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  • Articles  (90,347)
  • Springer  (65,798)
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  • Architecture, Civil Engineering, Surveying  (90,347)
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  • 1
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    GPS solutions 1 (1995), S. 3-4 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
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  • 2
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    GPS solutions 1 (1995), S. 1-2 
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  • 3
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    GPS solutions 1 (1995), S. 11-12 
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  • 4
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    GPS solutions 1 (1995), S. 7-8 
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  • 5
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    GPS solutions 1 (1995), S. 5-6 
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  • 6
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    GPS solutions 1 (1995), S. 9-10 
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  • 7
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    GPS solutions 1 (1995), S. 81-81 
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  • 8
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    GPS solutions 1 (1995), S. 86-87 
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  • 9
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    GPS solutions 1 (1995), S. 90-90 
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  • 10
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    GPS solutions 1 (1995), S. 91-93 
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  • 11
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    GPS solutions 1 (1995), S. 94-95 
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  • 12
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    GPS solutions 1 (1995), S. 88-89 
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  • 13
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    GPS solutions 1 (1995), S. 108-112 
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  • 14
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    GPS solutions 1 (1995), S. 99-107 
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  • 15
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    GPS solutions 1 (1995), S. 96-98 
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  • 16
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    GPS solutions 1 (1995), S. 129-138 
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  • 17
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    GPS solutions 1 (1995), S. 121-128 
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    Notes: In the previous article we covered what asset location systems (ALS) are and the features and benefits they offer. In this article we explore the various features to be considered when acquiring an ALS and steps to be taken. We discuss what users are saying they want in an ALS, including the results of a survey of vehicle tracking system users and providers.
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  • 18
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    GPS solutions 1 (1995), S. 139-142 
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  • 19
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    GPS solutions 1 (1995), S. 113-120 
    ISSN: 1521-1886
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    Notes: Abstract The vertical component obtained from the Global Positioning System (GPS) observations is from the ellipsoid (a mathematical surface), and therefore needs to be converted to the orthometric height, which is from the geoid (represented by the mean sea level). The common practice is to use existing bench marks (around the four corners of a project area and interpolate for the rest of the area), but in many areas bench marks may not be available, in which case an existing geoid undulation is used. Present available global geoid undulation values are not generally as detailed as needed, and in many areas they are not known better than ±1 to ±5 m, because of many limitations. This article explains the difficulties encountered in obtaining precise geoid undulation with some example computations, and proposes a technique of applying corrections to the best available global geoid undulations using detailed free-air gravity anomalies (within a 2° × 2° area) to get relative centimeter accuracy. Several test computations have been performed to decide the optimal block sizes and the effective spherical distances to compute the regional and the local effects of gravity anomalies on geoid undulations by using the Stokes integral. In one test computation a 2° × 2° area was subdivided into smaller surface elements. A difference of 37.34 ± 1.6 cm in geoid undulation was obtained over the same 2° × 2° area when 1° × 1° block sizes were replaced by a combination of 5' × 5' and 1' × 1' subdivision integration elements (block sizes).
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  • 20
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    GPS solutions 1 (1995), S. 143-144 
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  • 21
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    GPS solutions 1 (1995), S. 145-146 
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  • 22
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    GPS solutions 1 (1995), S. 148-149 
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  • 23
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    GPS solutions 1 (1995), S. 146-146 
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  • 24
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    GPS solutions 2 (1998), S. 1-12 
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  • 25
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    GPS solutions 2 (1998), S. 13-20 
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  • 26
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    GPS solutions 2 (1998), S. 21-26 
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  • 27
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    GPS solutions 2 (1998), S. 27-35 
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  • 28
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    GPS solutions 2 (1998), S. 36-41 
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  • 29
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    GPS solutions 2 (1998), S. 42-48 
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  • 30
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    GPS solutions 3 (2000), S. 44-48 
    ISSN: 1521-1886
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    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: The global positioning system (GPS) is used increasingly to control horizontal and vertical displacement of large civil constructions. The displacements can occur over varius time scales. For example, in case of the loading test of a bridge, the time span between measurements is on the order of 30 min. The achievable precision in the vertical component and its relation to residual multiplath effects become critically important in such aaplications. A multipath-to-noise ratio (MNR) on individual satellites is introduced to quantify the multipath effects. © 2000 John Wiley & Sons, Inc.
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  • 31
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    GPS solutions 3 (2000), S. 65-68 
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  • 32
    ISSN: 1521-1886
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    Notes: In this article, initial results are presented of a method to improve fast carrier phase ambiguity resolution over longer baselines (with lengths up to about 200 km). The ionospheric delays in the global positioning system (GPS) data of these long baselines mainly hamper successful integer ambiguity resolution, a prerequisite to obtain precise positions within very short observation time spans. A way to correct the data for significant ionospheric effects is to have a GPS user operate within an active or permanently operating network use ionospheric estimates from this network. A simple way to do so is to interpolate these ionospheric estimates based on the expected spatial behaviour of the ionospheric delays. In this article such a technique is demonstrated for the Dutch Active Control Network (AGRS.NL). One hour of data is used from 4 of the 5 reference stations to obtain very precise ionospheric corrections after fixing of the integer ambiguities within this network. This is no problem because of the relatively long observation time span and known positions of the stations of the AGRS.NL. Next these interpolated corrections are used to correct the GPS data from the fifth station for its ionospheric effects. Initial conclusions about the performance of this technique are drawn in terms of improvement of integer ambiguity resolution for this baseline. © 1999 John Wiley & Sons, Inc.
