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  • What is the introduction of communication satellite?

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  • What are the 3 types of satellite communication?

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  • What are the 4 main types of satellites?

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  • Satellite Communications involves communication using the electromagnetic spectrum between ground receivers and transponders on artificial satellites. Satellite communications are involved in most parts of our daily lives. It is hard to imagine life without satellite communications.

Fundamentals of Satellite

Communications, Part 1

Howard Hausman

President

MITEQ, Inc.

Hauppauge, NY 11788

May 29, 2008

05/29/08 Howard Hausman, MITEQ, Inc. 2

Fundamentals of Satellite

Communications Part 1

Satellite Communications Introduction

Types of Satellite Services

Satellite Configurations

Geostationary Satellites

Non-Geostationary Satellites

Satellite Configurations

Frequency Reuse / Polarization

Earth Station Antennas

Major Earth Stations Components

Satellite Communications Summary

Part 2 - Communication System Link Analysis

Part 3 - Specifying Subsystems for Data

Communications

05/29/08 Howard Hausman, MITEQ, Inc. 3

Satellite Communications

Introduction

?Are Satellites a Cost Effective Means of Communications? Answer is NO. ?Limited Frequency Spectrum ?Limited Spatial Capacity (Orbital Slots) ?High Equipment Cost ?Land lines and Fiber are Much More Cost Effective ?Fiber Reuses Spectrum, Multi-Fiber Cables ?A few multi-fiber cables can have as much information as all the satellites in orbit ?Land Line Infrastructure is In Place

05/29/08 Howard Hausman, MITEQ, Inc. 4

Adaptable to the needs of different customers

Variable Information Rates

Mobility

Cost advantage over building land lines for a limited population

Versatility in use Paging, Voice, Data, Video

No geographical obstructions that prohibit landlines

Quick implementation - e.g. News Gathering

Alternate routing or redundancy as required

Cost is independent of distance

Cost effective for short term requirements e.g.

Sporting Events

Satellites Provides Capabilities Not Available

with Terrestrial Communication Systems

05/29/08 Howard Hausman, MITEQ, Inc. 5

Types of Satellite Services

Fixed Service Satellites (FSS)

Communication to non-moving satellites.

Generally Earth Station is not moving when in use.?

Low Cost Tracking antennas are making

communication on the move a reality

Types of service?

Video:

?Broadcast: Television network distribution ?Satellite News Gathering (SNG).

Voice:

?Telecommunications traffic / connecting cells. ?Connecting cellular telephone to small islands

Data: Internet, Business to Business

05/29/08 Howard Hausman, MITEQ, Inc. 6

Satellite Industry Issues and Concerns

?Frequency spectrum ?Orbital Slots ?Regulatory inconsistencies?Signals reach multiple countries ?Consolidation of manufacturers ?Multiple standards ?Quality control versus production lead time ?Rapid change in telecommunications requirements?Digital Television ?Rapid deployment of Fiber optics

05/29/08 Howard Hausman, MITEQ, Inc. 7

Satellite Configurations & Stabilization

05/29/08 Howard Hausman, MITEQ, Inc. 8

Satellite Components

•Propulsion System •Telemetry •Attitude Control •Fuel •Batteries •Power & Thermal Control •Solar Arrays ?LNA ?Down Converter ?High Power Amplifier ?Filter

Up Link

Path Loss

Down Link

Path Loss ?Up Link

Frequency Always

Higher than Down

Link Frequency

05/29/08 Howard Hausman, MITEQ, Inc. 9

Spin Stabilized Satellites

Satellite Body is Spin

Stabilized (60-100 RPM)

Gyroscopic stability

Spins to minimize thermal

effects

1/2 the solar cells face the

sun at one time

More efficient for smaller

satellites

Antenna must de-spun

Spin

Stabilized

05/29/08 Howard Hausman, MITEQ, Inc. 10

Body Stabilized Satellites

All solar cells face the

sun

Thermal control more

difficult

Requires more

stabilization control

More solar cells than

Spin Stabilized Satellites

Better design for larger

satellites

Body Stabilized

05/29/08 Howard Hausman, MITEQ, Inc. 11

Geo-Stationary Satellites

In a British magazine, "Wireless World", May, 1945, Arthur Clark, a renown science fiction author, wrote a paper predicting that three geo-stationary satellites would provide complete global telecommunications coverage.

Sir Arthur Clark

wrote '2001, A

Space Odyssey"

Died this year

2008

05/29/08 Howard Hausman, MITEQ, Inc. 12

Geo-Stationary Satellites

(Continued)

Clark Orbit, which is Equatorial Circular

35,800km (22,300 Miles ) above the Earth traveling

at a speed of 11,000km/hour?

