509 research outputs found

    Analysis Coordinator Report

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    We present the IVS analysis coordination issues of 2012. The IVS Analysis Coordinator is responsible for generating and disseminating the official IVS products. This requires consistency of the input data by strict adherence to models and conventions. The term of the current IVS Analysis Coordinator will end on February 28, 2013

    The Advent of Transport Authorities in South Africa

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    Institute of Transport and Logistics Studies. Faculty of Economics and Business. The University of Sydne

    The Financing of Land Transport in South Africa

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    Institute of Transport and Logistics Studies. Faculty of Economics and Business. The University of Sydne

    The impact of celestial pole offset modelling on VLBI UT1 Intensive results

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    Very Long Baseline Interferometry (VLBI) Intensive sessions are scheduled to provide operational Universal Time (UT1) determinations with low latency. UT1 estimates obtained from these observations heavily depend on the model of the celestial pole motion used during data processing. However, even the most accurate precession-nutation model, IAU 2000/2006, is not accurate enough to realize the full potential of VLBI observations. To achieve the highest possible accuracy in UT1 estimates, a celestial pole offset (CPO), which is the difference between the actual and modelled precession-nutation angles, should be applied. Three CPO models are currently available for users. In this paper, these models have been tested and the differences between UT1 estimates obtained with those models are investigated. It has been shown that neglecting CPO modelling during VLBI UT1 Intensive processing causes systematic errors in UT1 series of up to 20 microarcseconds. It has been also found that using different CPO models causes the differences in UT1 estimates reaching 10 microarcseconds. Obtained results are applicable to the satellite data processing as well.Comment: 8 pp., accepted for publication in Journal of Geodes

    Combinatorial optimization applied to VLBI scheduling

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    Due to the advent of powerful solvers, today linear programming has seen many applications in production and routing. In this publication, we present mixed-integer linear programming as applied to scheduling geodetic very-long-baseline interferometry (VLBI) observations. The approach uses combinatorial optimization and formulates the scheduling task as a mixed-integer linear program. Within this new method, the schedule is considered as an entity containing all possible observations of an observing session at the same time, leading to a global optimum. In our example, the optimum is found by maximizing the sky coverage score. The sky coverage score is computed by a hierarchical partitioning of the local sky above each telescope into a number of cells. Each cell including at least one observation adds a certain gain to the score. The method is computationally expensive and this publication may be ahead of its time for large networks and large numbers of VLBI observations. However, considering that developments of solvers for combinatorial optimization are progressing rapidly and that computers increase in performance, the usefulness of this approach may come up again in some distant future. Nevertheless, readers may be prompted to look into these optimization methods already today seeing that they are available also in the geodetic literature. The validity of the concept and the applicability of the logic are demonstrated by evaluating test schedules for five 1-h, single-baseline Intensive VLBI sessions. Compared to schedules that were produced with the scheduling software sked, the number of observations per session is increased on average by three observations and the simulated precision of UT1-UTC is improved in four out of five cases (6μs average improvement in quadrature). Moreover, a simplified and thus much faster version of the mixed-integer linear program has been developed for modern VLBI Global Observing System telescopes

    Etablierung eines neuen Hybridsystems zur Züchtung von Möhren mit spezifischer Anbaueignung unter Trocken- und Salzstressbedingungen in Zentralasien

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    Establishment of a new hybrid system for carrot breeding with enhanced drought and salt stress tolerance in Central Asia ZusammenfassungDie Züchtung neuer Möhrenhybriden mit verbesserter Trocken- und Salzstresstoleranz kann einen nachhaltigen Beitrag zur Steigerung der Anbaufläche, höhere Ertragsstabilität und eine wesentliche Qualitätsverbesserung des Erntegutes leisten. Ziel des Projektes ist es ein neues Hybridsystem zu etablieren und geeignete Hybridpartner auf der Basis wissenschaftlicher Evaluierungsdaten zu selektieren. Zur Evaluation und Selektion von trocken- und salzstresstoleranten Möhren-Genotypen wurde ein Prüfverfahren in Topfkultur unter Klimakammerbedingungen entwickelt. Die Ergebnisse der ersten Versuche sollen vorgestellt werden.Stichwörter: Möhren, Hybridsystem, Trocken- und SalzstresstoleranzAbstractPlant breeding of a new carrot hybrid with an enhanced drought and salt stress tolerance may lead to a sustained increase the global carrot production, stabilization of yield and quality. It is the goal to establish a new hybrid system and to select suitable hybrid partners based on scientific evaluation. A laboratory test (climate chamber) was developed to evaluate and select carrot cultivars with salt stress tolerance. The results of the first experiments will be presented. Keywords: carrot, hybrid, drought tolerance, salt stress toleranc

    Considerations of VLBI transmitters on Galileo satellites

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    For directly linking the dynamical reference frame of satellite orbits to the quasi-inertial reference frame of extra-galactic radio sources, observations of satellites with the Very Long Baseline Interferometry (VLBI) technique are the only conceivable method. Hence, the satellite observations should be embedded in VLBI network sessions during which also natural radio sources are observed. For this reason, it would be most practical if the artificial signal generated at the satellite for VLBI observations covers the same frequency bands as regularly observed by VLBI radio telescopes and should have a similar flux density across the observed bandwidth as these natural sources. The use of satellites of Global Navigation Satellite Systems (GNSS) such as the Galileo system is advisable because they are well monitored in terms of precise orbit determination and the altitude allows common visibilities of many VLBI telescopes. So far, signal generation on a GNSS satellite dedicated to VLBI observations has not been realized yet, partly because suitable signal generation equipment has not been considered in depth. In addition, many aspects, such as legal implications and technical complications, have not yet been addressed. In this publication, we compiled various aspects of generating an artificial VLBI signal on a GNSS satellite. We describe the legal and technical aspects of generating and emitting an artificial signal on a Galileo satellite suitable for VLBI observations including a design study for the necessary equipment on the satellite. Since geodetic VLBI is currently in a transition period from traditional observations at S and X band to the broadband VLBI Global Observing System (VGOS), the proposed equipment generates a signal suitable for both frequency setups. We have also considered the restrictions for installation on a satellite, such as power consumption, weight, and size. The equipment mainly consists of three devices: noise source, amplifier, and antenna. A diode is used as the noise source. This noise is amplified by a set of low noise amplifiers and then radiated by a spiral antenna. The diode and the amplifiers were chosen from the market, but the antenna was newly designed and simulated. The output signal of this chain was tested using a VLBI baseband data simulator, then correlated and fringe-fitted for validation. The instrumentation proposed here is easy to be constructed, but will still have to be tested in the laboratory together with the instruments on the actual satellite
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