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Short Paper
Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013

Optimization of Inter-satellite Link (ISL) in Hybrid
OFDM-IsOWC Transmission System
Vishal Sharma1, and Amandeep Kaur2
1
2

Shaheed Bhagat Singh State Technical Campus/ECE, Ferozepur, Punjab, India
Shaheed Bhagat Singh State Technical Campus/ECE, Ferozepur, Punjab, India
Email:1 er_vishusharma@yahoo.com, 2 amanjhand60@gmail.com

Abstract— Inter-satellite optical wireless communication
system (IsOWC), one of the important applications of FSO
(Free Space Optics) technology, will be deployed in space in
the near future because of providing power efficient and high
bandwidth allocation facilities unlike present microwave
satellite systems. In this paper, we have deliberated a novel
model of OFDM-IsOWC system using OPTISYSTEM T M
simulator to optimize an inter-satellite link (ISL) between
satellites with acceptable SNR and BER, which is not reported
in previous investigated work.

the transmitted power or decreasing the receiver noise. But,
with the increase of power, major problems like high energy
consumption, large weight and size of the satellite, high cost
and complexity in system arises [11]. Hence, a very small
transmitter divergence angles are used to assure maximum
received power which eliminates the problem of power
dissipation. A phased array based telescope is used to
achieve minimum BER. But, due to use of very narrow beam,
the transmitter may sometimes miss the receiver satellite due
to pointing vibrations. Therefore, for small divergence angles,
the transmitter optics having large aperture is required [1213].
This paper is an attempt to optimize the ISL link between
two satellites with acceptable SNR by incorporating OFDM
technique. The OFDM technique distributes the data over a
large number of carriers that are spaced apart at precise
frequencies with overlapping bands. The use of FFT for
modulation provides orthogonality to the subcarriers, which
prevents the demodulators from seeing frequencies other
than their own. Hence, by incorporating OFDM, IsOWC
system can be used for optimizing the ISL links at very high
data rates. Based on OFDM technology and optics, IsOWC
system can construct high-speed, large-capacity and lowcost ISL links [14]. Also, its channel capacity is highly scalable,
allowing smooth up-gradation or transition from existing
networks. Moreover, OFDM-IsOWC system can not only
reduce fading of wireless signals, but also improve signal
quality. The feasibility of OFDM as modulation technique
for a RoF based WLAN system has been investigated to
carry 20 Mbps data, using carrier frequency of 2.4 GHz and
prolonged the fiber length from 10 Km to 50 Km [15]. A
conventional IsOWC has been demonstrated with at 2.5Gbps
up to ISL link of 1000Km. This work is further extended by
signifying of a hybrid OFDM—IsOWC system in this work
to optimize the ISL link with acceptable SNR and minimum
BER, which is not achieved in previous research work [16].

Index Terms— IsOWC System, ISL Link, OFDM

I. INTRODUCTION
Optical communications systems have evolved from
lengthy fibers to powerful wireless system resulting in the
use of optical wireless communication system in space
communications. Laser communication technology is able to
send information at data rates up to several Gbps and
coverage of thousands of kilometers. This has opened up
the idea to adapt optical wireless communication technology
into space technology and hence inter-satellite optical wireless
communication (IsOWC) came into being [1]. An inter—
satellite optical wireless communications system offers a high
bandwidth, small size, low power and low cost as compared
to microwave satellite systems [2]. In addition, RF wavelength
is much longer compared to lasers hence the beamwidth that
can be achieved using lasers is narrow than that of the RF
system. This result in lower loss compared to RF [3].
IsOWC can be used to connect one satellite to another,
whether the satellite is in the same orbit or in different orbits.
Commonly used orbits for satellites to revolve around Earth
are LEO, MEO and GEO. A highly accurate tracking system
is required which involves the use of beacon signal on the
one side and a quadrant detector with tracking system at
other satellite which ensures that the connected satellites
are well aligned and have proper line of sight. To meet this
requirement, the satellites use the Ephemerides data for rough
pointing and a tracking system for fine pointing to the other
satellite [4]. Several satellites have been developed with OWC
inter—satellite links such as European Space Agency (ESA)’s
Artemis and Japan’s Kirari satellites [5-6]. IsOWC proves to
be a better alternative for transmission of data at high rates
but various parameters need to be taken into account which
degrades the system performance [7-10]. The decrease in
received signal causes the SNR to decrease which tends to
increase BER.This problem is overcome by either increasing
© 2013 ACEEE
DOI: 03.LSCS.2013.1.525

