2018
DOI: 10.1007/s11431-018-9241-7
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The electromagnetic wave experiment for CSES mission: Search coil magnetometer

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Cited by 54 publications
(34 citation statements)
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“…The SCM on the CSES was manufactured by Beihang University, China; it is designed to measure the magnetic field fluctuation or electromagnetic waves in the low frequency range of 10 Hz–20 kHz (Cao JB et al, ). The SCM is comprised of a three‐axis search coil sensor mounted on a 4.5 m boom.…”
Section: Initial Results From Scientific Payloadsmentioning
confidence: 99%
“…The SCM on the CSES was manufactured by Beihang University, China; it is designed to measure the magnetic field fluctuation or electromagnetic waves in the low frequency range of 10 Hz–20 kHz (Cao JB et al, ). The SCM is comprised of a three‐axis search coil sensor mounted on a 4.5 m boom.…”
Section: Initial Results From Scientific Payloadsmentioning
confidence: 99%
“…Then the digital processing unit processes the digitized signals and outputs the waveform and spectral data. The performance of the SCM, including its sensitivity, transfer functions, and calibration results, were checked in the paper of Cao JB et al ().…”
Section: Scm Data Descriptionmentioning
confidence: 99%
“…It aims to measure the magnetic field fluctuation of low‐frequency EM waves in the frequency range of 10 Hz to 20 kHz. Ground calibration results have indicated that SCM is advanced compared the current SCMs in other international space missions, particularly in terms of the –3 dB measurement bandwidth, frequency resolution, and sensitivity (Cao JB et al, ). In this paper, the definitions of each level of the SCM data product are presented in Section 2.…”
Section: Introductionmentioning
confidence: 99%
“…It is the first satellite in China to measure geophysical fields. It carries eight instruments, including a search‐coil magnetometer (SCM) (Cao JB et al, ), electric field detector (EFD), high precision magnetometer (HPM) (Cheng BJ et al, ), GNSS occultation receiver (GOR), plasma analyzer package (PAP), Langmuir probe (LAP), high energetic particle package (HEPP) and detector (HEPD) (Ambrosi et al, ), and tri‐band beacon (TBB). The satellite has a sun‐synchronous orbit at an altitude of 507 km and a descending node time of 14:00 LT.…”
Section: Introductionmentioning
confidence: 99%