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  • 33
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    GPS solutions 3 (2000), S. 69-69 
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  • 34
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    GPS solutions 3 (2000), S. 58-64 
    ISSN: 1521-1886
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    Notes: Since global positioning system (GPS) measurements are ranges (code) and biased ranges (carrier), it seems natural to model them as ranges and determine the biases. This is particularly compelling since the double-difference range biases turn out to be integers. At some level there is also an elegance, perhaps therefore a naturalness, to modeling the carrier measurements as time differences of double differences. While something is lost something else is gained. Here we apply the proven delayed-state Kalman filter to processing carrier phase measurements as triple differences. In practice we process these triple differences along with double-difference code measurements. We also treat the measurement error as, mostly, Gauss-Markov states to be determined. Many of the details are discussed and experimental results are included. These demonstrate that excellent performance can be obtained if the Kalman filter modeling is done carefully. © 2000 John Wiley & Sons, Inc.
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  • 35
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    GPS solutions 3 (2000), S. 75-77 
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  • 36
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    GPS solutions 3 (2000), S. 1-9 
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    Notes: A third civil frequency at 1176.45 MHz will be added to the Global Positioning System (GPS). This new frequency will bring a number of benefits. The aviation user will be one of the prime beneficiaries because the new frequency is in a protected aviation band. Thus, the system will be more robust against interference and jamming. The carrier-phase differential user will also be a prime beneficiary as long as his application has a reasonably short baseline. It is this high accuracy use that is explored in some depth. The process of forming linear combinations of both the code and carrier-phase measurements is studied, and the benefits and problems are explained. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 70-74 
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    Notes: The ionospheric range delay is highly variable both in space and in time. The ionospheric correlation distance is defined as the distance over which a measurement of the difference from monthly mean ionospheric range delay at one location can be used to determine the difference from mean conditions at a second location. The percentage improvement required is dependent upon the actual correlation coefficient, which must be relatively large to produce a significant improvement over differences from average conditions at two stations. Results of studies of the correlation distance show that, in order to obtain even a 28% improvement over monthly median conditions, the measurement location must be within approximately 3,000 km in longitude or 1,800 km in latitude from the location where the update from monthly mean conditions is required, at least in the mid-latitude region. Another study showed that, in order to be able to determine an improvement of 1 m in ionospheric range delay from average ionospheric conditions at a location remote from where the actual measurement of range delay is made, the measurement must be within approximately 500 km of that location. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 24-34 
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    Notes: At the Delft University of Technology (DUT), the data of six stations participating in the first international GLONASS (Global Navigation Satellite System, the Russian counterpart of GPS) tracking campaign, IGEX-98, were analyzed with integrity monitoring software. The software was developed at the Department of Mathematical Geodesy and Positioning of DUT. The main function of this software is to detect slips and outliers in phase and code observations in real time. In addition, the software also allowe the validation of the information contained in the broadcast navigation messages. The results of the IGEX-98 data analyses will be presented in a three-part series. In this second part of the series, GLONASS outlier and slip statistics will be discussed in detail. The first part was concerned with the availability of GLONASS observations, while in the third one the broadcast navigation message validation results will be considered. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 35-38 
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    Notes: The forthcoming World Radiocommunication Conference (WRC) will deal with frequency allocation and protection issues that are of fundamental importance to GNSS (Global Navigation Satellite System) and GPS (Global Positioning System), which is a component of GNSS. In many countries, GPS L1 and L2 are not protected, and much needs to be done to obtain a frequency allocation for GPS L5. A brief explanation of the International Telecommunication Union (ITU) and how it can impact satellite navigation at its World Radiocommunication Conference in 2000 (WRC-2000) is provided. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 39-47 
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    Notes: Positioning and navigation – as are presently possible with the American Global Positioning System (GPS) and the Russian GLONASS system – is briefly reviewed. Deficiencies, which have led to augmentations like the European Geostationary Navigation Overlay System (EGNOS), are outlined. Europe's decision to get involved in the definition and possible set-up of a Global Navigation Satellite System (GNSS) of the second generation (GNSS-2), called Galileo, is discussed in detail as well as the GPS modernization program that might take place during the sample phase. Finally, some brief thoughts on the benefit of GNSS-2 for geodesy and surveying are given. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 10-23 
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    Notes: The International GLONASS Experiment 1998 (IGEX-98) was the first international tracking campaign of the Russian counterpart to the Global Positioning System (GPS), GLONASS. Started in October 1998, the campaign was originally scheduled to last for three months. However, the launch of additional GLONASS satellites and a widespread enthusiasm among the participants led to an indefinite continuation of the campaign on a “best effort” basis. At the Delft University of Technology, the data of six IGEX-98 stations have been analyzed in detail with integrity monitoring software, developed at the Department of Mathematical Geodesy and Positioning of the University. The software aims to detect outliers and slips in code and phase observations in real time. In addition, the software also allows the validation of the information contained in the broadcast navigation messages. The results of the IGEX-98 data analyses will be presented in a three-part series. In the second part, GLONASS outlier and slips statistics will be discussed, while in the third part the anomaly detection results of the GLONASS and GPS messages will be shown. In this first part of the series, however, the most basic of all statistics will be considered: a simple day-to-day count of the number of GLONASS and GPS observations. Although simple, this statistic yields a surprising amount of information both on the availability of the GLONASS satellites and on the peculiarities of some of the receiver makes participating in the IGEX-98 campaign. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 48-57 
