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VSAT Communication |
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| Name : Muhammad Ali Khan Email : None Date : 08-02-2003 Submitted : 08/2/2003 VSAT
The first artificial satellite "SPUTNIK I" was launched by the erstwhile USSR, in 1957. This began a series of space initiatives by USA and USSR. The first satellite communication experiment was the US government's project SCORE (Signal Communication by Orbiting Relay Equipment), which launched a satellite on December 18, 1958. This satellite circled the earth in an elliptical orbit and retransmitted messages recorded on a magnetic tape. It lasted for about 13 days after which the batteries ran out!! The US Army Signal Corp's Courier IB, launched in October 1960, lasted for about 17 days. It could handle typewriter data and voice and facsimile messages. It was a balloon, Echo 1, launched in August 1960, which led American
Telephone & Telegraph Company (AT&T) to build Telstar. Communication tests
carried out by reflecting radio signals from Echo 1's surface were completely
successful. In 1964 a global initiative was undertaken leading to the formation
of INTELSAT, which has been one of the major driving forces for the large
scale commercial exploitation of satellite technology for communications.
Since then there has been no looking back.
The VSAT comprises of two modules - an outdoor unit and an indoor unit. The outdoor unit consists of an Antenna and Radio Frequency Transceiver. (RFT). The antenna size is typically 1.8 metre or 2.4 metre in diameter, although smaller antennas are also in use. The indoor unit functions as a modem and also interfaces with the end user equipment like stand alone PCs, LANs, Telephones or an EPABX. VSATs can typically be divided into two parts- an outdoor unit and an indoor unit. The outdoor unit is generally ground or even wall mounted and the indoor unit which is the size of a desktop computer is normally located near existing computer equipment in your office. Outdoor Unit The antenna system comprises of a reflector, feedhorn and a mount. The size of a VSAT antenna varies from 1.8 metres to 3.8 metres. The feedhorn is mounted on the antenna frame at its focal point by support arms. The FEED HORN directs the transmitted power towards the antenna dish or collects the received power from it. It consists of an array of microwave passive components. Antenna size is used to describe the ability of the antenna to amplify the signal strength. The RFT is mounted on the antenna frame and is interconnected to the feed horn. Also termed as outdoor electronics, RFT, in turn, consists of different subsystems. These include low noise Amplifiers (LNA) and down converters for amplification and down conversion of the received signal respectively. LNAs are designed to minimise the noise added to the signal during this first stage of the converter as the noise performance of this stage determines the overall noise performance of the converter unit. The noise temperature is the parameter used to describe the performance of a LNA Upconverters and High Powered Amplifiers (HPA) are also part of the RFT and are used for upconverting and amplifying the signal before transmitting to the feedhorn. The Up/Down converters convert frequencies between intermediate frequency (Usually IF level 70 MHz) and radio frequency. For Extended C band, the downconverter receives the signal at 4.500 to 4.800 GHz and the upconverter converts it to 6.725 to 7.025 GHz. The HPA ratings for VSATs range between 1 to 40 watts Interlink Facility The outdoor unit is connected through a low loss coaxial cable to the indoor unit. The typical limit of an IFL cable is about 300 feet. Indoor Unit The IDU consists of modulators which superimpose the user traffic signal on a carrier signal. This is then sent to the RFT for upconversion, amplification and transmission. It also consists of demodulators which receive the signal from the RFT in the IF range and demodulates the same to segregate the user traffic signal from the carrier. The IDU also determines the access schemes under which the VSAT would operate. The IDU also interfaces with various end user equipment, ranging from stand alone computers, LAN's, routers, multiplexes, telephone instruments, EPABX as per the requirement. It performs the necessary protocol conversion on the input data from the customer end equipment prior to modulation and transmission to the RFT. An IDU is specified by the access technique, protocols handled and number of interface ports supported. Advantages of VSATs If by now you believe that VSATs provide an edge over terrestrial lines only in cases where the land lines are difficult to install, say in the case of remote locations, then consider this. Close to 50 percent of the total VSAT population is installed in the US which also boasts of world's best terrestrial communications. Networking of business activities, processes and divisions is essential to gain a competitive edge in any industry. VSATs are an ideal option for networking because they enable Enterprise Wide Networking with high reliability and a wide reach which extends even to remote sites. Last Mile Problem Let us begin with the situation where you have reliable high-speed links between city exchanges for meeting your communication requirements. But before you begin to feel comfortable, connections from the nearest exchange to your company's office often fail. Consequently, stretching what is technically called the last mile problem into much longer distances. VSATs located at your premises guarantee seamless communication even across the last mile. Reach You must be well aware of the limitations faced by terrestrial lines in reaching remote and other difficult locations. VSATs,on the other hand, offer you unrestricted and unlimited reach. Reliability Uptime of upto 99.5 percent is achievable on a VSAT network. This is significantly higher than the typical leased line uptime of approximately 80 to 85 percent. Time VSAT deployment takes no more than 4-6 weeks as compared to 4 to 6 months for leased lines. Network Management Network monitoring and control of the entire VSAT network is much simpler than a network of leased lines, involving multiple carriers at multiple locations. A much smaller number of elements needs to be monitored incase of a VSAT network and also the number of vendors and carriers involved in between any two user terminals in a VSAT network is typically one. This results in a single point of contact for resolving all your VSAT networking issues. A VSAT NMS easily integrates end-to-end monitoring and configuration control for all network subsystems. Maintenance A single point contact for operation, maintenance, rapid fault isolation and trouble shooting makes things very simple for a client, using VSAT services. VSATs also enjoy a low mean time to repair (MTTR) of a few hours, which extends upto a few days in the case of leased lines. Essentially, lesser elements imply lower MTTR. Flexibility VSAT networks offer enormous expansion capabilities. This feature factors in changes in the business environment and traffic loads that can be easily accommodated on a technology migration path. Additional VSATs can be rapidly installed to support the network expansion to any site, no matter however remote. Cost A comparison of costs between a VSAT network and a leased line network
reveals that a VSAT network offers significant savings over a two to three
years timeframe. This does not take into account the cost of downtime,
inclusion of which would result in the VSAT network being much more cost
- effective. Pay-by-mile concept in case of leased line sends the costs
spiraling upwards. More so if the locations to be linked are dispersed
all over the country. Compare this to VSATs where the distance has nothing
to do with the cost.Additionally, in case of VSATs, the service charges
depend on the bandwidth which is allocated to your network in line with
your requirements. Whereas with a leased line you get a dedicated circuit
in multiples of 64Kbps whether you need that amount of bandwidth or not.
