Site hosted by Angelfire.com: Build your free website today!

welcome jestin + padakathu website

welcome to jestin & padakathu website

hosted by Angelfire
Search the web with Hotbot Try Blogging for FREE


 

WELCOME TO PADAKATHU  REMOTE SENSING GEOINFORMATICS WEBSITE

r.padakathu

M.Tech, Remote sensing and geoinformatics

Bharathidasan University

Trichy-620 023

 2.1.2 Introduction to GPS

SATELLITE-BASED POSITIONING SYSTEMS

 

 

Some characteristics of satellite-based positioning systems, past, operational and proposed, are:

TRANSIT Doppler (NNSS)

TSIKADA

NAVSTAR Global Positioning System

GLONASS

STARFIX

GEOSTAR/LOCSTAR

ARGOS

NAVSAT & other LEO systems


Back to Chapter 2 Contents / Next Topic / Previous Topic

TRANSIT Doppler System

 

The history of TRANSIT coincides with the start of the Space Age (4th October 1957). Sputnik I was launched and the Doppler shift of the signals were used to determine the satellite orbit. The method was inverted so that if the orbit were known, the position of the receiver could be determined (PARKINSON et al, 1995). Special features and milestones:



Figure 1. The TRANSIT Doppler satellite positioning system configuration.

 

ARGOS System

 

ARGOS is another satellite system which uses the Doppler principle for positioning. ARGOS is a cooperative project between the French Centre National d'Etudes (CNES), NASA, and the U.S. National Oceanic and Atmospheric Administration (NOAA), and was first deployed in 1978. Transmitters are operated by users on variety of "platforms" (buoys, animal tracking, radiosondes, etc.), and satellites act as receivers (one of two U.S. TIROS weather stations). CNES computes position and velocity of platform, sends information (and the bill!) to user. Other such "subscriber" systems in place include the COSPAS-SARSAT search & rescue system and GEOSTAR. The important distinction is that ARGOS is essentially a satellite-based tracking system, while many of the other systems (including GPS) are self-navigating systems.

The GLONASS System

 

Russian equivalent to the GPS system, having the following characteristics (KLEUSBERG, 1990; IVANOV & SALISTCHEV, 1991; PARKINSON et al, 1995):

64.8 inclination, 19,100km altitude (11hr 15min period).

 

2.1.1 Introduction to GPS

WHAT IS GPS?

 

The NAVSTAR Global Positioning System (GPS) is a satellite-based positioning system, which by virtue of its special characteristics, is revolutionising the tasks of navigation and surveying:

Relatively high positioning accuracies, from the dekametre to the millimetre level.

Determination of velocity and time to an accuracy commensurate with position.

Available to users anywhere on the globe: in the air, on the ground, or at sea.

Relatively low cost system, with no user charges.

All-weather system, available 24 hours a day.

The position information is in three dimensions, that is, vertical as well as horizontal information is provided.

 

Who Developed GPS?

 

The Global Positioning System is, in the first instance, a military navigation system designed, financed, deployed and controlled by the U.S. Department of Defense.


Development work on GPS commenced in 1973 as a result of the merger of several R&D programs within the U.S. Department of Defense, namely the Navy's "TIMATION" project, and the Air Force's "621B" project. The first satellite was launched in 1978. (For a background to the development of the GPS program the reader is referred to PARKINSON, 1994, and PARKINSON et al, 1995.) The development and production program for the GPS is managed by the U.S. Air Force (USAF) Systems Command, Space Systems Division, Joint Program Office (JPO) at the Los Angeles Air Force Base, California. The JPO is manned by personnel from the USAF, U.S. Navy, U.S. Army, U.S. Marine Corps, U.S. Coast Guard, U.S. Defense Mapping Agency, NATO nations and Australia.

The aim of the JPO was to develop an all-weather, 24-hour, truly global navigation system to support the positioning requirements for the armed forces of the U.S. and its allies. As such a system was designed to replace the large variety of navigational systems already in use, a great import was placed on the system's utility, reliability and survivability. A number of stringent conditions therefore had to be met. In addition to those listed above, they included:

 

This led to a design concept based on:

 

 

 The total investment by the U.S. military in the GPS system to date is well over $10 BILLION (US)!

However, although the primary goal of GPS is to provide land, air and marine positioning capabilities to the U.S. armed forces and its allies, GPS is freely available to all users. The number of civilian users is already far greater than the military users, and the applications of the positioning technology are growing rapidly. The civilian sector therefore represents an important user group that is increasingly lobbying in order to influence official GPS policy. The U.S. military however still operates several "levers" with which they control the performance of GPS. On the other hand, there is tremendous innovation occurring within the civilian sector, with the development of technology and procedures that are increasing making redundant many of the U.S. military procedures intended to restrict GPS performance.