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    Notes: The Federal Aviation Administration (FAA) is developing the wide-area augmentation system (WAAS) to supplement the Global Positioning System (GPS) and serve as a single en-route navigation aid. The program traveled a rocky road so far. We compare the original concept of WAAS with its current scaled down version, analyze the changed perspectives with respect to the utility of GPS for air navigation and the concomitant role of WAAS, and explore the future of GPS/WAAS. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 70-70 
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    GPS solutions 3 (2000), S. 58-64 
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    Notes: There are various applications in which a Global Positioning System (GPS) sensor only down-converts and digitizes the received GPS signal and sends the digitized data to a processor, where the processor software performs all the correlation, search/track operations, navigation solution, and so on. Among the applications are military and commercial ones (e. g., GPS(Communication handheld sets, people tracking systems). A major problem with the Software GPS Receiver is the large computing resources required for correlation or acquisition of the GPS signal. In this article, several possible approaches for reducing computing resources will be introduced and analyzed. It will be shown that the performance of the GPS software design strongly depends on the features of the computer hardware. Implementations will be described on the TMS320C6201 processor and the Pentium II. Experimental results will be demonstrated by processing of real GPS signals. A complete 16-channel GPS receiver was implemented on the single TMS320C6201 processor in real-time mode and on the Pentium II processor with a duty cycle of about 50%. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 65-69 
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    Notes: The law affects the Global Positioning System (GPS) industry both on a macro and on a micro level. On a macro level, issues such as future regulation of telematics, frequency spectrum allocation, and international agreements will shape the future of the industry. On a micro level, GPS companies can benefit from knowledge of legal pitfalls common in the high technology arena. Many thanks to Ingrid Lagarrigue, a French aviation and space lawyer specializing in Global Navigation Satellite legal issues, for her assistance and comments. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 3 (2000), S. 71-74 
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  • 47
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    GPS solutions 3 (2000), S. 80-82 
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  • 48
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    GPS solutions 4 (2000), S. 1-1 
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  • 49
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    Notes: A number of statistic Global Positioning System (GPS) measurement campaigns have been made on a floating Antarctic ice shelf, the Amery Ice Shelf, as part of ongoing glaciological studies designed to investigate the ice shelf dynamics, grounding zone definition, and ice shelf strain. Such studies ar fundamental to improving out knowledge of the Antarctic ice-sheet mass balance and dynamical models of ice sheet/ocean interaction. This article describes two techniques used to process the statistic GPS data. One approach uses a segmented version of the classical static methodology, and the other approach adopts a new sequential processing technique. Both approaches yield similar results for the station coordinates and demonstrate the potential of GPS for extracting the tidal signal on the ice shelves and giving information on the dynamical motion of the ice sheet. To verify our results for the vertical component, we compare the ice shelf GPS tidal signal with a tidal model derived from tide gauge measurements at nearby Beaver Lake. Comparison of the GPS results with the tide model give good agreement in amplitude at the few cm level (GPS results always larger) but clearly shows evidence of phase propagation of the ocean tidal wave under the ice shelf. Improving the resolution of the tides over the ice shelves will be of tremendous benefit for future satellite missions, such as Ice, Cloud and Land Elevation Satellite (ICESAT), and the integrated use of GPS and satellite data will be fundamental for any on-going Antarctic ice sheet mass balance studies. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 4 (2000), S. 13-20 
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    Notes: A new computer-aided design (CAD) program called Falcon 3.0 has been created to simulate and evaluate receiver designs. This CAD tool aims to solve tasks at the design stage of navigation receivers that operate with signals from Navigational Satellite Time and Ranging (NAVSTAR) and Global Navigational Satellite System (GLONASS). Specific tasks include: · Defining the receiver frequency plan (frequencies of oscillators and filters that guarantee accuracy of the receiver) · Specifying parameters for the digital processing of received signal · Computing interpath and interchannel biases · Computing statistical characteristics of correlation signals I, Q, dl, and dQ · Calculating noise and multipath errors of measurements · Determeining energy losses This CAD tool has been used in the design of receivers such as Javad Positioning Systems (JPS) Legacy, Regency, Odyssey, and Eurocard and in the prediction of their accuracy. It has been shown that experimental and predicted data agree well. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 4 (2000), S. 21-33 
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    Notes: The recent development of low-cost, high-precision oscillators has allowed many applications in various fields to become financially feasible. The stability of an oscillator is ultimatively what determines its usefulness for a certain application, and is therefore desirable to quantify. Current methods of evaluating stability require a direct comparison of the oscillator under test (OUT) with amore stable reference oscillator, the cost of which often offsets the initial benefit of a low-cost device. However, a relatively inexpensive Global Positioning System (GPS) receiver is capable of exploiting the highly stable GPS time scale, thus obviating the need for an expensive reference oscillator. By allowing the OUT to drive a GPS receiver, and processing the data with precise GPS orbits and clock corrections to eliminate the effects of selective availability (SA), the time series of computed clock offsets provides a measure of the oscillator's stability relative to GPS time. The use of GPS for assessing clock stability in the time domain is evaluated herein via the computation of Allan variance values. Performance of one rubidium and three ovenized crystal oscillator are investigated. Results show the method is limited to time intervals less than about two seconds or longer than about 300 seconds, where the effects of measurement noise and residual SA is less pronounced. © 2000 John Wiley & Sons, Inc.
