2,127 research outputs found

    “Will We Ever Learn?”

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    COCAP : a carbon dioxide analyser for small unmanned aircraft systems

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    Unmanned aircraft systems (UASs) could provide a cost-effective way to close gaps in the observation of the carbon cycle, provided that small yet accurate analysers are available. We have developed a COmpact Carbon dioxide analyser for Airborne Platforms (COCAP). The accuracy of COCAP's carbon dioxide (CO2) measurements is ensured by calibration in an environmental chamber, regular calibration in the field and by chemical drying of sampled air. In addition, the package contains a lightweight thermal stabilisation system that reduces the influence of ambient temperature changes on the CO2 sensor by 2 orders of magnitude. During validation of COCAP's CO2 measurements in simulated and real flights we found a measurement error of 1.2 mu mol mol(-1) or better with no indication of bias. COCAP is a self-contained package that has proven well suited for the operation on board small UASs. Besides carbon dioxide dry air mole fraction it also measures air temperature, humidity and pressure. We describe the measurement system and our calibration strategy in detail to support others in tapping the potential of UASs for atmospheric trace gas measurements.Peer reviewe

    Diagnostic and Therapeutic Challenges

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    This case is submitted by Drs. Salvador Pastor-Idoate, Manchester Royal Eye Hospital, and Manchester Vision Regeneration (MVR) Lab at NIHR/Wellcome Trust, Manchester CRF, United Kingdom; Heinrich Heimann, Royal Liverpool and Broadgreen University Hospitals NHS Trust; Pearse A. Keane, Moorfields Eye Hospital, London, United Kingdom, and Konstantinos Balaskas; Manchester Royal Eye Hospital, Manchester, United Kingdom; commented by Dr. Brandon J. Lujan, Portland, Oregon

    Experimental evaluation of confidence interval procedures in sequential steady-state simulation

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    Sequential analysis of simulation output is generally accepted as the most efficient way for securing representativeness of samples of collected observations. In this scenario a simulation experiment is stopped when the relative precision of estimates, defined as the relative width of confidence intervals at an assumed confidence level, reaches the required level. This paper deals with the statistical correctness of the methods proposed for estimating confidence intervals for mean values in sequential steady-state stochastic simulation. We formulate basic rules that should be followed in proper experimental analysis of coverage of different steadystate interval estimators. Our main argument is that such analysis should be done sequentially. The numerical results of our preliminary coverage analysis of the method of Spectral Analysis (SA/HW) and Nonoverlapping Batch Means are presented, and compared with those obtained by traditional, non-sequential approaches

    Bent crystal spectrometer for both frequency and wavenumber resolved x-ray scattering at a seeded free-electron laser

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    We present a cylindrically curved GaAs x-ray spectrometer with energy resolution ΔE/E=1.1104\Delta E/E = 1.1\cdot 10^{-4} and wave-number resolution of Δk/k=3103\Delta k/k = 3\cdot 10^{-3}, allowing plasmon scattering at the resolution limits of the Linac Coherent Light Source (LCLS) x-ray free-electron laser. It spans scattering wavenumbers of 3.6 to 5.2/5.2/\AA\ in 100 separate bins, with only 0.34\% wavenumber blurring. The dispersion of 0.418~eV/13.5μ13.5\,\mum agrees with predictions within 1.3\%. The reflection homogeneity over the entire wavenumber range was measured and used to normalize the amplitude of scattering spectra. The proposed spectrometer is superior to a mosaic HAPG spectrometer when the energy resolution needs to be comparable to the LCLS seeded bandwidth of 1~eV and a significant range of wavenumbers must be covered in one exposure

    Требования к узлу сопряжения секций геохода

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    Проведен анализ работы узла сопряжения секций (УСС) геохода. Сформированы требования к узлу сопряжения секций геохода.The analysis of the operation of the bearing unit of the geokhod is carried out. The requirements for the bearing unit of the geokhod are formed
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