticipated high frequencies
satellite systems in the tropics.
ACKNOWLEDGMENT
The authors acknowledge the Research Management
Centre of the International Islamic University Malaysia
(IIUM). The reported research findings are part of the
deliverables for the research funded under IIUM’s Endowment
Grant Type B.
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