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    Notes: Patricia Doherty joins the regular contributors of this column to discuss the correlation between measurements of solar 10.7 cm radio flux and ionospheric range delay effects on GPS. Mrs. Doherty has extensive experience in the analysis of ionospheric range delays from worldwide systems and in the utilization and development of analytical and theoretical models of the Earth's ionosphere. Ionospheric range delay effects on GPS and other satellite ranging systems are directly proportional to the Total Electron Content (TEC) encountered along slant paths from a satellite to a ground location. TEC is a highly variable and complex parameer that is a function of geographic location, local time, season, geomagnetic activity, and solar activity. When insufficiently accounted for, ionospheric TEC can seriously limit the performance of satellite ranging applications. Since the ionosphere is a dispersive medium, dual-frequency Global Positoning System (GPS) users can make automatic corrections for ionospheric range delay by computing the apparent difference in the time delays between the two signals. Single-frequency GPS users must depend on alternate methods to account for the ionospheric range delay. Various models of the ionosphere have been used to provide estimates of ionospheric range delay. These models range from the GPS system's simple eight-coefficient algorithm designed to correct for approximately 50% rms of the TEC, to state-of-the-art models derived from physical first principles, which can correct for up to 70 to 80% rms of the TEC but at a much greater computational cost. In an effort to improve corrections for the day-to-day variability of the ionosphere, some attempts have been made to predict the TEC by using the daily values of solar 10.7 cm radio flux (F10,7). The purpose of this article is to show that this type of prediction is not useful due to irregular, and sometimes very poor, correlation between daily values of TEC and F10.7. Long-term measurements of solar radio flux, however, have been shown to be well correlated with monthly mean TEC, as well as with the critical frequency of the inonospheric F2 region (foF2), which is proportional to the electron density at the peak of the ionospheric F2 region. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 4 (2000), S. 14-18 
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    Notes: Neural networks have been proposed as nonlinear filters in a variety of applications that involve nonlinear processing of input signals; examples include blind signal separation, image registration, and blind deconvolution. The Global Positioning System (GPS) navigation equations are nonlinear (quadratic) in nature, and a direct closed form solution of the GPS navigation equations does not exist. This article presents a new approach to solving the GPS pseudorange equations using three-layer neural networks. A three-layer radial basis function (RBF) neural network is designed, which solves the non-linear GPS pseudorange equations directly as opposed to the linear least squares or extended Kalman filter approaches in traditional GPS receivers. For training the neural network, a carefully selected cost function is minimized using a variation of the classical conjugate gradient algorithm such that training time for the neural network is reasonable. Simulations have been performed at SiRF Technology Inc. that show stable behavior even under bad geometry conditions where the traditional recursive least squares and extended Kalman filter approaches show high sensitivity to measurement errors. Under good geometry conditions the neural network solution shows slightly improved noise performance compared to the expected performance of traditional leas squares solution. Simulations have been performed with additive white Gaussian noise and correlated noise models to evaluate the performance of the trained neural network. © 2000 John Wiley & Sons, Inc.
