satellite system
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Satellite System. Azizol Bin Abdullah [email protected] (A2.04) Rujukan: Text Book Chapter 11. The First Satellite. The Soviet Sputnik satellite was the first to orbit Earth, launched on October 4, 1957. Sputnik was a 23-inch (58-cm), 184-pound (83-kg) metal ball. - PowerPoint PPT PresentationTRANSCRIPT
The First Satellite The Soviet Sputnik
satellite was the first to orbit Earth, launched on October 4, 1957.
Sputnik was a 23-inch (58-cm), 184-pound (83-kg) metal ball.
After 92 days, gravity took over and Sputnik burned in Earth's atmosphere.
Satellite-Related Terms Earth Stations – antenna systems on or near earth Uplink – transmission from an earth station to a
satellite Downlink – transmission from a satellite to an
earth station Transponder – electronics in the satellite that
convert uplink signals to downlink signals
Ways to CategorizeCommunications Satellites Coverage area
Global, regional, national Service type
Fixed service satellite (FSS) Broadcast service satellite (BSS) Mobile service satellite (MSS)
General usage Commercial, military, amateur, experimental
Geometry Terms Elevation angle - the angle from the
horizontal to the point on the center of the main beam of the antenna when the antenna is pointed directly at the satellite
Minimum elevation angle Coverage angle - the measure of the portion
of the earth's surface visible to the satellite
Minimum Elevation Angle Reasons affecting minimum elevation angle
of earth station’s antenna (>0o) Buildings, trees, and other terrestrial objects
block the line of sight Atmospheric attenuation is greater at low
elevation angles Electrical noise generated by the earth's heat
near its surface adversely affects reception
Classification of Satellite Orbits Circular or elliptical orbit
Circular with center at earth’s center Elliptical with one foci at earth’s center
Orbit around earth in different planes Equatorial orbit above earth’s equator Polar orbit passes over both poles Other orbits referred to as inclined orbits
Altitude of satellites Geostationary orbit (GEO) Medium earth orbit (MEO) Low earth orbit (LEO)
Frequency Bands Available for Satellite Communications
Satellite Link Performance Factors Distance between earth station antenna and
satellite antenna For downlink, terrestrial distance between earth
station antenna and “aim point” of satellite Displayed as a satellite footprint (Figure 9.6)
Atmospheric attenuation Affected by oxygen, water, angle of elevation, and
higher frequencies
Satellite Footprint
Satellite Network Configurations
Capacity Allocation Strategies Frequency division multiple access
(FDMA) Time division multiple access (TDMA) Code division multiple access (CDMA)
What is Global Positioning System(GPS) ?
3D Coordinates for Fixed and Moving Objects on Earth A Nanosecond accurate universal time. Information and data about the atmosphere around the
globe Time & Location data for military purposes Managed and controlled by the U.S. Defense Dept.
Global Positioning System (GPS)
Started development in 1973 First four satellites launched in 1978 Full Operational Capacity (FOC) reached on July 17, 1995 System cost of $12 billion GPS provides both civilian and military positioning globally GPS comprised of three “segments”
Space Segment (the satellites) Ground Segment (the ground control network) User Segment (GPS receiver and their users)
GPS Satellite NAVSTAR GPS
satellite
The GPS System ArchitectureOverview
The GPS System Architecture The Space Segment
The Space-Segment consists of the combination of satellites that orbit the globe. The space segment of the NAVSTAR constellation includes at least 24 orbiting satellites
Orbiting Earth every 12 hours
Located at 20.200km from
Earth’s Surface
Orbiting Earth every 12 hours
Located at 20.200km from
Earth’s Surface
60 degrees apart,
55 degrees to
the Equator
60 degrees apart,
55 degrees to
the Equator
24 or more GPS Satellites
Called a Constellation
(e.g. NAVSTAR)
24 or more GPS Satellites
Called a Constellation
(e.g. NAVSTAR)
Space SegmentSpace Segment
The GPS System Architecture The Space Segment
The GPS Constellation consists of 24 satellites distributed on 6 orbital planes positioned at 55 degree inclination. There are 4 satellites in each orbital plane.
The orbits are at distances exceeding 20,200 km above the surface of Earth.
The GPS System Architecture The Space Segment
The GPS System Architecture The Space Segment
The GPS System Architecture The User Segment
The User –Segment consists of all agencies, organizations, businesses, and individuals who use GPS.
GPS ReceiversCommunication devices
that receive and analyze
signals from the
GPS Constellation.
GPS ReceiversCommunication devices
that receive and analyze
signals from the
GPS Constellation.
End User Software
Applications (e.g. surveying)
End User Software
Applications (e.g. surveying)
PeopleIndividuals, researchers,
businessmen, …etc.
