|
The GPS is a space-based
radio-positioning and time transfer system. The GPS has
three major segments: Space Division, Control Segment,
and User Equipment Division. As a universal positioning
system, GPS provides several characteristics not found in
other existing equipment which will
enhance the conduct of mission operations: Extremely
accurate (3-dimensional) position, velocity and time
(PVT) determination; a worldwide common grid easily
converted to other local datums; passive, all weather
operation; real-time and continuous information; and
survivability in a hostile environment.
|
For a casual
browsing of the system and its military and civil uses,
please visit the Aerospace Corporation's GPS System Principles. For an excellent introduction
of GPS policy and description please visit this USNO page.
|
Navstar
GPS Fact
Sheet
The Navstar GPS Joint Program Office
(JPO) is a joint service effort directed by the US Air Force and
managed at the Space and Missile Systems Center (SMC), Air Force Space
Command, Los Angeles Air Force Base, California. The JPO is the Department of Defence (DoD)
acquisition office for developing and producing GPS satellites, ground
systems, and military user equipment. The GPS constellation is
operated and controlled by the 50th Space Wing's (Air Force Space
Command) 2nd Space Operations Squadron, Schriever Air Force Base,
Colorado.
GPS is a space-based
radio-positioning system nominally consisting of a 24-satellite
constellation that provides navigation and timing information to
military and civilian users worldwide. GPS satellites, in one of six
medium earth orbits, circle the earth every 12 hours emitting
continuous navigation signals on two different L-band frequencies, L1
and L2. In addition to the satellites, the system consists of a
worldwide satellite control network and GPS receiver units that
acquire the satellite's signals and translate them into precise
position and timing information.
GPS provides the following:
- 24-hour, worldwide service
- Highly accurate, three-dimensional
location information
- Precision velocity and timing
services
- Accessibility to an unlimited
number of global military, civilian, and commercial users
The GPS satellite control system
consists of five monitor stations and four ground antennas around the
globe. The monitor stations use high fidelity GPS receivers to
passively track the navigation signals of all the satellites.
Information from the monitor stations is then processed at the Master
Control Station, operated by the 2nd Space Operations Squadron at
Schriever Air Force Base, Colorado, and used to accurately update the
satellites' navigation messages. The Master Control Station sends
updated navigation information to the GPS satellites through ground
antennas using an S-band signal. The ground antennas are also used to
transmit commands to satellites and to receive the satellites'
telemetry data.
Four generations of GPS satellites
have flown in the constellation: the Block I, the Block II, the Block
IIA, and the Block IIR. Block I satellites were used to test the
principles of space-based navigation, and lessons learned from these
11 satellites were incorporated into later blocks. Block II, IIA and
IIR satellites make up the current constellation.
Block IIRs began replacing older
Block II/IIAs on 22 July 1997. There are currently twelve Block IIR
satellites in orbit.
Block IIR satellites boast dramatic improvements over the previous
blocks. They also have reprogrammable satellite processors enabling
problem fixes and upgrades in flight. Seven Block IIR satellites are
being modernized to radiate the new military (M-Code) signal on both the
L1 and L2 channels as well as the more robust civil signal (L2C) on
the L2 channel. The M-Code signal is a more robust and capable signal
architecture. The first modernized Block IIR (designated as the IIR-M)
was launched on 25 Sep 2005.
Block IIF satellites are the next
generation of GPS Space Vehicles. Block IIF provides all the
capabilities of the previous blocks with some additional benefits as
well. Improvements include an extended design life of 12 years, faster
processors with more memory, and a new civil signal on a third
frequency (L5). The first Block IIF satellite is scheduled to launch in
2008.
GPS continues to perform as the
world's premier space-based positioning and navigation system.
Endeavors such as mapping, aerial refueling, rendezvous operations,
geodetic surveying, and search and rescue operations have all
benefited greatly from GPS's accuracy. GPS capabilities are integrated
into nearly all facets of US military operations. GPS receivers are
incorporated into nearly every type of system used by the DoD:
aircraft, spacecraft, ground vehicles and ships. In addition,
GPS-guided munitions have showcased their increased accuracy in recent
conflicts with unprecedented precision, thus improving military
capability while decreasing the number of weapons required to achieve
military objectives.
As a service to GPS users, the
Department of Transportation has established the "Navigation
Information Service" (formerly "GPS Information
Service") as a point of contact for civil GPS users. Operated and
maintained by the United States Coast Guard, the NIS can be reached at
(703) 313-5900, seven days a week, 24 hours a day, and at
www.navcen.uscg.gov.
