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Neugebauer M. Steinberg J.T. Tokar R.L. Barraclough B.L. Dors E.E. Wiens R.C. Gingerich D.E. Luckey D. Whiteaker D.B. 《Space Science Reviews》2003,105(3-4):661-679
Some of the objectives of the Genesis mission require the separate collection of solar wind originating in different types
of solar sources. Measurements of the solar wind protons, alpha particles, and electrons are used on-board the spacecraft
to determine whether the solar-wind source is most likely a coronal hole, interstream flow, or a coronal mass ejection. A
simple fuzzy logic scheme operating on measurements of the proton temperature, the alpha-particle abundance, and the presence
of bidirectional streaming of suprathermal electrons was developed for this purpose. Additional requirements on the algorithm
include the ability to identify the passage of forward shocks, reasonable levels of hysteresis and persistence, and the ability
to modify the algorithm by changes in stored constants rather than changes in the software. After a few minor adjustments,
the algorithm performed well during the initial portion of the mission.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
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Möbius E. Kistler L.M. Popecki M.A. Crocker K.N. Granoff M. Turco S. Anderson A. Demain P. Distelbrink J. Dors I. Dunphy P. Ellis S. Gaidos J. Googins J. Hayes R. Humphrey G. Kästle H. Lavasseur J. Lund E.J. Miller R. Sartori E. Shappirio M. Taylor S. Vachon P. Vosbury M. Ye V. Hovestadt D. Klecker B. Arbinger H. Künneth E. Pfeffermann E. Seidenschwang E. Gliem F. Reiche K.-U. Stöckner K. Wiewesiek W. Harasim A. Schimpfle J. Battell S. Cravens J. Murphy G. 《Space Science Reviews》1998,86(1-4):449-495
The Solar Energetic Particle Ionic Charge Analyzer (SEPICA) is the main instrument on the Advanced Composition Explorer (ACE)
to determine the ionic charge states of solar and interplanetary energetic particles in the energy range from ≈0.2 MeV nucl−1
to ≈5 MeV charge−1. The charge state of energetic ions contains key information to unravel source temperatures, acceleration,
fractionation and transport processes for these particle populations. SEPICA will have the ability to resolve individual charge
states and have a substantially larger geometric factor than its predecessor ULEZEQ on ISEE-1 and -3, on which SEPICA is based.
To achieve these two requirements at the same time, SEPICA is composed of one high-charge resolution sensor section and two
low- charge resolution, but large geometric factor sections. The charge resolution is achieved by the focusing of the incoming
ions, through a multi-slit mechanical collimator, deflection in an electrostatic analyzer with a voltage up to 30 kV, and
measurement of the impact position in the detector system. To determine the nuclear charge (element) and energy of the incoming
ions, the combination of thin-window flow-through proportional counters with isobutane as counter gas and ion-implanted solid
state detectors provide for 3 independent ΔE (energy loss) versus E (residual energy) telescopes. The multi-wire proportional
counter simultaneously determines the energy loss ΔE and the impact position of the ions. Suppression of background from penetrating
cosmic radiation is provided by an anti-coincidence system with a CsI scintillator and Si-photodiodes. The data are compressed
and formatted in a data processing unit (S3DPU) that also handles the commanding and various automatted functions of the instrument.