II. MODEL DECRIPTION
The OFDM-IsOWC system consists of three main
communication parts which are transmitter, propagation
channel and receiver which shown in Fig.1 where the
transmitter is in the first satellite and the receiver is in the
second satellite. The IsOWC system is not much different
from free space optics and fiber optic communication where
the difference relies in the propagation medium.The free space
between two connecting satellites is considered as OWC
25
Short Paper
Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013
4000Km at 5Gbps and 5000Km at 2.5Gbps is achieved with
acceptable SNR of 20dB. Consequently, the total received
power at photo detector at 5Gbps is computed as -81dBm at
the ISL link of 4000 Km and at ISL link of 5000Km at 2.5Gbps.
The total received power at satellite 2 is improved by 4dBm in
both the case but at the ISL link of 4000 Km with 5Gbps and
at ISL link of 5000Km at 2.5Gbps as shown in Figure 2 (c, d)
with acceptable BER. Further, the proposed OFDM—IsOWC
system is investigated under the impact of aperture diameter
of transmitting antenna at fixed Rx = 15cm.

Fig. 1. Design of Hybrid OFDM-IsOWC System.

channel which is the propagating medium for the transmitted
light. In the proposed OFDM-IsOWC, 5Gbps QAM data
signals are generated using 4QAM sequence generator with
2 bits per symbol. These 5Gbps QAM data signals are then
OFDM modulated by means of OFDM modulator using 512
subcarriers and FFT size of 1024 to generate 5Gbps OFDM
analog data signals which, further, QAM modulated at 7.5GHz
modulator frequency. This 5Gbps QAM-OFDM treated
analog data signals are then transmitted by means of a CW
laser of 0dBm. These OFDM signals are transmitted over
OWC channel, considered to be outer space, where it is
assumed to be a vacuum and free from atmospheric
attenuation factors. Therefore, the free space loss is taken as
0 dB/Km of optical wireless channel in our proposed model.
The OWC channel is modeled between the two satellites with
different aperture diameter of optical antenna at each end to
simulate optimized divergence angles to achieve high
receiving power [14-15]. The transmitter and receiver gains
are 0dB. The transmitter and receiver antennas are also
assumed to be ideal where the optical efficiency is equal to 1
and there are no pointing errors. Additional losses from
scintillation and mispointing are also assumed to be zero. In
this work, the only cause of signal attenuation is the distance
of the transmission. The receiving end of the IsOWC system
consists of a photo-detector and a low pass filter.
III. RESULT DISCUSSION
In this section, we have discussed the results obtained
from our simulative setup consisting of optical OFDM analog
data signals at 2.5Gbps and 5Gbps modulated at 7.5GHz
QAM—modulator—frequency. This QAM-OFDM treated
analog data signals are modulated with laser operating at
different wavelengths. Then, it is directly transmitted over
an ISL link by means of transmitting antenna of different
aperture diameters. Firstly, SNR and total received power is
calculated at different operating wavelengths with Tx = 15cm
and Rx = 15cm as shown in Figure 2. From Figure 2 (a, b), it is
observed that an improvement of 6dB in SNR is achieved
with 1550nm as compared to 850nm. Secondly, the ISL link of
© 2013 ACEEE
DOI: 03.LSCS.2013.1.525

Fig. 2. SNR and Total received power via ISL at (a,c) 5 Gbps and
(b,d) 2.5 Gbps with Tx = 15 cm amd Rx = 15 cm.

It has been observed that on doubling the size of aperture
26
Short Paper
Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013
diameter of transmitting antenna, the ISL link has been
lengthened to 8000Km at 5Gbps and to 10000Km with Tx =
50cm respectively with acceptable SNR of 20dBm as shown
in Figure 3 (a, c). Also, the total received power at satellite 2
is computed as -79dBm with Tx = 30cm and -78dBm with Tx =
50cm at the ISL link of 8000 Km respectively and at ISL link of
10000Km as shown in Figure 3 (b, d) with acceptable BER.