 

Why a Satellite Positioning System?

 

Satellite Positioning Systems are global. The signals can be "seen" over a large area, and are not interfered with by terrain or geography to the same extent as conventional ground-based positioning systems.

 

GPS was designed to replace the TRANSIT Doppler satellite navigation system which has given good service to the navigation and geodetic community for over 20 years. The advantages of TRANSIT are essentially those of GPS as well. A microwave satellite-based system:

 

However, in addition, the NAVSTAR Global Positioning System has some further advantages over other satellite-based positioning systems:

It is a one-way (listen only) system, in which the satellites transmit signals, but are unaware who is using the signal (no receiving function). The user (or listener) does not transmit a signal, and therefore:

As GPS is a multi-satellite system, there is always a number of satellites visible simultaneously anywhere on the globe, and at any time.

GPS can support a number of positioning and measurement modes in order to satisfy simultaneously a variety of users, from those only requiring navigation (dekametre) accuracies to those demanding very high (millimetre - centimetre) accuracies.

Back to Chapter 2 Contents / Next Topic

 

2.1.2 Introduction to GPS

SATELLITE-BASED POSITIONING SYSTEMS

 

 

Some characteristics of satellite-based positioning systems, past, operational and proposed, are:

TRANSIT Doppler (NNSS)

TSIKADA

NAVSTAR Global Positioning System

GLONASS

STARFIX

GEOSTAR/LOCSTAR

ARGOS

NAVSAT & other LEO systems


Back to Chapter 2 Contents / Next Topic / Previous Topic

TRANSIT Doppler System

 

The history of TRANSIT coincides with the start of the Space Age (4th October 1957). Sputnik I was launched and the Doppler shift of the signals were used to determine the satellite orbit. The method was inverted so that if the orbit were known, the position of the receiver could be determined (PARKINSON et al, 1995). Special features and milestones:



Figure 1. The TRANSIT Doppler satellite positioning system configuration.

 

ARGOS System

 

ARGOS is another satellite system which uses the Doppler principle for positioning. ARGOS is a cooperative project between the French Centre National d'Etudes (CNES), NASA, and the U.S. National Oceanic and Atmospheric Administration (NOAA), and was first deployed in 1978. Transmitters are operated by users on variety of "platforms" (buoys, animal tracking, radiosondes, etc.), and satellites act as receivers (one of two U.S. TIROS weather stations). CNES computes position and velocity of platform, sends information (and the bill!) to user. Other such "subscriber" systems in place include the COSPAS-SARSAT search & rescue system and GEOSTAR. The important distinction is that ARGOS is essentially a satellite-based tracking system, while many of the other systems (including GPS) are self-navigating systems.

The GLONASS System

 

Russian equivalent to the GPS system, having the following characteristics (KLEUSBERG, 1990; IVANOV & SALISTCHEV, 1991; PARKINSON et al, 1995):

 



Figure 2. The GLONASS satellite configuration.

 

Table Comparing GPS and GLONASS ( IVANON & SALISTCHEV, 1991 )

Parameter

GLONASS

GPS

Ephemeris information presentation method

9 parameters of s/c motion in the gecentric rectangular rotated coordinate system

Interpolation coefficients of satelite orbits

Geodesic coordinate system

SGS 85

WGS 84

Referencing of the ranging signal phases

To the timer of GLONASS system

To the timer of GPS system

System time corrections relative to the universal coordinates time ( UTC )

UTC ( SU )

UTC ( USNO )

Duration of the almanac transmission

2.5 min

12.5 min

Number of satelites in the full operational system

21 + 3 apares

21 + 3 spares

Number of orbital planes

3

6

Inclination

64.8

55

Orbit altitude

19.100 km

20.180 km

Orbital period

11 h 15 min

12 h

Satelite signal division method

Frequency division

Code division

frequency band allocated

1602.5625-1615.5
0.5 MHz

1575.42 1 MHz

Type of ranging code

PRN-sequence of maximal length

Gold code

Number of code elements

511

1023

Timing frequency of code

0.511 MHz

1.023 MHz

Crosstalk level between two neighboring channels

- 48 dB

- 21.6 dB

Synchrocode repetition period

2 sec

6 sec

Symbol number in the synchrocode

30

8

 

Back to Chapter 2 Contents / Next Topic / Previous Topic

© Chris Rizos, SNAP-UNSW, 1999

 

© Chris Rizos, SNAP-UNSW, 1999

 



Figure 2. The GLONASS satellite configuration.

