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COMMUNICATION SATELLITE LINK DESIGN

WEEK 5

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Information

Recommended Study Material:

 Book-1: Electronic Communication Systems, By George

Kennedy Book-2: Satellite Communications, By D.C Agarwal

Lecture Notes

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COMMUNICATION SATELLITE LINK DESIGN

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Topics:

Introduction

General Link Design Equations

System Noise temperature, C/N and G/T

Ratios

(5)

Design of the Satellite Link:

The satellite link is probably the most basic in

microwave communications since a line-of-sight path typically exists between the Earth and space.

 This means that an imaginary line extending

between the transmitting or receiving Earth station and the satellite antenna passes only through the atmosphere and not ground

obstacles.

 Such a link is governed by free-space

propagation with only limited variation with respect to time due to various constituents of the atmosphere.

(6)

Design of the Satellite Link

 Free-space attenuation is determined by

the inverse square law, which states that the power received is inversely proportional to the square of the distance.

 The same law applies to the amount of light that

reaches our eyes from a distant point source such as an automobile headlight or star.

 There are, however, a number of additional

effects that produce a significant amount of degradation and time variation.

 These include rain, terrain effects such as

absorption by trees and walls, and some less-obvious impairment produced by unstable

(7)

Design of the Satellite Link

It is the job of the communication

engineer to identify all of the significant

contributions to performance and make

sure that they are properly taken into

account.

The required factors include the

(8)

Design of the Satellite Link

Also important is the efficient transfer of

user information across the relevant

interfaces at the Earth stations, involving

such issues as the precise nature of this

information, data protocol, timing, and the

telecommunications interface standards

that apply to the service.

A proper engineering methodology

(9)

Design of the Satellite Link

Baseband

The basic direct output signal in an intermediate frequency based obtained directly from a television camera, satellite television receiver, or video tape recorder. Baseband

signals can be viewed only on studio monitors. To display the baseband signal on a conventional television set a "modulator" is required to convert the baseband signal to one of the VHF or UHF television channels which the

television set can be tuned to receive.

Carrier

The basic radio, television, or telephony center of

(10)

Design of the Satellite Link

 The RF carrier in any microwave communications

link begins at the transmitting electronics and propagates from the transmitting antenna

through the medium of free space and absorptive atmosphere to the receiving antenna, where it is recovered by the receiving electronics.

 The carrier is modulated by a baseband signal

that transfers information for the particular application.

 The first step in designing the microwave link is to

identify the overall requirements and the critical components that determine performance.

 For this purpose, we use the basic arrangement of

(11)

Design of the Satellite Link

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Design of the Satellite Link

LNB (LOW NOISE BLOCK DOWN CONVERTER)

 A device mounted in the dish, designed to amplify the satellite

signals and convert them from a high frequency to a lower

frequency. LNB can be controlled to receive signals with different polarization. The television signals can then be carried by a double-shielded aerial cable to the satellite receiver while retaining their high quality. A universal LNB is the present standard version, which can handle the entire frequency range from 10.7 to 12.75 GHz and receive signals with both vertical and horizontal polarization.

Demodulator

A satellite receiver circuit which extracts or "demodulates" the "wanted "signals from the received carrier.

Decoder

 A box which, normally together with a viewing card, makes it

(13)

Design of the Satellite Link

Modulation

The process of manipulating the frequency or amplitude of a carrier in relation to an incoming video, voice or

data signal.

Modulator

A device which modulates a carrier. Modulators are

found as components in broadcasting transmitters and in satellite transponders. Modulators are also used by CATV companies to place a baseband video television signal onto a desired VHF or UHF channel. Home video tape recorders also have built-in modulators which

enable the recorded video information to be played

(14)

Design of the Satellite Link

The example shows a large hub type

Earth station in the uplink and a small

VSAT in the downlink; the satellite is

represented by a simple frequency

translating type repeater (e.g., a bent

pipe).

Most geostationary satellites employ

bent-pipe repeaters since these allow the

widest range of services and

(15)

Design of the Satellite Link

Bidirectional (duplex) communication

occurs with a separate transmission from

each Earth station.