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    Notes: In order to achieve to GPS solutions of first-order accuracy and integrity, carrier phase observations as well as pseudorange observations have to be adjusted with respect to a linear/linearized model. Here the problem of mixed integer-real valued parameter adjustment (IRA) is met. Indeed, integer cycle ambiguity unknowns have to be estimated and tested. At first we review the three concepts to deal with IRA: (i) DDD or triple difference observations are produced by a properly chosen difference operator and choice of basis, namely being free of integer-valued unknowns (ii) The real-valued unknown parameters are eliminated by a Gauss elimination step while the remaining integer-valued unknown parameters (initial cycle ambiguities) are determined by Quadratic Programming and (iii) a RA substitute model is firstly implemented (real-valued estimates of initial cycle ambiguities) and secondly a minimum distance map is designed which operates on the real-valued approximation of integers with respect to the integer data in a lattice. This is the place where the integer Gram-Schmidt orthogonalization by means of the LLL algorithm (modified LLL algorithm) is applied being illustrated by four examples. In particular, we prove that in general it is impossible to transform an oblique base of a lattice to an orthogonal base by Gram-Schmidt orthogonalization where its matrix enties are integer. The volume preserving Gram-Schmidt orthogonalization operator constraint to integer entries produces “almost orthogonal” bases which, in turn, can be used to produce the integer-valued unknown parameters (initial cycle ambiguities) from the LLL algorithm (modified LLL algorithm). Systematic errors generated by “almost orthogonal” lattice bases are quantified by A. K. Lenstra et al. (1982) as well as M. Pohst (1987). The solution point ${\hat z}$ of Integer Least Squares generated by the LLL algorithm is ${\hat z}$ = (L')−1[L'◯] ∈ ℤ m where L is the lower triangular Gram-Schmidt matrix rounded to nearest integers, [L], and ${\hat z}$ = [L'◯] are the nearest integers of L'◯, ◯ being the real valued approximation of z ∈ ℤ m , the m-dimensional lattice space Λ. Indeed due to “almost orthogonality” of the integer Gram-Schmidt procedure, the solution point ${\hat z}$ is only suboptimal, only close to “least squares.” © 2000 John Wiley & Sons, Inc.
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    GPS solutions 4 (2000), S. 45-53 
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    Notes: At the Delft University of Technology (DUT), data of six stations participating in the first international GLONASS tracking campaign, IGEX-98, were analyzed with integrity monitoring software. The software was developed at the Department of Mathematical Geodesy and Positioning of DUT. The main function of the software is to detect slips and outliers in phase and code observations in real time. In addition, the software also allows the validation of the information contained in the broadcast navigation messages. The results of the IGEX-98 data analyses are presented in a three part series. In this third and final part of the series, GLONASS and GPS navigation message validation results will be discussed in detail. The first part was concerned with the availability of GLONASS observations (Jonkman & de Jong, 2000a), while in the second part, GLONASS slip and outlier statistics were considered (Jonkman & de Jong, 2000b). The discussion of the navigation message validation results concentrates on anomalies detected in the data of an IGEX-98 station in Switzerland. Data collected at this station from September 1998 to December 1999 was analyized. In all, 19 anomalies were detected by the integrity monitoring software, 8 in GLONASS messages and 11 in GPS messages. The cause of the anomalies was established by evaluating the original data files, studying official bulletins of the GLONASS and GPS ground segments, and in some cases tracing the anomaly through the complete IGEX-98 network. © 2000 John Wiley & Sons, Inc.
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    GPS solutions 1 (1995), S. 23-27 
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    Notes: This is the first in a series of three articles authored by John Beukers. In this series, John will lead us through some of today's relevant radionavigation history putting turbulent times into perspective. Picking out what he considers significant in the current debate, he projects the future for satellite and terrestrial radionavigation systems well into the 21st century.
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    GPS solutions 1 (1995), S. 48-53 
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    GPS solutions 1 (1995), S. 38-47 
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    GPS solutions 1 (1995), S. 54-58 
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    GPS solutions 1 (1995), S. 59-64 
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    GPS solutions 1 (1995), S. 13-22 
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    Notes: Asset location systems, including vehicle and property tracking systems, are in the verge of exploding onto the scene for widespread business and personal use. This is due in part to decreased costs of GPS equipment, and greater availability of wireless communication systems, but also largely due to public awareness of their capabilities and benefits. Companies, organizations, and individual consumers that earlier could not justify the costs of tracking systems are now seriously considering their implementation. Public awareness of such systems is growing daily. Newspapers regularly have articles covering the latest applications of GPS. En route nagivation for aircraft, assisting blind people to navigate the streets of a city, and tracking skiers on slopes are some of the topics of recent newspapers articles on GPS. This article explores GPS asset location systems, looks at their features and foibles, and considers their cost, utility, ease of use, and drawbacks.
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    GPS solutions 1 (1995), S. 28-37 
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    Notes: Executive Summary GPS is a scientific method used as an adjunct to geographic information systems (GIS) for determining high-accuracy control points over large areas. Recent improvements in receiver technology, differential surveying, and software have made use of GPS technology more practical for smaller GIS projects. This article compares three different GPSs with occupation times of 2 and 12 min using an existing control network, comparing the location of the points and the distances between points. The control network internal distances vary from 40 to 280 m, and within 2000 m of the nearest second-order National Geodetic Survey (NGS) triangulation station. The partnership of GPS and GIS will lead to higher surveying integrity while improving digital mapping on the ground over small and large areas. It also allows for postsurvey analysis with solutions coming from multiple base stations. Presented here is a case study of how to achieve highly accurate and effective control points using using GPS/GIS, particularly for a small area.
