GLONASS-K attitude: rapid turning maneuvers and other deviations from ideal yaw steering

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This paper describes GLONASS-K yaw turn maneuvers that occur regularly near orbit noon and orbit midnight and provides formulas to model these maneuvers when the Sun’s elevation angle relative to the satellite orbital plane is between −2.0 and +2.0 degrees. The authors analyze triple-frequency carrier-phase observations from the global IGS tracking network to evaluate how well the model predicts yaw performance, using yaw angle estimates for the first GLONASS-K1 and first GLONASS-K2 spacecraft. They report that the actual yaw attitude follows the theoretical steering model with an accuracy of about 2 degrees, and they present examples of other systematic deviations from ideal yaw attitude. The paper’s evaluation is limited to these two spacecraft and the stated Sun-elevation conditions. The paper does not explicitly discuss endometriosis or adenomyosis; it was included in the corpus via a keyword match in the upstream search index.

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Abstract

AbstractThis paper provides a description of the GLONASS-K yaw turn maneuvers that regularly occur at orbit noon and orbit midnight when the Sun’s elevation angle relative to the satellite orbital plane is between − 2.0 and + 2.0 degrees. Formulas for maneuver modeling are presented, which can be easily integrated into any Global Navigation Satellite System (GNSS) software. Triple-frequency carrier phase observations from the global International GNSS Service (IGS) tracking network are analyzed to evaluate the performance of the model. Yaw angle estimates for the first GLONASS-K1 and first GLONASS-K2 spacecraft indicate that the actual yaw attitude follows the theoretical steering model with an accuracy of about 2 degrees. In addition to the regular yaw maneuvers, examples of other systematic deviations from the ideal GLONASS-K yaw attitude are presented.
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GLONASS-K attitude: rapid turning maneuvers and other deviations from ideal yaw steering | Research Square window.SnipcartSettings = { analytics: { enabled: false } }; (function() { var accessVector = localStorage.getItem('access_vector') || ''; window.dataLayer = window.dataLayer || []; if (accessVector) { window.dataLayer.push({ user: { profile: { profileInfo: { snid: accessVector } } } }); } })(); (function(w,d,s,l,i){w[l]=w[l]||[];w[l].push({'gtm.start':new Date().getTime(),event:'gtm.js'});var f=d.getElementsByTagName(s)[0],j=d.createElement(s),dl=l!='dataLayer'?'&l='+l:'';j.async=true;j.src='https://www.googletagmanager.com/gtm.js?id='+i+dl;f.parentNode.insertBefore(j,f);})(window,document,'script','dataLayer','GTM-K279D39R'); Browse Preprints In Review Journals COVID-19 Preprints AJE Video Bytes Research Tools Research Promotion AJE Professional Editing AJE Rubriq About Preprint Platform In Review Editorial Policies Our Team Advisory Board Help Center Sign In Submit a Preprint Cite Share Download PDF Research Article GLONASS-K attitude: rapid turning maneuvers and other deviations from ideal yaw steering Florian Dilssner, Tim Springer This is a preprint; it has not been peer reviewed by a journal. https://doi.org/ 10.21203/rs.3.rs-4102651/v1 This work is licensed under a CC BY 4.0 License Status: Published Journal Publication published 19 Jun, 2024 Read the published version in GPS Solutions → Version 1 posted 7 You are reading this latest preprint version Abstract This paper provides a description of the GLONASS-K yaw turn maneuvers that regularly occur at orbit noon and orbit midnight when the Sun’s elevation angle relative to the satellite orbital plane is between − 2.0 and + 2.0 degrees. Formulas for maneuver modeling are presented, which can be easily integrated into any Global Navigation Satellite System (GNSS) software. Triple-frequency carrier phase observations from the global International GNSS Service (IGS) tracking network are analyzed to evaluate the performance of the model. Yaw angle estimates for the first GLONASS-K1 and first GLONASS-K2 spacecraft indicate that the actual yaw attitude follows the theoretical steering model with an accuracy of about 2 degrees. In addition to the regular yaw maneuvers, examples of other systematic deviations from the ideal GLONASS-K yaw attitude are presented. GNSS IGS GLONASS-K yaw attitude Full Text Additional Declarations No competing interests reported. Cite Share Download PDF Status: Published Journal Publication published 19 Jun, 2024 Read the published version in GPS Solutions → Version 1 posted Editorial decision: Revision requested 06 Jun, 2024 Reviews received at journal 29 Apr, 2024 Reviewers agreed at journal 10 Apr, 2024 Reviewers invited by journal 27 Mar, 2024 Editor assigned by journal 27 Mar, 2024 Submission checks completed at journal 20 Mar, 2024 First submitted to journal 14 Mar, 2024 You are reading this latest preprint version Research Square lets you share your work early, gain feedback from the community, and start making changes to your manuscript prior to peer review in a journal. As a division of Research Square Company, we’re committed to making research communication faster, fairer, and more useful. We do this by developing innovative software and high quality services for the global research community. Our growing team is made up of researchers and industry professionals working together to solve the most critical problems facing scientific publishing. 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