8000Km with Rx = 50cm respectively with acceptable SNR of
20dBm as shown in Figure 3(a, c). Also, the total received
power at satellite 2 is computed as -79dBm with Rx = 30cm
and -78dBm with Rx = 50cm at the ISL link of 6000 Km and at
ISL link of 8000Km respectively as shown in Figure 3 (b, d)
with acceptable BER.
CONCLUSIONS
A significant improvement in SNR along with acceptable
BER at different data rates is achieved along with the maximum
length of ISL link between the two satellites by incorporating
OFDM scheme in IsOWC systems than that of conventional
IsOWC systems [16]. It is also revealed out that not only the
operating wavelength but also the aperture diameter of
transmitting- and receiving antenna plays an important role
in prolonging the ISL link with OFDM scheme in IsOWC
systems.
REFERENCES

Fig. 3. SNR and Total received power via ISL Link at 5 Gbps with
(a, b) Rx = 30 cm and (b, d) Rx = 50 cm with Tx = 15 cm.

Also, the proposed OFDM-IsOWC system is
investigated at varied values of aperture diameter of receiving
antenna at fixed Tx = 15cm. It has been observed that on
doubling the size of aperture diameter of receiving antenna,
the ISL link has been lengthened to 6000Km at 5Gbps and to
27
© 2013 ACEEE
DOI: 03.LSCS.2013.1. 525

[1] A. H. Hashim, “Modeling and performance study of intersatellite optical wireless communication system”, International
Conference on Photonics (ICP), IEEE, pp.1–4, 2010.
[2] M. A. Krainak, “Inter-satellite communications optoelectronics research at the Goddard Space Flight Center”, Aerospace and Electo-system Magazine, IEEE, vol. 7, pp.44–47,
1992.
[3] Chan, V.W.S, “Optical Satellite Networks”, Journal of Light
wave Technology”, vol. 21, pp. 2811–2817, 2003.
[4] S. Arnon and N. S. Kopeika,, “Laser satellite commu-nication
network-vibration effects and possible solutions”, Pro-ceedings
of the IEEE, vol. 85, pp.1646–1661, 1997.
[5] Z. Sodnik, B. Furch and H. Lutz, “Free-Space Laser
Communication Activities in Europe: SILEX and beyond”,
Lasers and Electro-Optics Society (LEOS), IEEE, pp.78–79,
2006.
[6] C. C. Chen and C. S. Gardner, “Impact of random pointing
and tracking errors on the design of coherent and incoherent
optical inter-satellite communication links”, IEEE Transactions
on Communication, vol. 37, pp: 252–260, 1989.
[7] S. G. Lambert and W. L. Casey, “Laser communication in
space”, Journal of Applied Optics, vol. 37, pp.41–65, 1998.
[8] D. K. Paul and et al, “Optical inter-satellite links: Application
to commercial satellite communications”, In 14th AIAA
Interna-tional Communication Satellite Systems Conference,
Washington, pp. 277–289, 1992.
[9] Dyne, P. P. Collins, and D. Tunbridge, “Satellite mechanical
health monitoring”, Advanced Vibration Measurements, Techniques and Instrumentation for the Early Predication of Failure,
IEE Colloquium, pp. 4/1– 4/8,1992.
[10] S. Arnon and N. S. Kopeika, “Adaptive bandwidth for satellite
optical communication”, Optoelectron, IEE Proceeding, vol.
145, pp.109–115,1998.
[11] K. Inagaki and Y. Karasawa,”Ultra high speed optical beam
steering by optical phased array antenna”, Proceeding SPIE
Free Space Laser Communication Technologies VIII, vol. 2699,
pp. 210–217, 1996.
[12] W. M. Neubert, W. R. Leeb, and A. L. Scholts, “Experi-mental
results on an optical array antenna for non mechanical beam
steering”, Proceeding SPIE Free Space Laser Communication
Technologies IV, vol. 1635, pp.82–89,1992.
Short Paper
Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013
[13] J. E. Mitchell, “Performance of OFDM at 5.8GHz using radio
over fiber link”, Electronics Letters, vol no. 21, 2004.
[14] R. Prasad, “OFDM for Wireless Communications Systems”,Artech House Publication, 2004.
[15] Yunazar, Ferdian, “Modeling and performance analysis of the
OFDM scheme for radio over fiber system”, Master’s thesis,

© 2013 ACEEE
DOI: 03.LSCS.2013.1.525

University Teknologi Malaysia, Faculty of Electrical Engineering, 2009.
[16] V. Sharma and N. Kumar, “Modeling of 2.5Gbps-intersatellite
link (ISL) in inter-Satellite optical wireless com-munication
IsOWC) System”, Optics Communication, Elsevier, vol. 286,
pp.99–102, 2013.