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    GPS solutions 1 (1995), S. 65-73 
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    Notes: The NAVSTAR Global Positioning System is a space-based, all-weather, worldwide satellite navigation system. GPS uses the constellation of satellites and associated ground equipment to perform the primary missions of highly accurate navigation, time transfer, and nuclear detonation detection. To achieve these missions, GPS has three clearly defined segments – space, user and control (see Figure 1). The control segment, otherwise referred to as the operational control segment (OCS), consists of the personnel and equipment that controls the space segment and interfaces with the user segment. The OCS is made up of the master control station (MCS), the ground antennas (GA), and the monitor stations (MS). The purpose of this article is to describe how the 2nd Space Operations Squadron runs the MCS, the key element of the OCS.
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    GPS solutions 1 (1995), S. 74-75 
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    GPS solutions 1 (1995), S. 76-79 
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    GPS solutions 1 (1995), S. 80-80 
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    GPS solutions 1 (1995), S. 85-85 
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    GPS solutions 2 (1998), S. 62-65 
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    GPS solutions 2 (1998), S. 66-66 
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    GPS solutions 2 (1998), S. 67-68 
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    GPS solutions 2 (1998), S. 1-2 
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    GPS solutions 2 (1998), S. 16-27 
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    Notes: The potential 48-satellite constellation offered by the combination of observations from both the GPS and GLONASS positioning systems has created considerable interest among existing GPS users. In the published literature, a considerable amount of work has been devoted to the theoretical issue of algorithm design for combined GPS/GLONASS positioning solutions. Little work has been published, however, on the practical conversion of existing GPS software to include GLONASS observations. This paper considers the computation issues pertaining to the GLONASS broadcast ephemeris for inclusion of GLONASS observations into existing GPS software. The format of the GLONASS broadcast ephemeris is discussed and theory of satellite orbits and their stepwise numerical integration is reviewed. Finally, a strategy for GLONASS broadcast ephemeris computation is proposed to facilitate combination of GPS and GLONASS observations. © 1998 John Wiley & Sons, Inc.
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    Notes: The International Association of Geodesy officially established the International GPS Service (IGS) on Janaury 1, 1994. Its prime objective is to provide support and a rerefence system for a wide variety of scientific and practical applications involving GPS. To fulfill its role the IGS also generates, in addition to its fundamental products (orbital/staion positions and consistent Earth orientation parameters), additional reference-system products providing the necessary infrastructure, standards, and means of calibrations for timing and various atmospheric applications of GPS. The generation and efficient application of IGS products and their impact on a number of positioning and atmospheric applications, including low earth orbit satellites, is reviewed and discussed. @ 1998 John Wiley & Sons, Inc.
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    Notes: A proper choice of the observation weight matrix is of importance for both adjusting and testing GPS data. Our understanding of the noise characteristic of GPS observations, on which the weight matrix should be based, is, however, still underdeveloped. This makes it difficult to draw up an appropriate weight matrix. The first and foremost purpose of this contribution is therefore to draw attention to the need to improve upon our rudimentary knowledge of the GPS stochastic model. To this end, results will be presented of a relatively simple case study in which the possible presence of cross-correlation between observables is considered. With these results we hope to spur further discussion and research on this important topic. © 1998 John Wiley & Sons, Inc.
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    Notes: An effective method of decreasing multipath errors in GPS or GPS/GLONASS receivers by changing delay lock loop correlator reference signal is discussed. Unlike other approaches, this method does not lead to apparatus complication, power comsumption increase, or augmentation of digital processor load. This method eliminates the multipath error completely if the difference in delays of direct and reflected signal is more than 30 m, and decreases this error for smaller delays. The cost of such decrease is that the noise error is decreased. However, the noise error is much less dangerous than the multipath one because of its smaller value and much shorter correlation interval. Calculated and experimental data for the method are given for multipath and noise errors. © 1998 John Wiley & Sons, Inc.
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    GPS solutions 2 (1998), S. 67-67 
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    GPS solutions 2 (1998), S. 64-66 
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    GPS solutions 2 (1998), S. 68-68 
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    GPS solutions 2 (1998), S. 69-71 
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    GPS solutions 2 (1998), S. 72-72 
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    GPS solutions 2 (1999), S. 1-2 
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    GPS solutions 2 (1999), S. 24-36 
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    Notes: The purpose of this article is to report on an integrated system that uses GPS and other low cost sensors for azimuth and pitch determination. The ability of the integrated system to maintain a solution over periods of induced GPS outage is also demonstrated. © 1999 John Wiley & Sons, Inc.