The S3DPU is shared with the Solar Wind Ion Charge Spectrometer (SWICS) and the Solar Wind Ion Mass Spectrometer (SWIMS) and
thus provides the same services for three of the ACE instruments. It has evolved out of a long family of data processing units
for particle spectrometers.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
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The FIELDS Instrument Suite on MMS: Scientific Objectives,Measurements, and Data Products 总被引:1,自引:0,他引:1
R. B. Torbert C. T. Russell W. Magnes R. E. Ergun P.-A. Lindqvist O. LeContel H. Vaith J. Macri S. Myers D. Rau J. Needell B. King M. Granoff M. Chutter I. Dors G. Olsson Y. V. Khotyaintsev A. Eriksson C. A. Kletzing S. Bounds B. Anderson W. Baumjohann M. Steller K. Bromund Guan Le R. Nakamura R. J. Strangeway H. K. Leinweber S. Tucker J. Westfall D. Fischer F. Plaschke J. Porter K. Lappalainen 《Space Science Reviews》2016,199(1-4):105-135
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O.?Le?ContelEmail author P.?Leroy A.?Roux C.?Coillot D.?Alison A.?Bouabdellah L.?Mirioni L.?Meslier A.?Galic M.?C.?Vassal R.?B.?Torbert J.?Needell D.?Rau I.?Dors R.?E.?Ergun J.?Westfall D.?Summers J.?Wallace W.?Magnes A.?Valavanoglou G.?Olsson M.?Chutter J.?Macri S.?Myers S.?Turco J.?Nolin D.?Bodet K.?Rowe M.?Tanguy B.?de?la?Porte 《Space Science Reviews》2016,199(1-4):257-282
The tri-axial search-coil magnetometer (SCM) belongs to the FIELDS instrumentation suite on the Magnetospheric Multiscale (MMS) mission (Torbert et al. in Space Sci. Rev. (2014), this issue). It provides the three magnetic components of the waves from 1 Hz to 6 kHz in particular in the key regions of the Earth’s magnetosphere namely the subsolar region and the magnetotail. Magnetospheric plasmas being collisionless, such a measurement is crucial as the electromagnetic waves are thought to provide a way to ensure the conversion from magnetic to thermal and kinetic energies allowing local or global reconfigurations of the Earth’s magnetic field. The analog waveforms provided by the SCM are digitized and processed inside the digital signal processor (DSP), within the Central Electronics Box (CEB), together with the electric field data provided by the spin-plane double probe (SDP) and the axial double probe (ADP). On-board calibration signal provided by DSP allows the verification of the SCM transfer function once per orbit. Magnetic waveforms and on-board spectra computed by DSP are available at different time resolution depending on the selected mode. The SCM design is described in details as well as the different steps of the ground and in-flight calibrations. 相似文献
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Barraclough B.L. Dors E.E. Abeyta R.A. Alexander J.F. Ameduri F.P. Baldonado J.R. Bame S.J. Casey P.J. Dirks G. Everett D.T. Gosling J.T. Grace K.M. Guerrero D.R. Kolar J.D. Kroesche J.L. Lockhart W.L. McComas D.J. Mietz D.E. Roese J. Sanders J. Steinberg J.T. Tokar R.L. Urdiales C. Wiens R.C. 《Space Science Reviews》2003,105(3-4):627-660
The Genesis Ion Monitor (GIM) and the Genesis Electron Monitor (GEM) provide 3-dimensional plasma measurements of the solar
wind for the Genesis mission. These measurements are used onboard to determine the type of plasma that is flowing past the
spacecraft and to configure the solar wind sample collection subsystems in real-time. Both GIM and GEM employ spherical-section
electrostatic analyzers followed by channel electron multiplier (CEM) arrays for detection and angle and energy/charge analysis
of incident ions and electrons. GIM is of a new design specific to Genesis mission requirements whereas the GEM sensor is
an almost exact copy of the plasma electron sensors currently flying on the ACE and Ulysses spacecraft, albeit with new electronics
and programming. Ions are detected at forty log-spaced energy levels between ∼ 1 eV and 14 keV by eight CEM detectors, while
electrons with energies between ∼ 1 eV and 1.4 keV are measured at twenty log-spaced energy levels using seven CEMs. The spin
of the spacecraft is used to sweep the fan-shaped fields-of-view of both instruments across all areas of the sky of interest,
with ion measurements being taken forty times per spin and samples of the electron population being taken twenty four times
per spin. Complete ion and electron energy spectra are measured every ∼ 2.5 min (four spins of the spacecraft) with adequate
energy and angular resolution to determine fully 3-dimensional ion and electron distribution functions. The GIM and GEM plasma
measurements are principally used to enable the operational solar wind sample collection goals of the Genesis mission but
they also provide a potentially very useful data set for studies of solar wind phenomena, especially if combined with other
solar wind data sets from ACE, WIND, SOHO and Ulysses for multi-spacecraft investigations.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
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R. B. Torbert H. Vaith M. Granoff M. Widholm J. A. Gaidos B. H. Briggs I. G. Dors M. W. Chutter J. Macri M. Argall D. Bodet J. Needell M. B. Steller W. Baumjohann R. Nakamura F. Plaschke H. Ottacher J. Hasiba K. Hofmann C. A. Kletzing S. R. Bounds R. T. Dvorsky K. Sigsbee V. Kooi 《Space Science Reviews》2016,199(1-4):283-305
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R. B. Torbert H. Vaith M. Granoff M. Widholm J. A. Gaidos B. H. Briggs I. G. Dors M. W. Chutter J. Macri M. Argall D. Bodet J. Needell M. B. Steller W. Baumjohann R. Nakamura F. Plaschke H. Ottacher J. Hasiba K. Hofmann C. A. Kletzing S. R. Bounds R. T. Dvorsky K. Sigsbee V. Kooi 《Space Science Reviews》2016,199(1-4):307-308
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