 

Table Comparing GPS and GLONASS ( IVANON & SALISTCHEV, 1991 )

Parameter

GLONASS

GPS

Ephemeris information presentation method

9 parameters of s/c motion in the gecentric rectangular rotated coordinate system

Interpolation coefficients of satelite orbits

Geodesic coordinate system

SGS 85

WGS 84

Referencing of the ranging signal phases

To the timer of GLONASS system

To the timer of GPS system

System time corrections relative to the universal coordinates time ( UTC )

UTC ( SU )

UTC ( USNO )

Duration of the almanac transmission

2.5 min

12.5 min

Number of satelites in the full operational system

21 + 3 apares

21 + 3 spares

Number of orbital planes

3

6

Inclination

64.8

55

Orbit altitude

19.100 km

20.180 km

Orbital period

11 h 15 min

12 h

Satelite signal division method

Frequency division

Code division

frequency band allocated

1602.5625-1615.5
0.5 MHz

1575.42 1 MHz

Type of ranging code

PRN-sequence of maximal length

Gold code

Number of code elements

511

1023

Timing frequency of code

0.511 MHz

1.023 MHz

Crosstalk level between two neighboring channels

- 48 dB

- 21.6 dB

Synchrocode repetition period

2 sec

6 sec

Symbol number in the synchrocode

30

8

 

Back to Chapter 2 Contents / Next Topic / Previous Topic

© Chris Rizos, SNAP-UNSW, 1999

 

2.3.2 Applications of GPS

GPS SATELLITE SURVEYING

 


Adopting the broadest definition of "GPS surveying", the following classes of surveys can be identified:

 

What are the criteria for deciding if an application belongs to "surveying", "navigation", or "other"? This is not as easy as it may first appear. In general (and there are exceptions), a "surveying" application is a positioning task that:

 

In the case of land surveying applications, the characteristics of GPS satellite surveying are less contentious:

 

Land Surveying Applications for GPS


A convenient approach is to adopt an applications classification on the basis of accuracy requirements. Three classes of applications can be identified on this basis, for which a range of relative accuracies (it is assumed that single receiver point positioning is not accurate enough to satisfy these applications) ranging from low-to-moderate, 1 part in 104, through to the ultra-high 1 part in 107 or better accuracies:

Category A (Scientific)

: better than 1 ppm

Category B (Geodetic)

: 1 to 10 ppm

Category C (General Surveying)

: lower than 10 ppm.

Category A surveys primarily encompass those surveys undertaken for precise engineering, deformation analysis, and geodynamic applications. Category B surveys include geodetic surveys undertaken for the establishment, densification and maintenance of control networks to support mapping. Category C surveys primarily encompass lower accuracy surveys, primarily undertaken for urban, cadastral, geophysical prospecting, GIS and other general purpose mapping applications. Users in the latter two categories form the majority of the GPS user community, while category A users often provide the primary "technology-pull" for the development of new instrumentation and processing strategies, which may ultimately be adopted by the category B and C users.

Note that this classification scheme is entirely arbitrary, and does not reflect any "order" of survey as defined by Survey Authorities. It does, however, provide a convenient breakdown of GPS survey "type", enabling the similarities and differences between the categories to be highlighted. Below are listed the advantages and disadvantages of the GPS technology (in the context of land survey applications) in broad-brush terms only.

Advantages of GPS Over Conventional Surveying Methods


There are several advantages of the GPS satellite surveying technique:

Disadvantages of GPS Surveying


It would be remiss not to also mention the disadvantages, some of which will no doubt be overcome in time, others with some additional effort, while others cannot be dismissed so easily:

 

Further Remarks


The prospect for increased acceptance of GPS satellite surveying is very good, particularly as the cost of GPS systems drops and new higher productivity techniques are developed. Although GPS was initially used for high-order geodesy and geodetic control surveys on the one hand, and geophysical exploration surveys on the other, adoption of the GPS technology for applications such as lower-order control densification, and even cadastral, engineering and detail surveys, has already commenced.

However, for all its technical advantages, there remain a number of significant differences between the results of the GPS surveying technology and that of conventional terrestrial techniques. To reconcile these differences, and in order to ensure that GPS will complement these other technologies (and hence maintain compatibility with the geodetic framework established in many countries over a long period of time), a significant amount of post-processing of GPS results is necessary. This tends to make the GPS technology less attractive, and has the effect of raising the threshold of acceptance slightly higher than it would otherwise have been.

In addition there is an investment in human resource development that must be taken into account. GPS manufacturers are striving to make equipment that is ever more "user-friendly", which will mean that many other professionals apart from "qualified professional surveyors" will be able to carry out high accuracy GPS surveys. The challenge, however, to surveyors is to maintain the "edge", by seeking to use their best judgement and skills not only to achieve high GPS accuracy, but also to ensure that the quality and reliability of the results are at the level demanded by the client. A further advantage that surveyors enjoy over other professionals is that they often are the only ones skilled in integrating GPS results into previously coordinated networks.

 

Back To Chapter 2 Contents / Next Topic / Previous Topic

© Chris Rizos, SNAP-UNSW, 1999