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    GPS solutions 2 (1999), S. 18-23 
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    Notes: The Global Positioning System (GPS) satellita navigation aiding system, sometimes called NAVSTAR, has become a utility to the military and many civilian areas. GPS, currently consisting of 24 satellites, is used by the military for navigation, precision weapons delivery, and the future digital battlefield. In the civilian sector, GPS is widely used as the primary or secondary aid for land, water, and air navigation; as a surveying aid; as a vehicle location system; and as a precision time standard for cellular and ATM sites. In the aviation community, GPS is becoming an integral part of the WAAS (Wide Area Augmentation System) and the LAAS (Local Area Augmentation System) for en route navigation in North America and Category II and III precision approach, and for surface navigation. The vulnerability of GPS have become the vulnerabilities of WAAS and LAAS, and require consideration of interference mittigation techniques. © 1999 John Wiley & Sons, Inc.
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    GPS solutions 2 (1999), S. 37-40 
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    Notes: The growing importance and effectiveness of the Global Positioning System (GPS) in positioning geophysical surveys is now well established. In Ecuador's Amazon basin the use of GPS was the determining factor in the successful completion of a gravity survey carried out in 1994. Over 500 gravity stations, spaced from 1 to 5 km apart and positioned by GPS, were collected in the jungle environment in the country's southeast, where the preexisting data, of variable and unknown quality, were mostly confined to areas along the major rivers. This station densification, which includes the reoccupation of selected points, contributed to increase the gravity coverage; it also allowed us to evaluate and correct 1100 preexisting data points in the area, so that the different surveys can be merged. The composite data set is used for a geologic analysis of the study area, where previously unknown structures are discovered. © 1999 John Wiley & Sons, Inc.
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    GPS solutions 2 (1999), S. 41-49 
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    Notes: The permanent GPS tracking site at Annapolis, MD shows a 7-mm seasonal signal primarily in its horizontal position. It is suggested that thermal expansion of the pier on which the antenna rests is the source of this motion. A simple numerical model of the pier reproduces the observed motion of the GPS antenna, lending credence to this hypothesis. Although adding an additional level of complexity, this motion is predictable and the site retains it s value for high precision monitoring. Although the arrangement of this GPS site it somewhat uncommon, these results emphasize the importance of the underlying antenna monumentation when measuring crustal motions. © 1999 John Wiley & Sons, Inc.
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    GPS solutions 2 (1999), S. 63-69 
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    Notes: GPS ambiguity resolution is the process of resolving the unknown cycle ambiguities of double-difference (DD) carrier-phase data as integers. It is the key to fast and high-precision relative GPS positioning. Critical in the application of ambiguity resolution is its reliability. Unsuccessful ambiguity resolution, when passed unnoticed, will too often lead to unacceptable errors in the positioning results. High success rates are required for ambiguity resolution to be reliable. In this contribution we will introduce and evaluate such diagnostic measures. They complement existing methods of ambiguity resolution and allow the user and/or analyst to infer their reliability. © 1999 John Wiley & Sons, Inc.
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    GPS solutions 2 (1999), S. 50-62 
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    Notes: The largest error in currently used GPS orbit models is due to the effect of solar radiation pressure. Over the last few years many improvements were made in modeling the orbits of GPS satellites within the International GPS Service (IGS). Howeer, most improvements were achieved by increasing the number of estimated orbit and/or solar radiation pressure parameters. This increase in the number of estimated satellite parameters weakens the solutions of all estimated parameters (not only orbit parameters). Because of correlations the additional orbit parameters may introduce biases in other estimated quantities, for example the length of day. We present a recently developed solar radiation pressure model for the GPS satellites. This model is based on experiences and results gained at the Center for Orbit Determination in Europe (CODE) in the context of its IGS activities since June 1992. The performance of the new model is almost an order of magnitude better than that of the existing ROCK models. It also allows a reduction of the number of orbit parameters that have to be estimated. © 1999 John Wiley & Sons, Inc.
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  • 91
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: A solar-powered GPS receiver has been installed near Beaver Lake, Antarctica, to monitor postglacial isostatic rebound that may be occurring as a result of ice thinning near the Lambert Glacier since the last glacial maximum. The equipment is 400 km from the nearest Australian Antarctic base and is completely automated. It is expected that there will be sufficient solar power to operate the equipment from January 1998 to May 1998, but the data will not be recovered until the following summer season. The scatter in height computed from the first 25 days of data is ± 7.5 mm. If such precision is representative of the accuracy of the height estimates, isostatic rebound of 〈 1 mm/yr will be able to be detected after a few years of observations at the site. © 1999 John Wiley & Sons, Inc.
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  • 92
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    GPS solutions 2 (1999), S. 79-80 
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  • 93
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    GPS solutions 2 (1999), S. 81-83 
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  • 94
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    GPS solutions 2 (1999), S. 76-78 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: Automatic analysis of geodetic-quality GPS data is available with the use of e-mail and ftp (file transfer program) as an interface to a computer at the Jet Propulsion Laboratory (JPL), where precise transmitter parameters – GPS ephemerides and clock errors – are computed regularly. The interface is such that e-mail from an external user causes the JPL computer to fetch the user's data. The computer than analyzes the data, and places the results in an area accessible to the user. An e-mail to the user gives information on the location of the analysis results, which the user can subsequently fetch. Operations on the JPL computer are entirely automatic, and require essentially no labor. © 1999 John Wiley & Sons, Inc.