Due to the analog nature of the radio

frequency link, each element contributes

a gain or loss to the link and may add

(16)

Design of the Satellite Link

Carrier to Noise Ratio (C/N)

The ratio of the received carrier power and the noise power in a given bandwidth, expressed in dB. This figure is directly related to G/T and S/N; and in a video signal the higher the C/N, the

better the received picture.

G/T

A figure of merit of an antenna and low noise

amplifier combination expressed in dB. "G" is the net gain of the system and "T" is the noise

(17)

Design of the Satellite Link

 The result in the overall performance is presented

in terms of the ratio of carrier power to noise (the carrier-to-noise ratio, C/N) and, ultimately,

information quality (bit error rate, video impairment, or audio fidelity).

 Done properly, this analysis can predict if the link

will work with satisfactory quality based on the specifications of the ground and space

components.

 Any uncertainty can be covered by providing an

appropriate amount of link margin, which is over and above the C/N needed to deal with

(18)

Design of the Satellite Link

 The result in the overall performance is presented

in terms of the ratio of carrier power to noise (the carrier-to-noise ratio, C/N) and, ultimately,

information quality (bit error rate, video impairment, or audio fidelity).

 Done properly, this analysis can predict if the link

will work with satisfactory quality based on the specifications of the ground and space

components.

 Any uncertainty can be covered by providing an

appropriate amount of link margin, which is over and above the C/N needed to deal with

(19)

The Received Power

Calculation

General

Link Design

Equations

Geometry of a Radio Link

(20)

The Received Power

Calculation

General

Link Design

Equations

Geometry of a Radio Link

The power density over area A0 is PT/Ao

If AR the effective area of the receiving antenna then poser incident upon is

Directivity GT of the receiving antenna

2.1

(21)

The Received Power

Calculation

General

Link Design

Equations

Combining equation 2.1 and 2.2

Gain of the receiving antenna GR in relation to effective area

AR

Substituting AR of equation 2.4 in 2.3

First Transmission Equation=

The Power attenuation in decibel is, where GT and GR are the gain of

transmitting and receiving antennas in decibel.

2.3

2.4

2.5

(22)

The Received Power

Calculation

General

Link Design

Equations

The product PTGT is called effective isotropic radiated power.

From eq. 2.7 it is clear that path loss increase with frequency

But can be compensated by increasing antenna gain.

Uplink path loss at 6Ghz =199dB Downlink path loss at 4Ghz =196dB

2.7

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The Received Power

Calculation

General

Link Design

Equations

Thus eq. 2.8 cab be written as

2.9

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System Noise temperature, C/N

and G/T Ratios

Noise Power due to thermal noise is given by

Where

K is Boltzmann constant

Ts is system noise temperature B is the bandwidth of the system

If G is the overall Gain

The Noise Power at the demodulator input

2.11

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System Noise temperature, C/N

and G/T Ratios

If Pr is the power reaching at the input of the receiver.

Then the signal power reaching at the input of the modulator is PrG.

The carrier to noise ratio at the demodulator input isA Satellite Receiver RF amplifier

Down converter mixerIF amplifier

And their respective noise temperature is Trf , Tm and Tif

Noise model of an RF receiver

(26)

System Noise temperature, C/N

and G/T Ratios

The total noise power at the output of IF amplifier is

Let Ts be the Noise temperature of the total receiver

2.14

(27)

System Noise temperature, C/N

and G/T Ratios

Equating eq.2.14 with 2.15, we get

Let Ts be the Noise temperature of the total receiver

2.16

(28)

System Noise temperature, C/N

and G/T Ratios

Again using eq. 2.5 and 2.8, eq 2.13 can be written as

The noise power spectral density No =N/B in Watt/Hz

The carrier Power to Noise Power spectral density ratio is

2.17

(29)

System Noise temperature, C/N

and G/T Ratios

Again using eq. 2.5 and 2.8, eq 2.13 can be written as

The noise power spectral density No =N/B in Watt/Hz

The carrier Power to Noise Power spectral density ratio is

2.17

References

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