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  • 1
    Keywords: Geography. ; Geography.
    Description / Table of Contents: Introduction -- Surveying the Earth through the ages -- Geodesy in the 21st century - Global reference systems and modern geodetic space observation techniques -- Our planet in focus - Phenomena of global change -- Social relevance of high-precision measurement of our planet from space.
    Abstract: How does your cell phone know where you are right now? How is our planet changing due to geodynamic processes and ongoing climate change? How can these changes be precisely measured from space in order to obtain reliable information about the melting of ice sheets or the threat to coastal regions from rising sea levels? This popular science book provides answers to these and many other socially relevant questions. It is aimed at interested non-professionals who want to learn more about our fascinating planet, but also at experts in natural sciences. You are taken on an exciting journey through time from the first surveys in ancient times to the satellite era, which is providing us with a global view of our home planet. Illustrative examples demonstrate how deeply global positioning and navigation with satellites pervade our daily life, and what fundamental contributions geodesy makes to understanding the Earth system and determining the effects of climate change. With interview contributions by Günter Hein, Harald Lesch and Stefan Rahmstorf. This book is a translation of the original German 1st edition Mission Erde by Detlef Angermann et al., published by Springer-Verlag GmbH Germany, part of Springer Nature in 2021. The translation was done with the help of artificial intelligence (machine translation by the service DeepL.com). Content and language were subsequently revised by the authors. Springer Nature works continuously to further the development of tools for the production of books and on the related technologies to support the authors. The Authors Detlef Angermann holds a doctorate in geodesy and heads the Research Area Reference Systems at the Deutsches Geodätisches Forschungsinstitut of the Technical University of Munich. Roland Pail is Professor of Astronomical and Physical Geodesy at the Technical University of Munich. Florian Seitz is Professor of Geodetic Geodynamics and heads the Deutsches Geodätisches Forschungsinstitut of the Technical University of Munich. Urs Hugentobler is Professor of Satellite Geodesy and heads the Satellite Geodesy Research Facility of the Technical University of Munich.
    Type of Medium: Online Resource
    Pages: XII, 246 p. 74 illus., 68 illus. in color. , online resource.
    Edition: 1st ed. 2022.
    ISBN: 9783662641064
    DDC: 910
    Language: English
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  • 2
    Series available for loan
    Series available for loan
    Zürich : Schweizer. Geodät. Komm.
    Associated volumes
    Call number: SR 90.0084(57)
    In: Geodätisch-geophysikalische Arbeiten in der Schweiz
    Type of Medium: Series available for loan
    Pages: 209 S.
    Series Statement: Geodätisch-geophysikalische Arbeiten in der Schweiz 57
    Language: English
    Location: Lower compact magazine
    Branch Library: GFZ Library
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  • 3
    Call number: M 22.94778
    Type of Medium: Monograph available for loan
    Pages: xii, 246 Seiten , Illustrationen, Diagramme , 23.5 cm x 15.5 cm
    ISBN: 9783662641057 , 3662641054
    Language: English
    Location: Upper compact magazine
    Branch Library: GFZ Library
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  • 4
    Call number: M 21. 94487
    Description / Table of Contents: Einführung -- Die Vermessung der Erde im Wandel der Zeit -- Die Geodäsie im 21. Jahrhundert – Globale Referenzsysteme und moderne geodätische Raumbeobachtungsverfahren -- Unser Planet im Fokus – Phänomene des globalen Wandels -- Gesellschaftliche Relevanz der hochgenauen Vermessung unseres Planeten aus dem Weltraum.