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  • 95
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    GPS solutions 2 (1999), S. 1-6 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: This article describes the Nationwide Differential Global Positioning System (NDGPS) service being developed in the United States and the enormous benefits to federal agencies, state governments, and the general public. © 1999 John Wiley & Sons, Inc.
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  • 96
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    GPS solutions 2 (1999), S. 35-43 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: The noise term of GPS phase data can be calculated from the measured carrier-to-noise power density ratios (C/N0). The C/N0 values are used in the proposed SIGMA-ɛ model to calculate the variance matrix of double-differenced GPS phase data. Examples show the capability of this model to yield higher accuracies for GPS surveys than the use of the standard weighting scheme. Most importantly, the SIGMA-ɛ model allows the use of noisier phase data from very low elevation satellites to overcome poor satellite geometry problems. © 1999 John Wiley & Sons, Inc.
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  • 97
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    GPS solutions 2 (1999), S. 44-51 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: Investigations of deformation styles in Asia have already led to new kinematic models that predict the spatial and temporal evolution of deformations in the region. Testing these models is now within realm of current GPS technology. In this study, GPS data during 4 months from six stations in Asia, including a new station from Hong Kong whose data were not in public domain, were analyzed for generating kinematic geophysical constraints for the deformations at the regional scale. Processing of 4 months' continuous GPS data from all stations shows small relative station velocities (Wuhan, Shanghai, Xian, and Hong Kong stations in China), except the Lhasa station, which has a northeasterly velocity of about 3 cm/year with respect to the fixed GPS station operating in Taiwan. © 1999 John Wiley & Sons, Inc.
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  • 98
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    GPS solutions 2 (1999), S. 7-21 
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: Accurate estimates of the velocity and acceleration of a platform are often needed in high dynamic positioning, airborne gravimetry, and geophysics. In turn, differentiation of GPS signals is a crucial process for obtaining these estimates. It is important in the measurement domain where, for example, the phase measurements are used along with their instantaneous derivative (Doppler) to estimate position and velocity. It is also important in postprocessing, where acceleration is usually estimated by differentiating estimates of position and velocity. Various methods of differentiating a signal can have very different effects on the resulting derivative, and their suitability varies from situation to situation. These comments set the stage for the investigations in this article. The objective is twofold: (1) to carry out a comprehensive study of possible differentiation methods, characterizing each in the frequency domain; and (2) to use real data to demonstrate each of these methods in both of the measurement and position domains, in conditions of variable, high, or unknown dynamics. Examples are given using real GPS data in both the measurement domain and in the position and velocity domain. The appropriate differentiator is used in several cases of varying dynamics to derive a Doppler signal from carrier phase measurements (rather than using the raw Doppler generated by the receiver). In the statistic case, it is seen that the accuracy of velocity estimates can be improved from 4.0 mm/s to 0.7 mm/s by using the correct filter. In conditions of medium dynamics experienced in an airborne gravity survey, it is demonstrated that accelerations as the 2–4 mGal level (1 mGal = 0.00001 m/s2) can be obtained at the required filtering periods. Finally, a precision motion table is used to show that when using the correct filter, velocity estimates under high dynamics can be improved by an order of magnitude to 27.0 mm/s. © 1999 John Wiley & Sons, Inc.
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  • 99
    ISSN: 1521-1886
    Source: Springer Online Journal Archives 1860-2000
    Topics: Architecture, Civil Engineering, Surveying , Geosciences
    Notes: LandStar is a differential global positioning service (DGPS) that provides 24-h real-time positioning for various applications on land, water, and air in North America, Australia, New Zealand, Europe, and Africa. Its focus is on real-time applications requiring a submeter positioning capability such as agriculture, forestry, Geospatial Information Systems (GIS), survey/mapping, and land/vehicular navigation. LandStar uses a Wide Area Network of reference stations to derive DGPS corrections to model the variation of GPS error sources over a large area. These model parameters are used by the Virtual Reference Station processors to calculate standard corrections that are available for all predefined locations in the network. The corrections are transmitted to the user by L-band satellite communication in the standard RTCM SC104 DGPS correction format. This article investigates the performance of the LandStar Mk III system under various operational conditions and assesses its performance in both static and kinematic modes. Four field tests were conducted during 12 months that tested the sysem in clear static and kinematic conditions as well as suboptimal environments associated with low and heavy foliage conditions. Both the accuracy and availability of the system under these conditions is investigated, with an emphasis on whether the above variables are caused by the LandStar system differential corrections, the GPS measurements, or a combination of both. © 1999 John Wiley & Sons, Inc.
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  • 100
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    GPS solutions 2 (1999), S. 57-59 
    ISSN: 1521-1886
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