VSAT System Architecture A VSAT system consists of a satellite transponder, central hub or a master earth station, and remote VSATs. The VSAT terminal has the capability to receive as well as transmit signals via the satellite to other VSATs in the network. Depending on the access technology used the signals are either sent via satellite to a central hub, which is also a monitoring centre, or the signals are sent directly to VSATs with the hub being used for monitoring and control. Topologies The network of VSATs at different locations adopts different topologies depending on the end applications traffic flow requirements. These topologies could be Star or Mesh. The most popular of these is Star topology. Here we have a big, central earthstation known as the hub. Generally the hub antenna is in the range of 6-11metre in diameter. This hub station controls, monitors and communicates with a large number of dispersed VSATs. Since all VSATs communicate with the central hub station only, this network is more suitable for centralized data applications. Large organizations, like banks, with centralized data processing requirements is a case in point. In a mesh topology a group of VSATs communicate directly with any other
VSAT in the network without going through a central hub. A hub station
in a mesh network performs only the monitoring and control functions.
These networks are more suitable for telephony applications. These have
also been adopted to deploy point to point high speed links. Access Technologies The primary objective and advantage of these networks is to maximise the use of common satellite and other resources amongst all VSAT sites. The method by which these networks optimise the use of satellite capacity, and spectrum utilisation in a flexible and cost effective manner are referred to as satellite access schemes. Each of the above topologies is associated with an appropriate satellite access scheme. The most commonly used satellite access schemes are:
These technologies are explained in another article VSAT access technologies. Space Segment Support The ideal orbit for a communications satellite is geostationary , or motionless relative to the ground. Satellites used for communications are almost exclusively in the geostationary orbit, located at 36000 km above the equator. In line with ITU stipulations, for avoiding interference, all satellites are placed 2 degree apart. This places a maximum limit of 180 satellites operating in a geostationary orbit. However, with a view to maximise the utilisation of orbital slots, Co-located satellites are being deployed. Co-located satelites are separated by 0.1 degree in space or approximately 30 kms. Signal interference from the Co-located satellites is prevented by using orthogonal polarisations. Hence a ground station equipment can receive signals from two Co-located satellites without any reorientation of the antenna. The signals can be differentiated based on their polarisation. Space segment : Space Segment is available from organisations which have procured satellites, arranged launches and conducted preliminary tests in-orbit and who then operate these satellites on commercial basis. Transponders : Contained in the satellite body are a number of transponders, or repeaters.
The various frequency bands are as below –
Internationally Ku-Band is a popular frequency band in use. The Ku- Band by virtue of its higher frequency can support traffic with smaller antenna sizes in comparison to C / Ext-C Band. It is , however, susceptible to rain outages making it unsuitable for use in South East Asian regions. Indian service providers are presently allowed to hire space segment only on the INSAT series and operate in Ext-C band only. Ext-C band is available only on the INSAT series of satellites and is not a standard band available internationally.
Ascertains that the RF equipment would cater to the requirements of the network topology and satellite modems in use. The link Budget estimates the ground station and satellite EIRP required. Equivalent isotropically radiated power (EIRP) is the power transmitted from a transmitting object. Satellite ERP can be defined as the sum of output power from the satellite’s amplifier, satellite antenna gain and losses. Calculations of signal levels through the system (from originating earth station to satellite to receiving earth station) to ensure the quality of service should normally be done prior to the establishment of a satellite link. This calculation of the link budget highlights the various aspects. EIRP required at the transmitting VSAT, Satellite EIRP which will be required for a desired specified gain of this receiving system. Apart from the known losses due to various cables and inter - connecting devices, it is customary to keep sufficient link margin for various extraneous noise which may effect the performance. It is also a safeguard to meet eventualities of signal attenuation due to rain/snow. As mentioned earlier a satellite provides two resources, bandwidth and amplification power. In most VSAT networks the limiting resource in satellite transponder is power rather than bandwidth. With all their advantages, VSATs are taking on an expanding role in a variety of interactive, on-line data, voice and multimedia applications. Whether it is gas station service, rural telephony, environmental monitoring, distance learning / remote training or the Internet, VSATs are truly poised to be the Space Age Technology. © Muhammad Ali Khan 2003 |
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