    Description / Table of Contents: Woher weiß Ihr Handy, wo Sie gerade unterwegs sind? Wie verändert sich unser Planet aufgrund von geodynamischen Prozessen und dem fortschreitenden Klimawandel? Wie können diese Veränderungen präzise aus dem Weltraum vermessen werden, um verlässliche Aussagen etwa über das Abschmelzen der Eisschilde oder die Bedrohung von Küstenregionen durch den steigenden Meeresspiegel zu erhalten? Das vorliegende Sachbuch gibt Antworten auf diese gesellschaftlich relevanten Fragen. Es richtet sich an interessierte Laien, die mehr über unseren faszinierenden Planeten erfahren wollen, aber auch an Fachexperten naturwissenschaftlicher Disziplinen. Sie werden mitgenommen auf eine spannende Zeitreise von den ersten Vermessungen in der Antike bis in das Zeitalter der Satelliten, die uns die weltweite Bestimmung von extrem genauen Positionen und eine globale Sicht auf unseren Heimatplaneten ermöglichen. Anhand anschaulicher Beispiele wird vermittelt, wie tief die globale Positionierung und Navigation mit Satelliten unseren Alltag durchdrungen haben, und welche fundamentalen Beiträge die Geodäsie als die Wissenschaft von der Vermessung der Erde zum Verständnis des Erdsystems und zur Bestimmung der Auswirkungen des Klimawandels liefert. Mit Interviewbeiträgen von Günter Hein, Harald Lesch und Stefan Rahmstorf Die Autoren Detlef Angermann ist promovierter Geodät und leitet den Bereich Referenzsysteme am Deutschen Geodätischen Forschungsinstitut der TU München. Roland Pail ist Professor für Astronomische und Physikalische Geodäsie an der TU München. Florian Seitz ist Professor für Geodätische Geodynamik und leitet das Deutsche Geodätische Forschungsinstitut der TU München. Urs Hugentobler ist Professor für Satellitengeodäsie und leitet die Forschungseinrichtung Satellitengeodäsie der TU München.
    Pages: XVI, 275 Seiten , Illustrationen
    ISBN: 9783662623374
    URL: Cover
    Language: German
    Location: Upper compact magazine
    Branch Library: GFZ Library
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  • 5
    Publication Date: 2023-12-15
    Description: Solar radiation pressure (SRP) is the dominant non-gravitational perturbation for GPS satellites. In the IGS (International GNSS Service), this perturbation is modeled differently by individual analysis centers (ACs). The two most widely used methods are the Empirical CODE orbit Model (ECOM, ECOM2) and the JPL GSPM model. When using ECOM models, a box-wing model or other a priori models, as well as stochastic pulses at noon or midnight, are optionally adopted by some ACs to compensate for the deficiencies of the ECOM or ECOM2 model. However, both box-wing and GSPM parameters were published many years ago. There could be an aging effect going with time. Also, optical properties and GSPM parameters of GPS Block IIF satellites are currently not yet published. In this contribution, we first determine Block-specific optical parameters of GPS satellites using GPS code and phase measurements of 6 years. Various physical effects, such as yaw bias, radiator emission in the satellite body-fixed − X and Y directions and the thermal radiation of solar panels, are considered as additional constant parameters in the optical parameter adjustment. With all the adjusted parameters, we form an enhanced box-wing model adding all the modeled physical effects. In addition, we determine Block-specific GSPM parameters by using the same GPS measurements. The enhanced box-wing model and the GSPM model are then taken as a priori model and are jointly used with ECOM and ECOM2 model, respectively. We find that the enhanced box-wing model performs similarly to the GSPM model outside eclipse seasons. RMSs of all the ECOM and ECOM2 parameters are reduced by 30% compared to results without the a priori model. Orbit misclosures and orbit predictions are improved by combining the enhanced box-wing model with ECOM and ECOM2 models. In particular, the improvement in orbit misclosures for the eclipsing Block IIR and IIF satellites, as well as the non-eclipsing IIA satellites, is about 25%, 10% and 10%, respectively, for the ECOM model. Therefore, the enhanced box-wing model is recommended as an a priori model in GPS satellite orbit determination.