Top
GPS SATELLITES ON ORBIT
|
BLOCK
II/IIA SATELLITE CHARACTERISTICS
|
|
Heritage Signals: L1, C/A and L1, L2 P(Y)
First Launch: 14 Apr 89
28 Procured. 16 Healthy On-Orbit (1 Block IIs, 15 Block IIAs)
Weight (in orbit): 2,175 pounds
Orbit altitude: 10,988 nautical miles
Power source: solar panels generating 700 watts
Launch vehicle: Delta II
Dimensions: 5 feet wide, 17.5 feet long (including wing span)
Design life: 7.5 years
|
BLOCK
IIA |
BLOCK IIR SATELLITE CHARACTERISTICS
|
|
Heritage Signals: L1, C/A and L1, L2 P(Y)
First Launch: 22 Jul 97
21 Procured. 12 healthy on-Orbit
Weight (in orbit): 2370 pounds
Orbit altitude: 10,988 nautical miles
Power source: Solar panels generating 1136 watts
Launch vehicle: Delta II
Dimensions: 5 feet wide, 6.33 feet in diameter, 6.25 feet high (38.025 feet wide including wingspan)
Design life: 10 years |
BLOCK IIR |
GPS SATELLITES IN DEVELOPMENT
|
BLOCK IIR-M SATELLITE CHARACTERISTICS
|
|
Heritage Signals: Same as Blocks II/IIA/IIR
Modernized Signals: Adds 2nd civil signal on L2
Also adds new L1 & L2 M-Code Signal
First Launch: 25 Sep 2005
7 Block IIRs will be modernized into IIR-Ms
1 healthy on-orbit
Weight (in orbit): 2370 pounds
Orbit altitude: 10,988 nautical miles
Power source: Solar panels generating 1136 watts
Launch vehicle: Delta II
Dimensions: 5 feet wide, 6.33 feet in diameter, 6.25 feet high (38.025 feet wide including wingspan)
Design life: 10 years |
BLOCK IIR-M |
|
|
BLOCK IIF SATELLITE CHARACTERISTICS |
|
Signals: All the capabilities of previous Blocks
Plus a 3rd civil signal on L5
First Launch: 2008
12-19 satellite production run
Weight (in orbit): 3439 pounds
Orbit altitude: 10,988 nautical miles
Power source: Gallium Arsenide solar panels generating up to
2900 watts (BOL) & 2400 watts (EOL)
Launch vehicle: EELV (Delta IV and Atlas V)
Dimensions: 9.6 ft x 6.47 ft (stowed) ft (43.1 ft wide including wingspan) x 12.9 ft
Design life: 12 years |
BLOCK
IIF |
(Current as of April 2006)
|
Top
|
Most Frequently Asked Questions & Answers on GPS
How was GPS developed?
A: From an idea that took shape during the "race to space" between the United States and the Soviet Union in the late 1950's, scientists at John
Hopkins University developed a way to use radio signals originating from a satellite in space to provide accurate position updates to navigation
equipment located on the U.S. Navy's ships and submarines. By the mid-1960's, the Air Force initiated a program consisting of several satellites
with very accurate clocks onboard that could give off timing signals of their location in space which would accurately determine the position of a
vehicle moving on land or in the air. In 1973, the Navy and the Air Force programs combined to form the Navigation Technology Program, which
later evolved into the Navstar Global Positioning System (GPS) in operation today.
Navstar GPS is the world's premier position, navigation and timing information service. The U.S. military and its allies are not the only
beneficiaries of Navstar GPS however; civilian users around the globe rely upon Navstar GPS as well. In fact, the system serves millions of civil
users. Over 1.4 million civilian GPS receivers have been produced each year since 1997. Perhaps very few individuals realized early on the
financial impact that GPS would have in the global financial landscape. This is not the case now. The rapidly growing GPS market, including
equipment and applications, reached $6.2 billion in 2000 and is expected to easily surpass $50 billion by 2010.
Can I get a good layman's description of how it works?
A:
Managed by the Navstar GPS Joint Program Office at the Space and Missile Systems Center at Los Angeles Air Force Base, California,
Navstar GPS is a space-based radio navigation and time distribution system. The GPS constellation consists of 24 or more satellites, which orbit
the Earth in six distinct orbital planes at an altitude of 10,900 nautical miles. GPS satellites circle the Earth twice per day and continuously
transmit signals, which provide navigation and timing information to military and civilian users worldwide. GPS consists of three main elements,
or "segments." In addition to the satellites themselves -- called the "Space" segment --the system includes a worldwide satellite control network --
the "Control" segment -- and GPS receiver units -- called the "User" segment. GPS receivers use the signals from the satellites to compute
position and time information for users. The receivers do not send out any signals, or communicate back to the satellites.
The fundamental concept of GPS is to use simultaneous distance measurements from four satellites to compute the position and time of any
receiver. The GPS satellites broadcast signals on two different frequencies so that sophisticated user receivers can correct for distortion effects
due to the ionosphere, a layer of the atmosphere several hundred miles above the Earth. It takes between 65 and 85 milliseconds for a signal to
travel from a GPS satellite to a receiver on the surface of the Earth. The signals are so accurate that time can be figured to much less than a
millionth of a second, velocity can be figured to within a fraction of a mile per hour, and location can be figured to within a few meters. Typical
horizontal positioning accuracy for military users is 5 to 10 meters, while for single frequency users is 10 to 20 meters.