28

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525Optimization of Inter-satellite Link (ISL) in Hybrid OFDM-IsOWC Transmission System

  • 1. Short Paper Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013 Optimization of Inter-satellite Link (ISL) in Hybrid OFDM-IsOWC Transmission System Vishal Sharma1, and Amandeep Kaur2 1 2 Shaheed Bhagat Singh State Technical Campus/ECE, Ferozepur, Punjab, India Shaheed Bhagat Singh State Technical Campus/ECE, Ferozepur, Punjab, India Email:1 er_vishusharma@yahoo.com, 2 amanjhand60@gmail.com Abstract— Inter-satellite optical wireless communication system (IsOWC), one of the important applications of FSO (Free Space Optics) technology, will be deployed in space in the near future because of providing power efficient and high bandwidth allocation facilities unlike present microwave satellite systems. In this paper, we have deliberated a novel model of OFDM-IsOWC system using OPTISYSTEM T M simulator to optimize an inter-satellite link (ISL) between satellites with acceptable SNR and BER, which is not reported in previous investigated work. the transmitted power or decreasing the receiver noise. But, with the increase of power, major problems like high energy consumption, large weight and size of the satellite, high cost and complexity in system arises [11]. Hence, a very small transmitter divergence angles are used to assure maximum received power which eliminates the problem of power dissipation. A phased array based telescope is used to achieve minimum BER. But, due to use of very narrow beam, the transmitter may sometimes miss the receiver satellite due to pointing vibrations. Therefore, for small divergence angles, the transmitter optics having large aperture is required [1213]. This paper is an attempt to optimize the ISL link between two satellites with acceptable SNR by incorporating OFDM technique. The OFDM technique distributes the data over a large number of carriers that are spaced apart at precise frequencies with overlapping bands. The use of FFT for modulation provides orthogonality to the subcarriers, which prevents the demodulators from seeing frequencies other than their own. Hence, by incorporating OFDM, IsOWC system can be used for optimizing the ISL links at very high data rates. Based on OFDM technology and optics, IsOWC system can construct high-speed, large-capacity and lowcost ISL links [14]. Also, its channel capacity is highly scalable, allowing smooth up-gradation or transition from existing networks. Moreover, OFDM-IsOWC system can not only reduce fading of wireless signals, but also improve signal quality. The feasibility of OFDM as modulation technique for a RoF based WLAN system has been investigated to carry 20 Mbps data, using carrier frequency of 2.4 GHz and prolonged the fiber length from 10 Km to 50 Km [15]. A conventional IsOWC has been demonstrated with at 2.5Gbps up to ISL link of 1000Km. This work is further extended by signifying of a hybrid OFDM—IsOWC system in this work to optimize the ISL link with acceptable SNR and minimum BER, which is not achieved in previous research work [16]. Index Terms— IsOWC System, ISL Link, OFDM I. INTRODUCTION Optical communications systems have evolved from lengthy fibers to powerful wireless system resulting in the use of optical wireless communication system in space communications. Laser communication technology is able to send information at data rates up to several Gbps and coverage of thousands of kilometers. This has opened up the idea to adapt optical wireless communication technology into space technology and hence inter-satellite optical wireless communication (IsOWC) came into being [1]. An inter— satellite optical wireless communications system offers a high bandwidth, small size, low power and low cost as compared to microwave satellite systems [2]. In addition, RF wavelength is much longer compared to lasers hence the beamwidth that can be achieved using lasers is narrow than that of the RF system. This result in lower loss compared to RF [3]. IsOWC can be used to connect one satellite to another, whether the satellite is in the same orbit or in different orbits. Commonly used orbits for satellites to revolve around Earth are LEO, MEO and GEO. A highly accurate tracking system is required which involves the use of beacon signal on the one side and a quadrant detector with tracking system at other satellite which ensures that the connected