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  • 1
    Electronic Resource
    Electronic Resource
    [S.l.] : American Institute of Physics (AIP)
    Review of Scientific Instruments 64 (1993), S. 2771-2781 
    ISSN: 1089-7623
    Source: AIP Digital Archive
    Topics: Physics , Electrical Engineering, Measurement and Control Technology
    Notes: We have developed a fast real-time spectral analysis algorithm for space plasma three-dimensional (3D) ion mass spectrometers that deconvolves contributions to time-of-flight ion mass spectra for various ion species abundances. The algorithm is composed of a set of coupled linear equations with constant coefficients. The algorithm is implemented so that in-flight computers need only apply a predetermined number of multiplies and adds to the spectral data. The algorithm allows run times to be short and highly predictable, can accommodate the presence of background in the ion mass spectra, and can be updated to adjust to calibration changes and unexpected instrument anomalies or failures. Space plasma 3D ion mass spectrometers have the capability of generating large volumes of data and if not compressed would produce data rates that far exceed the telemetry rate usually allocated to space plasma instruments. The real-time application of this algorithm allows one to achieve compression ratios greater than 100 for the spectral data without introducing systematic errors to the computed ion abundances. It also allows the application of other higher level data compression techniques to provide additional compression of the telemetry data. Finally, the algorithm can be thought of as a way to increase the mass resolution of the ion spectrometer.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Space science reviews 87 (1999), S. 199-206 
    ISSN: 1572-9672
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Notes: Abstract We have developed a 2D semi-empirical model (Sittler and Guhathakurta 1999) of the corona and the interplanetary medium using the time independent MHD equations and assuming azimuthal symmetry, utilizing the SOHO, Spartan and Ulysses observations. The model uses as inputs (1) an empirically derived global electron density distribution using LASCO, Mark III and Spartan white light observations and in situ observations of the Ulysses spacecraft, and (2) an empirical model of the coronal magnetic field topology using SOHO/LASCO and EIT observations. The model requires an estimate of solar wind velocity as a function of latitude at 1 AU and the radial component of the magnetic field at 1 AU, for which we use Ulysses plasma and magnetic field data results respectively. The model makes estimates as a function of radial distance and latitude of various fluid parameters of the plasma such as flow velocity V, temperature Teff, and heat flux Qeff which are derived from the equations of conservation of mass, momentum and energy, respectively, in the rotating frame of the Sun. The term "effective" indicates possible wave contributions. The model can be used as a planning tool for such missions as Solar Probe and provide an empirical framework for theoretical models of the solar corona and solar wind.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    [s.l.] : Nature Publishing Group
    Nature 292 (1981), S. 711-714 
    ISSN: 1476-4687
    Source: Nature Archives 1869 - 2009
    Topics: Biology , Chemistry and Pharmacology , Medicine , Natural Sciences in General , Physics
    Notes: [Auszug] DURING the Voyager 1 encounter with Saturn, the electron plasma in the energy range 10-5,950 eV was sampled by the plasma science experiment (PLS). The electron distribution function in the vicinity of Saturn is comprised of smoothly joined thermal and suprathermal components; it is not well ...
    Type of Medium: Electronic Resource
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  • 4
    ISSN: 1572-9672
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Notes: Abstract The Solar Wind Experiment (SWE) on the WIND spacecraft is a comprehensive, integrated set of sensors which is designed to investigate outstanding problems in solar wind physics. It consists of two Faraday cup (FC) sensors; a vector electron and ion spectrometer (VEIS); a strahl sensor, which is especially configured to study the electron ‘strahl’ close to the magnetic field direction; and an on-board calibration system. The energy/charge range of the Faraday cups is 150 V to 8 kV, and that of the VEIS is 7 V to 24.8 kV. The time resolution depends on the operational mode used, but can be of the order of a few seconds for 3-D measurements. ‘Key parameters’ which broadly characterize the solar wind positive ion velocity distribution function will be made available rapidly from the GGS Central Data Handling Facility.
    Type of Medium: Electronic Resource
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