One Orbit takes 24 hours

Synchronous with the spinning of the Earth

Satellites headed for geosynchronous orbit first go to a Geostationary Transfer Orbit (GTO) ?Elliptical orbit with apogee about 23,000 miles. ?Firing the rocket engines at apogee then makes the orbit circular. A Single Satellite is visible from ≈≈≈≈1/3 of the earth"s surface, excluding extreme Polar Regions. Cannot see latitudes greater than ±±±±77°°°° Orbital locations are regulated by the International telecommunications Union (ITU)

05/29/08 Howard Hausman, MITEQ, Inc. 13

Geo-Stationary Satellites Beams

?Generally satellites must be spaced at least 1.5°°°°to 2°°°°apart (2°°°° ≈≈≈≈911 miles

or 1,466 Km ?Earth Station antenna will illuminate multiple satellites if they are spaced closer ?Orbital slots are measured in degrees going East from Greenwich meridian = 0°°°° •Satellite antenna beam width is 17.3°°°° for full earth coverage

05/29/08 Howard Hausman, MITEQ, Inc. 14

Advantages/Disadvantages

of Geo-Synchronous Orbits Advantages:■No ground station tracking required ■No inter-satellite handoff, permanently in view ■Three satellites give full earth coverage ■Almost no Doppler shift, yields reduced complexity receivers Disadvantages:■35786 km orbits imply long transmission latencies ■Weak received signal ■Poor coverage at high latitudes (>77 degrees)

05/29/08 Howard Hausman, MITEQ, Inc. 15

Satellite Link Delays

Satellite to the surface of the Earth is 22,300 miles

Two way transmission is 44,600 miles

C = speed of light = 186,282 miles per second

239 milliseconds Minimum delay?

Transmit and receive

stations on the equator at the same longitude as the satellite.

Typical signals may required

two hops through the satellite, i.e. around

500mSec?

500mS echo is barely

distinguishable >120 ms >120 ms

120 ms

05/29/08 Howard Hausman, MITEQ, Inc. 16

Elevation & Slant-Range

Not All Satellites are located above the Earth Station

At Higher Elevation Angles■

Signals Traverse Less Atmosphere

Overall Slant-Range is Reduced.

Signal Strength is Inversely Proportional to the Square of the Distance Atmospheric Effects are Significant at Low elevation

Note the difference

in traversed atmosphere

Top of the Atmosphere

05/29/08 Howard Hausman, MITEQ, Inc. 17

Elevation Angles & Atmospheric Effects

?Minimum Elevation Angles ?C-Band Elevations ≥≥≥≥5°°°° ?Ku-Band Elevations ≥≥≥≥10°°°° Low

Elevation

Angle High

Elevation

Angle

Atmospheric Effects are

critical to signal path Loss

22,300 miles Earth to

Satellite■

1st5 miles is most critical

> 5 miles at low angles of elevation

Atmospheric Problems■

Potential interference

from terrestrial sources.

Increased atmospheric

absorption

Partially depolarizes

signal

05/29/08 Howard Hausman, MITEQ, Inc. 18

Geo-Stationary Satellite Movement

North-South perturbations?

Due to gravitational pulls of the Sun and Moon (Similar to Tidal Effects)

North-South perturbations are the largest

Most demanding on satellite fuel reserves

East-West perturbations?

Due to lumpiness of the Earth

Incorrect satellite velocity & altitude

North-South

East-West

05/29/08 Howard Hausman, MITEQ, Inc. 19

North-South Satellite Movement

?An Object not exactly over the equator , transcribes a figure eight pattern to an observer on Earth ?Satellite lateral errors can be as much as ±±±±3 °°°°at end of life ?Looks like an up and down motion two times every 24 hours ?Large Earth Station Antennas must track the motion

05/29/08 Howard Hausman, MITEQ, Inc. 20

Satellite Orbit Stabilization & Life

Positioning is regularly corrected to within ±±±±0.1°°°° Without correction the movement in the North-South direction will be about 0.85 °°°°per year? ±±±±15°°°°over the satellites typical 12 year lifetime Life of satellite is determined by how much fuel is stored to correct its position? Last remaining fuel is used to move the satellite out of orbit Satellite fuel capacity is typically designed for 13 years, because the satellite technology becomes obsolete. Satellite life can be extended by making less frequentquotesdbs_dbs14.pdfusesText_20
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