satellites are well aligned and have proper line of sight. To meet this requirement, the satellites use the Ephemerides data for rough pointing and a tracking system for fine pointing to the other satellite [4]. Several satellites have been developed with OWC inter—satellite links such as European Space Agency (ESA)’s Artemis and Japan’s Kirari satellites [5-6]. IsOWC proves to be a better alternative for transmission of data at high rates but various parameters need to be taken into account which degrades the system performance [7-10]. The decrease in received signal causes the SNR to decrease which tends to increase BER.This problem is overcome by either increasing © 2013 ACEEE DOI: 03.LSCS.2013.1.525 II. MODEL DECRIPTION The OFDM-IsOWC system consists of three main communication parts which are transmitter, propagation channel and receiver which shown in Fig.1 where the transmitter is in the first satellite and the receiver is in the second satellite. The IsOWC system is not much different from free space optics and fiber optic communication where the difference relies in the propagation medium.The free space between two connecting satellites is considered as OWC 25
  • 2. Short Paper Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013 4000Km at 5Gbps and 5000Km at 2.5Gbps is achieved with acceptable SNR of 20dB. Consequently, the total received power at photo detector at 5Gbps is computed as -81dBm at the ISL link of 4000 Km and at ISL link of 5000Km at 2.5Gbps. The total received power at satellite 2 is improved by 4dBm in both the case but at the ISL link of 4000 Km with 5Gbps and at ISL link of 5000Km at 2.5Gbps as shown in Figure 2 (c, d) with acceptable BER. Further, the proposed OFDM—IsOWC system is investigated under the impact of aperture diameter of transmitting antenna at fixed Rx = 15cm. Fig. 1. Design of Hybrid OFDM-IsOWC System. channel which is the propagating medium for the transmitted light. In the proposed OFDM-IsOWC, 5Gbps QAM data signals are generated using 4QAM sequence generator with 2 bits per symbol. These 5Gbps QAM data signals are then OFDM modulated by means of OFDM modulator using 512 subcarriers and FFT size of 1024 to generate 5Gbps OFDM analog data signals which, further, QAM modulated at 7.5GHz modulator frequency. This 5Gbps QAM-OFDM treated analog data signals are then transmitted by means of a CW laser of 0dBm. These OFDM signals are transmitted over OWC channel, considered to be outer space, where it is assumed to be a vacuum and free from atmospheric attenuation factors. Therefore, the free space loss is taken as 0 dB/Km of optical wireless channel in our proposed model. The OWC channel is modeled between the two satellites with different aperture diameter of optical antenna at each end to simulate optimized divergence angles to achieve high receiving power [14-15]. The transmitter and receiver gains are 0dB. The transmitter and receiver antennas are also assumed to be ideal where the optical efficiency is equal to 1 and there are no pointing errors. Additional losses from scintillation and mispointing are also assumed to be zero. In this work, the only cause of signal attenuation is the distance of the transmission. The receiving end of the IsOWC system consists of a photo-detector and a low pass filter. III. RESULT DISCUSSION In this section, we have discussed the results obtained from our simulative setup consisting of optical OFDM analog data signals at 2.5Gbps and 5Gbps modulated at 7.5GHz QAM—modulator—frequency. This QAM-OFDM treated analog data signals are modulated with laser operating at different wavelengths. Then, it is directly transmitted over an ISL link by means of transmitting antenna of different aperture diameters. Firstly, SNR and total received power is calculated at different operating wavelengths with Tx = 15cm and Rx = 15cm as shown in Figure 2. From Figure 2 (a, b), it is observed that an improvement of 6dB in SNR is achieved with 1550nm as compared to 850nm. Secondly, the ISL link of © 2013 ACEEE DOI: 03.LSCS.2013.1.525 Fig. 2. SNR and Total received power via ISL at (a,c) 5 Gbps and (b,d) 2.5 Gbps with Tx = 15 cm amd Rx = 15 cm. It has been observed that on doubling the size of aperture 26