    Description: Projekt DEAL
    Keywords: ddc:526 ; GPS solar radiation pressure ; Radiator ; Yaw bias ; GSPM ; Enhanced box-wing model
    Language: English
    Type: doc-type:article
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  • 6
    Publication Date: 2023-07-04
    Description: To resolve undifferenced GNSS phase ambiguities, dedicated satellite products are needed, such as satellite orbits, clock offsets and biases. The International GNSS Service CNES/CLS analysis center provides satellite (HMW) Hatch-Melbourne-Wübbena bias and dedicated satellite clock products (including satellite phase bias), while the CODE analysis center provides satellite OSB (observable-specific-bias) and integer clock products. The CNES/CLS GPS satellite HMW bias products are determined by the Hatch-Melbourne-Wübbena (HMW) linear combination and aggregate both code (C1W, C2W) and phase (L1W, L2W) biases. By forming the HMW linear combination of CODE OSB corrections on the same signals, we compare CODE satellite HMW biases to those from CNES/CLS. The fractional part of GPS satellite HMW biases from both analysis centers are very close to each other, with a mean Root-Mean-Square (RMS) of differences of 0.01 wide-lane cycles. A direct comparison of satellite narrow-lane biases is not easily possible since satellite narrow-lane biases are correlated with satellite orbit and clock products, as well as with integer wide-lane ambiguities. Moreover, CNES/CLS provides no satellite narrow-lane biases but incorporates them into satellite clock offsets. Therefore, we compute differences of GPS satellite orbits, clock offsets, integer wide-lane ambiguities and narrow-lane biases (only for CODE products) between CODE and CNES/CLS products. The total difference of these terms for each satellite represents the difference of the narrow-lane bias by subtracting certain integer narrow-lane cycles. We call this total difference “narrow-lane” bias difference. We find that 3% of the narrow-lane biases from these two analysis centers during the experimental time period have differences larger than 0.05 narrow-lane cycles. In fact, this is mainly caused by one Block IIA satellite since satellite clock offsets of the IIA satellite cannot be well determined during eclipsing seasons. To show the application of both types of GPS products, we apply them for Sentinel-3 satellite orbit determination. The wide-lane fixing rates using both products are more than 98%, while the narrow-lane fixing rates are more than 95%. Ambiguity-fixed Sentinel-3 satellite orbits show clear improvement over float solutions. RMS of 6-h orbit overlaps improves by about a factor of two. Also, we observe similar improvements by comparing our Sentinel-3 orbit solutions to the external combined products. Standard deviation value of Satellite Laser Ranging residuals is reduced by more than 10% for Sentinel-3A and more than 15% for Sentinel-3B satellite by fixing ambiguities to integer values.
    Description: Technische Universität München (1025)
    Keywords: ddc:526 ; Bias comparison ; Sentinel-3A/B ; Undifferenced ambiguity resolution ; CNES/CLS ; CODE
    Language: English
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  • 7
    Publication Date: 2023-06-22
    Description: In this simulation study we analyze the benefit of ground-space optical two-way links (OTWL) for Galileo precise orbit determination (POD). OTWL is a concept based on continuous wave laser ranging and time transfer with modulated signals from and to ground stations. The measurements are in addition to Global Navigation Satellite System (GNSS) observations. We simulate the measurements with regard to 16 Galileo Sensor Stations. In the simulation study we assume that the whole Galileo satellite constellation is equipped with terminals for OTWL. Using OTWL together with Galileo L-band, in comparison with an orbit solution calculated with L-band-only, demonstrates the advantage of combining two ranging techniques with different influences of systematic errors. The two-way link allows a station and satellite clock synchronization. Furthermore, we compare the ground-space concept with the satellite-to-satellite counterpart known as optical two-way inter-satellite links (OISL). The advantage of OTWL is the connection between the satellite system and the solid Earth as well as the possibility to synchronize the satellite clocks and the ground station clocks. The full network, using all three observation types in combination is simulated as well. The possibility to estimate additional solar radiation pressure (SRP) parameters within these combinations is a clear benefit of these additional links. We paid great attention to simulate systematic effects of all observation techniques as realistically as possible. For L-band these are measurement noise, tropospheric delays, phase center variation of receiver and transmitter antennas, constant and variable biases as well as multipath. For optical links we simulated colored and distance-dependent noise, offsets due to the link repeatability and offsets related to the equipment calibration quality. In addition, we added a troposphere error for the OTWL measurements. We discuss the influence on the formal orbit uncertainties and the effects of the systematic errors. Restrictions due to weather conditions are addressed as well. OTWL is synergetic with the other measurement techniques like OISL and can be used for data transfer and communication, respectively.
