There are three types of GPS receivers, which are available in today's marketplace. Each of the three types offers different levels of accuracy, and has different requirements to obtain those accuracies.


C/A Code receivers
    C/A Code receivers typically provide 1-5 meter GPS position accuracy with differential correction. C/A Code GPS receivers provide a sufficient degree of accuracy to make them useful in most GIS applications.
    C/A Code receivers can provide 1-5 meter GPS position accuracy with an occupation time of 1 second. Longer occupation times (up to 3 minutes) will provide GPS position accuracies consistently within 1-3 meters. Recent advances in GPS receiver design will now allow a C/A Code receiver to provide sub-meter accuracy, down to 30 cm.


Carrier Phase receivers
    Carrier Phase receivers typically provide 10-30 cm GPS position accuracy with differential correction. Carrier Phase receivers provide the higher level of accuracy demanded by certain GIS applications.
    Carrier Phase receivers measure the distance from the receiver to the satellites by counting the number of waves that carry the C/A Code signal. This method of determining position is much more accurate; however, it does require a substantially higher occupation time to attain 10-30 cm accuracy. Initialising a Carrier Phase GPS job on a known point requires an occupation time of about 5 minutes. Initialising a Carrier Phase GPS job on an unknown point requires an occupation time of about 30-40 minutes.
    Additional requirements, such as maintaining the same satellite constellation throughout the job, performance under canopy and the need to be very close to a base station, limit the applicability of Carrier Phase GPS receivers to many GIS applications.


Dual-Frequency receivers
    Dual-Frequency receivers are capable of providing sub-centimetre GPS position accuracy with differential correction. Dual-Frequency receivers provide "survey grade" accuracies not often required for GIS applications.
    Dual-Frequency receivers receive signals from the satellites on two frequencies simultaneously. Receiving GPS signals on two frequencies simultaneously allows the receiver to determine very precise positions.



What is NMEA and SiRF II?
    In order to relay computed GPS variables such as position, velocity, course etc. to a peripheral (e.g. computer, screen, transceiver), GPS modules have a serial interface (TTL or RS-232 level). The most important elements of receiver information are broadcast via this interface in a special data format. This format is standardised by the National Marine Electronics Association (NMEA) to ensure that data exchange takes place without any problems. Nowadays, data is relayed according to the NMEA-0183 specification.
    SirfII is an alternate to NMEA, providing for a new communications protocol. SirfII protocols provide for more complete control of the GPS receiver as well as higher speed communications between the GPS receiver and the mapping/display application



What is WAAS and EGNOS?
    The North-American WAAS system (Wide Area Augmentation System) is a network of approx. 25 ground reference stations (WRS, Wide Area Ground Reference Station) that receive GPS signals. They have been surveyed exactly in terms of their position. Each reference station determines actual and target pseudo-range deviation. The error signals are relayed to a master station WMS (Wide Area Master Station). The WMS's calculate the differential signals and monitor the integrity of the GPS system. The precisely processed DGPS correction values are transmitted to two geo-stationary satellites (Inmarsat) and beamed back to Earth on the GPS L1 frequency (1575.42MHz). The WAAS signals are received by GPS receivers equipped for this task and further processed.

 

    EGNOS (European Geo-stationary Navigation Overlay System) is a satellite-based augmentation system for existing GPS and Glonass satellite navigation systems. A European network of GPS/Glonass receivers has been built up to receive the corresponding satellite signals and relay these to central data processing stations. The signals received at these data processing stations are evaluated taking into account the exact known position of the receiving stations. In this way, correction data can be determined that is ultimately broadcast to users via geo-stationary communications satellites. With the help of these corrections positional accuracy of around 7 m can initially be achieved. In addition, a level of data integrity is attained that enables instrument approaches to be made in aviation.
























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