DocumentCode :
396
Title :
Earth Magnetic Field Effects on Particle Sensors on LEO Satellites
Author :
Rehman, Saif Ur ; Marchand, Richard ; Berthelier, Jean-Jacques ; Onishi, Teruo ; Burchill, Johnathan
Author_Institution :
Dept. of Phys., Univ. of Alberta, Edmonton, AB, Canada
Volume :
41
Issue :
12
fYear :
2013
fDate :
Dec. 2013
Firstpage :
3402
Lastpage :
3409
Abstract :
Kinetic simulation results are presented for the interaction of spacecraft with space environment in low Earth orbit. Case studies are considered for DEMETER, for which small but distinctive potential variations have been measured on Instrument Champ Electrique (ICE) sensors, as the satellite goes through regions where the magnetic field B is nearly parallel to the satellite velocity v. Our results point to a small variation in the potential of ICE probes under these conditions, but owing to the smallness of the signal and inherent statistical noise in our simulations, it is not possible to unambiguously explain observations. An earlier study of magnetic field effects on the Swarm electric field instrument is extended by computing Langmuir probe characteristics with and without a magnetic field. The possibility of probe crosstalk is also examined by comparing collected currents when the two probes have same and opposite bias voltages. Accounting for a representative ionospheric magnetic field is found to lead to appreciable quantitative differences in the probe characteristics. No significant crosstalk or mutual coupling is predicted between the probes under normal operation.
Keywords :
Langmuir probes; artificial satellites; astrophysical plasma; atmospheric measuring apparatus; geomagnetism; ionosphere; magnetosphere; plasma kinetic theory; plasma magnetohydrodynamics; plasma simulation; DEMETER; Earth magnetic field effects; ICE sensors; Instrument Champ Electrique sensors; LEO satellite particle sensors; Langmuir probe characteristics; Swarm electric field instrument; bias voltage; kinetic simulation; low Earth orbit satellite; probe crosstalk; spacecraft-space environment interaction; Electric potential; Magnetic sensors; Payloads; Plasmas; Probes; Space vehicles; Induced electric effects; local magnetic field effects; low Earth orbit (LEO); sheath;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2013.2262715
Filename :
6542760
Link To Document :
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