What type of timing device is used on the GPS satellites and how
accurate are they?
A:
The GPS constellation presently (June 2005) consists of 1 Block II and 15 Block IIA satellites built by Boeing, and 7 Block IIR satellites
built by Lockheed Martin. 8 Block IIRs remain to be launched. Each Block II or IIA satellite has two cesium atomic clocks and two
rubidium atomic clocks, while each Block IIR has three rubidium atomic clocks. The stability of these clocks is estimated to be approximately 1
second per 300,000 years. (Atomic clocks utilize the vibration of atoms to achieve their accuracy. They are not nuclear powered.) Only one
clock is in use on each satellite at a time. The others are backups.
What powers the satellites?
A:
Each Block II/IIA satellite has two solar arrays, each 67" by 130". Each Block IIR solar array consists of two panels (four total on each
satellite), with each panel 70" x 75". In addition to providing power to the satellite, the solar arrays are also used to charge batteries, which the
satellite uses for power whenever it is in darkness. The Block II/IIA satellites have three nickel-cadmium batteries and the Block IIR satellites
have two nickel-hydrogen batteries.
How much does it cost to operate?
A:
The approximate cost to operate and maintain the constellation, including research and development, as well as, procurement for replenishment
satellites, is $750M annually.
Can you describe what it takes to operate the system, and what they
have to do to keep the satellites and signals working, etc.
A:
The GPS worldwide satellite network consists of six monitor stations and four ground antenna stations. The monitor stations (located at
Ascension Island, Cape Canaveral, Colorado Springs, Diego Garcia, Kwajalein and Hawaii) use specially designed GPS receivers to passively track
the navigation signals of all of the satellites. Data from the monitor stations is continually sent to the GPS Master Control Station (MCS), located
at Schriever Air Force Base, Colorado, for processing. The MCS computes precise, updated information on the satellites' orbits and clock status
every 15 minutes, 24 hours a day, seven days a week. Updated navigation information is sent from the MCS to the ground antenna stations (located
at Ascension Island, Cape Canaveral, Diego Garcia and Kwajalein) and then to the satellites. These "uploads" are done once or twice per day for
each satellite. This is sufficient to maintain the high accuracy of the GPS constellation.
In addition to uploads, the ground antennas are also used to transmit commands to the satellites and to receive the satellites' telemetry data. In
addition to the MCS, the Air Force currently maintains an interim backup Master Control Station near Washington, DC, while a permanent
alternate Master Control Station is under construction at Vandenberg AFB, California.
Can you tell me how many civilian companies make products that use
GPS?
A: Although the Air Force does not keep track of the number of civilian companies that make GPS-related products, it is commonly known that
civil users outnumber military users by 100 to 1 and the ratio is increasing. The Compound Annual Growth Rate of the GPS market is growing by
approximately 22%. The Department of Commerce conducted a comprehensive market study in September 1998. The study expected worldwide
sales to reach $4B by the end of 1998. Sales continued to grow by a little over $1B per year through 2000 to $6.2B.
What does a civilian company have to do to use the signal?
Don't they have to get some sort of code?
A:
To access GPS for general use, a person may purchase a handheld receiver or a vehicle equipped with a GPS navigation system. The signal is
free to all users worldwide. No subscription, license, fee or registration is required.
What plans are underway to ensure the reliability of GPS in the
future?
A:
To ensure the best GPS system for the next 30 years, the future of GPS includes increased power and accuracy, as well as increased civil
navigation safety with the addition of a new civil signal on the L2 link and a new civil-only signal on a new link, L5, to be broadcast at 1176.45
MHz. A new military-only signal (M-code) on the L1 and L2 links is programmable for completion in 2010. It will have increased power and
reduced vulnerability to signal jamming. In addition to the improved signals, the reliability of the GPS navigation message will be improved by
adding more monitor stations. These additional monitor stations will ensure that each satellite is simultaneously monitored by no less than two
monitor stations. The data collected by these additional monitor stations will be combined with the data from the existing monitoring stations, and
sent to the MCS for processing. The result is improved accuracy of the navigation message broadcast by the satellite.
For
your further research:
As a service to GPS users, the DoT has established the �Navigation
Information Service� (formerly �GPS Information Service�) as a
point of contact for GPS users. Operated
and maintained by the U.S. Coast Guard, the NIS can be reached at
(703) 313-5900 seven days a week, 24 hours a day and at www.navcen.uscg.gov.
For more detailed overviews of GPS, log onto: www.aero.org/publications/GPSPRIMER
There are also many books
about GPS available today, with more published all the time. They
cover topics ranging from recreational and commercial applications of
GPS to highly technical engineering volumes for scientists and
engineers.
(Current as of June 2005)
| GPS
Fact Sheet | FAQ | Front Office (GP)
Home |
| Navstar GPS JPO | Warning
| Top of this page |
|