150 research outputs found

    DGNSS-Vision Integration for Robust and Accurate Relative Spacecraft Navigation

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    Relative spacecraft navigation based on Global Navigation Satellite System (GNSS) has been already successfully performed in low earth orbit (LEO). Very high accuracy, of the order of the millimeter, has been achieved in postprocessing using carrier phase differential GNSS (CDGNSS) and recovering the integer number of wavelength (Ambiguity) between the GNSS transmitters and the receiver. However the performance achievable on-board, in real time, above LEO and the GNSS constellation would be significantly lower due to limited computational resources, weaker signals, and worse geometric dilution of precision (GDOP). At the same time, monocular vision provides lower accuracy than CDGNSS when there is significant spacecraft separation, and it becomes even lower for larger baselines and wider field of views (FOVs). In order to increase the robustness, continuity, and accuracy of a real-time on-board GNSS-based relative navigation solution in a GNSS degraded environment such as Geosynchronous and High Earth Orbits, we propose a novel navigation architecture based on a tight fusion of carrier phase GNSS observations and monocular vision-based measurements, which enables fast autonomous relative pose estimation of cooperative spacecraft also in case of high GDOP and low GNSS visibility, where the GNSS signals are degraded, weak, or cannot be tracked continuously. In this paper we describe the architecture and implementation of a multi-sensor navigation solution and validate the proposed method in simulation. We use a dataset of images synthetically generated according to a chaser/target relative motion in Geostationary Earth Orbit (GEO) and realistic carrier phase and code-based GNSS observations simulated at the receiver position in the same orbits. We demonstrate that our fusion solution provides higher accuracy, higher robustness, and faster ambiguity resolution in case of degraded GNSS signal conditions, even when using high FOV cameras

    X-ray scaling relations of early-type galaxies in IllustrisTNG and a new way of identifying backsplash objects

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    We investigate how feedback and environment shapes the X-ray scaling relations of early-type galaxies (ETGs), especially at the low-mass end. We select central-ETGs from the IllustrisTNG-100 box that have stellar masses log10(M/M)[10.7,11.9]\log_{10}(M_{\ast}/\mathrm{M_{\odot}})\in[10.7, 11.9]. We derive mock X-ray luminosity (LX,500L_{\mathrm{X, 500}}) and spectroscopic-like temperature (Tsl,500T_{\mathrm{sl, 500}}) of hot gas within R500R_{500} of the ETG haloes using the MOCK-X pipeline. The scaling between LX,500L_{\mathrm{X, 500}} and the total mass within 5 effective radii (M5ReM_{5R_{\rm e}}) agrees well with observed ETGs from Chandra. IllustrisTNG reproduces the observed increase in scatter of LX,500L_{\mathrm{X, 500}} towards lower masses, and we find that ETGs with log10(M5Re/M)11.5\log_{10} (M_{5R_{\rm e}}/\mathrm{M_{\odot}}) \leqslant 11.5 with above-average LX,500L_{\mathrm{X, 500}} experienced systematically lower cumulative kinetic AGN feedback energy historically (vice versa for below-average ETGs). This leads to larger gas mass fractions and younger stellar populations with stronger stellar feedback heating, concertedly resulting in the above-average LX,500L_{\mathrm{X, 500}}. The LX,500L_{\mathrm{X, 500}}--Tsl,500T_{\mathrm{sl, 500}} relation shows a similar slope to the observed ETGs but the simulation systematically underestimates the gas temperature. Three outliers that lie far below the LXL_{\rm X}--TslT_{\rm sl} relation all interacted with larger galaxy clusters recently and demonstrate clear features of environmental heating. We propose that the distinct location of these backsplash ETGs in the LXL_{\rm X}--TslT_{\rm sl} plane could provide a new way of identifying backsplash galaxies in future X-ray surveys.Comment: 16 pages, 10 figures. Submitted to MNRA

    Urogynecology digest

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