PeopleIndividuals, researchers,
businessmen, …etc.
User SegmentUser Segment
The GPS System Architecture The User Segment
The user -segment consists of all agencies, organizations, businesses, and individuals who use GPS.
The transportation industry makes the most use of GPS primarily for global navigation.
The GPS System Architecture The Control Segment
Control stations is where satellite atomic time, orbits, and other data are monitored and corrected if necessary.
The Master Control station for the NAVSTAR constellation of the 24 satellites is located in the Falcon AFB Colorado Springs - USA.
Updates, Upgrades,
CorrectionsAuthorization and
Access Control
Updates, Upgrades,
CorrectionsAuthorization and
Access Control
Different Ground Controls
Stations
Located in USA, Hawaii,
Diego Garcia, & other
places.
Different Ground Controls
Stations
Located in USA, Hawaii,
Diego Garcia, & other
places.
Master Control Station(Air Force Base)
Colorado, U. S. A.
Master Control Station(Air Force Base)
Colorado, U. S. A.
Control SegmentControl Segment
The GPS System Architecture The Control Segment
GPS Master Control and Monitor Station Network
Using the GPS Technology GPS Services (The U.S. Federal Radio Navigation
Plan)
Precise Positioning Service (PSS) Horizontal Accuracy (X, Y Coordinates): 22
meters. Vertical Accuracy (Z Coordinate): 27.7 meters Time Accuracy: 100 nanoseconds (10-7 seconds) Authorized Access Only (using signal encryption)
Military Applications and Authorized Government Agencies & Organizations
Using the GPS Technology GPS Services (The U.S. Federal Radio Navigation
Plan)
Standard Positioning Service (SPS) Horizontal Accuracy (X, Y Coordinates): 100
meters Vertical Accuracy (Z Coordinate): 156 meters Time Accuracy: 340 nanoseconds (3.4 x 10-7
seconds) Access to All Users (without restrictions or
charges)
Civil Applications (Individuals, Researchers, Businesses, …etc.)
Using the GPS TechnologyCalculating Positions: Sat-
Ranges Circles in plain colors represent GPS
satellite ranges with respect to a moving object on the ground, on the sea, or in the air. The position and tie of the GPS device (I.e. receiver) is where the satellite ranges intersect.
In reality, the physical satellite ranges are those shown in dotted lines. The difference is actually the clock bias to compensate for the delay in receiving the GPS signals.
These satellite ranges are used internally by the GPS device to calculate the position of the device at the time the GPS signals from the four satellites are received.
Note: A GPS device might be able to receive signals from many satellites but only 4 are needed to determine its position and time (i.e. Position Fix).
Using the GPS Technology How To Get A Position
Need signal from at least four satellites for 3D position
One SV provides a time reference
Distance to three remaining satellites is determined by observing the GPS signal travel time from SV to the receiver
With three known points, and distances to each, we can determine the GPS receiver’s position (trilateration)
Using the GPS TechnologyCalculating Positions -
ECEF(XYZ) The Earth Centered, Earth Fixed
(ECEF) coordinate system is a 3D frame of reference. In this frame, everything on the ground, under the ground, or in the air has a unique set of (X,Y,Z) coordinates.
A GPS satellite signal includes information about “orbital elements” of the satellite. This information is known as the "Ephemeris Data". The collection of these Ephemeris Data from each of the GPS Constellation satellites is known as the "Almenac".
A GPS receiver (i.e. device) receives signals from satellites and computes their position in the ECEF coordinate system using the “orbital elements” specified in the "Almenac". Once these positions are computed, the position of the GPS receiver itself (i.e. the intersection of the satellite ranges) can be computed.
Using the GPS TechnologySources of Position Errors
Atmosphere Ionosphere & Troposphere Selective Availability - Intentional
(Most Frequent) Noise Errors causing Data Errors Blunder Errors - Satellite Loss of
Orbit (Very Rare)
Using the GPS TechnologyCorrecting the Errors : Differential -
GPS The lack of precision in GPS
position caused primarily by errors can be minimized to a certain extent using a method known as "Differential GPS".
This method consists of using an additional GPS device at a fixed base station whose position is already known. The shift in position of a mobile GPS device (due to errors) can be corrected to some extent using the known position of the fixed GPS device.
Note: Position shift correction using Differential GPS is only partial. It does however in some situations improve precision quite considerably.
GPS Applications Industry & Business
Geography: Mapping & Surveying Agriculture Telecommunications Transportation & Vehicle Tracking
Aviation (Military & Civil), Land Transport, Marine Transport, Space
Travel,…etc.
Science & Research Archeology Atmospheric Science and the Environment Geodesy Geology & Geophysics
Leisure & Recreation Sea, Air, Land
GPS User Devices
GPS User Devices
GPS User Devices