  • 3. Short Paper Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013 diameter of transmitting antenna, the ISL link has been lengthened to 8000Km at 5Gbps and to 10000Km with Tx = 50cm respectively with acceptable SNR of 20dBm as shown in Figure 3 (a, c). Also, the total received power at satellite 2 is computed as -79dBm with Tx = 30cm and -78dBm with Tx = 50cm at the ISL link of 8000 Km respectively and at ISL link of 10000Km as shown in Figure 3 (b, d) with acceptable BER. 8000Km with Rx = 50cm respectively with acceptable SNR of 20dBm as shown in Figure 3(a, c). Also, the total received power at satellite 2 is computed as -79dBm with Rx = 30cm and -78dBm with Rx = 50cm at the ISL link of 6000 Km and at ISL link of 8000Km respectively as shown in Figure 3 (b, d) with acceptable BER. CONCLUSIONS A significant improvement in SNR along with acceptable BER at different data rates is achieved along with the maximum length of ISL link between the two satellites by incorporating OFDM scheme in IsOWC systems than that of conventional IsOWC systems [16]. It is also revealed out that not only the operating wavelength but also the aperture diameter of transmitting- and receiving antenna plays an important role in prolonging the ISL link with OFDM scheme in IsOWC systems. REFERENCES Fig. 3. SNR and Total received power via ISL Link at 5 Gbps with (a, b) Rx = 30 cm and (b, d) Rx = 50 cm with Tx = 15 cm. Also, the proposed OFDM-IsOWC system is investigated at varied values of aperture diameter of receiving antenna at fixed Tx = 15cm. It has been observed that on doubling the size of aperture diameter of receiving antenna, the ISL link has been lengthened to 6000Km at 5Gbps and to 27 © 2013 ACEEE DOI: 03.LSCS.2013.1. 525 [1] A. H. Hashim, “Modeling and performance study of intersatellite optical wireless communication system”, International Conference on Photonics (ICP), IEEE, pp.1–4, 2010. [2] M. A. Krainak, “Inter-satellite communications optoelectronics research at the Goddard Space Flight Center”, Aerospace and Electo-system Magazine, IEEE, vol. 7, pp.44–47, 1992. [3] Chan, V.W.S, “Optical Satellite Networks”, Journal of Light wave Technology”, vol. 21, pp. 2811–2817, 2003. [4] S. Arnon and N. S. Kopeika,, “Laser satellite commu-nication network-vibration effects and possible solutions”, Pro-ceedings of the IEEE, vol. 85, pp.1646–1661, 1997. [5] Z. Sodnik, B. Furch and H. Lutz, “Free-Space Laser Communication Activities in Europe: SILEX and beyond”, Lasers and Electro-Optics Society (LEOS), IEEE, pp.78–79, 2006. [6] C. C. Chen and C. S. Gardner, “Impact of random pointing and tracking errors on the design of coherent and incoherent optical inter-satellite communication links”, IEEE Transactions on Communication, vol. 37, pp: 252–260, 1989. [7] S. G. Lambert and W. L. Casey, “Laser communication in space”, Journal of Applied Optics, vol. 37, pp.41–65, 1998. [8] D. K. Paul and et al, “Optical inter-satellite links: Application to commercial satellite communications”, In 14th AIAA Interna-tional Communication Satellite Systems Conference, Washington, pp. 277–289, 1992. [9] Dyne, P. P. Collins, and D. Tunbridge, “Satellite mechanical health monitoring”, Advanced Vibration Measurements, Techniques and Instrumentation for the Early Predication of Failure, IEE Colloquium, pp. 4/1– 4/8,1992. [10] S. Arnon and N. S. Kopeika, “Adaptive bandwidth for satellite optical communication”, Optoelectron, IEE Proceeding, vol. 145, pp.109–115,1998. [11] K. Inagaki and Y. Karasawa,”Ultra high speed optical beam steering by optical phased array antenna”, Proceeding SPIE Free Space Laser Communication Technologies VIII, vol. 2699, pp. 210–217, 1996. [12] W. M. Neubert, W. R. Leeb, and A. L. Scholts, “Experi-mental results on an optical array antenna for non mechanical beam steering”, Proceeding SPIE Free Space Laser Communication Technologies IV, vol. 1635, pp.82–89,1992.
  • 4. Short Paper Proc. of Int. Conf. on Advances in Communication, Network, and Computing 2013 [13] J. E. Mitchell, “Performance of OFDM at 5.8GHz using radio over fiber link”, Electronics Letters, vol no. 21, 2004. [14] R. Prasad, “OFDM for Wireless Communications Systems”,Artech House Publication, 2004. [15] Yunazar, Ferdian, “Modeling and performance analysis of the OFDM scheme for radio over fiber system”, Master’s thesis, © 2013 ACEEE DOI: 03.LSCS.2013.1.525 University Teknologi Malaysia, Faculty of Electrical Engineering, 2009. [16] V. Sharma and N. Kumar, “Modeling of 2.5Gbps-intersatellite link (ISL) in inter-Satellite optical wireless com-munication IsOWC) System”, Optics Communication, Elsevier, vol. 286, pp.99–102, 2013. 28