    Description: Deutsche Forschungsgemeinschaft http://dx.doi.org/10.13039/501100001659
    Description: Technische Universität München (1025)
    Keywords: ddc:526 ; Galileo ; POD ; Optical two-way link ; Inter-satellite link
    Language: English
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  • 8
    Publication Date: 2023-06-22
    Description: Ambiguity resolution of a single receiver is becoming more and more popular for precise GNSS (Global Navigation Satellite System) applications. To serve such an approach, dedicated satellite orbit, clock and bias products are needed. However, we need to be sure whether products based on specific frequencies and signals can be used when processing measurements of other frequencies and signals. For instance, for Galileo E5a frequency, some receivers track only the pilot signal (C5Q) while some track only the pilot-data signal (C5X). We cannot compute the differences between C5Q and C5X directly since these two signals are not tracked concurrently by any common receiver. As code measurements contribute equally as phase in the Melbourne-Wuebbena (MelWub) linear combination it is important to investigate whether C5Q and C5X can be mixed in a network to compute a common satellite MelWub bias product. By forming two network clusters tracking Q and X signals, respectively, we confirm that GPS C5Q and C5X signals cannot be mixed together. Because the bias differences between GPS C5Q and C5X can be more than half of one wide-lane cycle. Whereas, mixing of C5Q and C5X signals for Galileo satellites is possible. The RMS of satellite MelWub bias differences between Q and X cluster is about 0.01 wide-lane cycles for both E1/E5a and E1/E5b frequencies. Furthermore, we develop procedures to compute satellite integer clock and narrow-lane bias products using individual dual-frequency types. Same as the finding from previous studies, GPS satellite clock differences between L1/L2 and L1/L5 estimates exist and show a periodical behavior, with a peak-to-peak amplitude of 0.7 ns after removing the daily mean difference of each satellite. For Galileo satellites, the maximum clock difference between E1/E5a and E1/E5b estimates after removing the mean value is 0.04 ns and the mean RMS of differences is 0.015 ns. This is at the same level as the noise of the carrier phase measurement in the ionosphere-free linear combination. Finally, we introduce all the estimated GPS and Galileo satellite products into PPP-AR (precise point positioning, ambiguity resolution) and Sentinel-3A satellite orbit determination. Ambiguity fixed solutions show clear improvement over float solutions. The repeatability of five ground-station coordinates show an improvement of more than 30% in the east direction when using both GPS and Galileo products. The Sentinel-3A satellite tracks only GPS L1/L2 measurements. The standard deviation (STD) of satellite laser ranging (SLR) residuals is reduced by about 10% when fixing ambiguity parameters to integer values.
    Description: Klinikum rechts der Isar der Technischen Universität München (8934)
    Keywords: ddc:526 ; Integer satellite clock ; Ambiguity resolution ; Daily code and phase biases ; GPS and Galileo signals ; Pilot and data
    Language: English
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  • 9
    Publication Date: 2024-03-12
    Description: The Russian Global Navigation Satellite System (GLONASS) satellites have a stretched body shape and take a specific attitude mode inside the eclipse. Based on previous studies, the new Empirical CODE orbit model (ECOM2) performs better than the classical ECOM model if a satellite has elongated shape or does not maintain yaw-steering mode, and the use of an a priori box-wing (BW) model improves the orbits significantly when employing the ECOM model. However, we find that the ECOM model performs better than the ECOM2 model for GLONASS satellites outside eclipse seasons, while it performs two times worse in eclipse seasons. The use of the conventional box-wing model results in very little improvement. By assessing the ECOM Y〈sub〉0〈/sub〉 estimates, we conclude that there are potential radiators on the -x surface of GLONASS satellites causing orbit perturbations also inside the eclipse. The higher-order Fourier terms of the ECOM2 model can compensate for such effects better than the ECOM model. Based on this finding, we first confirm that GLONASS-K satellites take a similar attitude mode as GLONASS-M satellites inside the eclipse. Then, we adjust optical parameters of GLONASS satellites as part of precise orbit determination (POD) considering the potential radiator and thermal radiation effects. Finally, the adjusted parameters are introduced into a new box-wing model and jointly used with the ECOM and ECOM2 model, respectively. Results show that the amplitude and the dependency of the empirical parameters on the β angle are greatly reduced for both ECOM and ECOM2 models. Rather than the conventional box-wing model, the new box-wing model reduces the orbit misclosure between two consecutive arcs for both GLONASS-M and GLONASS-K satellites. In particular, the improvement in GLONASS-M satellites is more than 30% for the ECOM model during eclipse seasons. Further evaluation from 24-h predicted orbits demonstrates that the improvement during eclipse seasons is mainly in along- and cross-track directions. Finally, we validate GLONASS satellite orbits using Satellite Laser Ranging (SLR) observations. The use of the new box-wing model reduces the spurious pattern of the SLR residuals as a function of β and Δu significantly, and the linear dependency of the SLR residuals on the elongation drops from as large as -0.760 mm/deg to almost zero for both ECOM and ECOM2 models. In general, GLONASS-M satellites benefit more from the new a priori box-wing model and the BW+ECOM model results in the best SLR residuals, with an improvement of about 50% and 20%, respectively, for the mean and standard deviation (STD) values with respect to the orbit products without a priori model.
    Description: Technische Universität München (1025)
    Keywords: ddc:526 ; Solar radiation pressure ; Eclipse ; Radiator ; GLONASS ; Box-wing
    Language: English
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  • 10
    Electronic Resource
    Electronic Resource
    Springer
    General relativity and gravitation 26 (1994), S. 427-428 
    ISSN: 1572-9532
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Type of Medium: Electronic Resource
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