| NAVSTAR GPS |
GPS design objectives
|
| |
| . |
Suitable for different platforms: aircraft, ship, land-based and space (missiles and satellites), |
| . |
Ability to handle a wide variety of dynamics, |
| . |
Real-time positioning, velocity and time determination capability to an appropriate accuracy, |
| . |
Single global geodetic datum (reference system) for defining position,
|
| . |
Differential accuracy standards:
highest accuracy to be restricted to a certain class of authorized
users, |
| . |
Resistant to jamming (intentional and unintentional), |
| . |
Redundancy provisions to ensure the survivability of the system, |
| . |
Passive positioning system that does not require the transmission of signals from the user to the satellite(s), |
| . |
Ability to provide the service to an unlimited number of users and world-wide coverage |
| . |
Low cost, low power, therefore highly complex satellite segment, |
| . |
Total replacement of the Transit 1 satellite and other terrestrial navigation aid systems. |
| |
| Background
of GPS evolution |
- The US Air Force (USAF) conducted concept
studies for a 3-dimensional navigation system called 621B which
provided three dimensional (latitude, longitude, and altitude)
navigation with continuous service.
In April 1973, the
Deputy Secretary of Defense designated the Air Force as the
lead agency to consolidate the various satellite navigation
concepts into a single comprehensive DoD system to be known
as the Defense Navigation Satellite System (DNSS).
-
By September 1973, a compromise system was
conceptualized which combined the best features of earlier
Navy and Air Force programs and was called Navigation Satellite Timing and Ranging
Global Positioning System or NAVSTAR GPS . The signal
structure and frequencies were taken from the Air Force's
621B. Satellite orbits were based on those proposed for the
Navy's Timation system, but higher in altitude, giving twelve-hour
instead of eight-hour periods (Parkinson and Spilker, 1996).
-
Thus NAVSTAR can be expressed as a combination
of two systems as: NAVSTAR = USN
TIMATION + USAF 621B
-
Popularly known as the Global
Positioning System (GPS), the system was designed
to take over from existing navigation systems.
-
NAVSTAR GPS is a satellite-based, radio
based, radio-positioning and time positioning and time-transfer
system, designed, financed, deployed and operated by the
US DoD.
-
Developed
by the US DoD, GPS is first and foremost a defense military
system for providing worldwide coverage at all time and
all places with a low end user cost and a navigation position
accuracy of 10-20 m.
-
The first test signals from space were
transmitted from the Navigation Test Satellite 2, launched
in June 1977. The first NAVSTAR satellite was launched in
1978. The system was declared to have the full operational
capability (FOC) in 1993.
-
Requiring a minimum of 4 satellites, three
for 3D position and one to keep track of time information
to minimize certain types of errors , GPS
is the most advanced real time positioning technique based
on transmitting a coded satellite message, which could be
received by a ground portable receiving unit (receiver) consisting
of antenna (radio receiving unit mounted on tripod), power
supply source (battery), oscillator (usually quartz crystal),
internal clock ,and mini computer.
|
|