Date post: | 17-Jan-2016 |
Category: |
Documents |
Upload: | blanche-norris |
View: | 215 times |
Download: | 1 times |
THEMIS ESA SWT ESA-1 UCB, Aug 6 - 8 2007
ESA In-Flight Calibration and First Results
J. McFadden, C. Carlson, D. Larson UC Berkeley SSL
THEMIS ESA SWT ESA-2 UCB, Aug 6 - 8 2007
Requirements and Specifications
• The ESA instrument measures 3-D electron and ion energy distribution functions over the Energy range ~5 eV to 30 keV (25 keV for ions).
• Typical energy sweep has 16 or 32 energy samples and logrithmic sweep (dE/E~constant).
• A full 4-pi distribution measurement is produced during each spin.
• Sweep rate of 32/spin gives dense sample of 3-D particle distributions. Ion sensor is capable of 64 sweeps/spin to provide adequate sampling of solar wind.
• The ETC board compresses the raw measurements into three selectable “distributions arrays” that come down in separate packets (full, burst and reduced packets) at selectable rates.
• The ETC also computes moments with corrections for detector efficiency and spacecraft potential.
THEMIS ESA SWT ESA-3 UCB, Aug 6 - 8 2007
Block Diagram
• Electronics functional design is identical to FAST (with ACTEL upgrades)• Three circuit modules plug together for efficient assembly and test• MCP pulse amplifiers are Amptek A121 with programmable gain• All discrete logic, counters, and HV DAC drivers are Actel FPGAs• HV & LV supplies are mature designs built at UCB SSL
THEMIS ESA SWT ESA-4 UCB, Aug 6 - 8 2007
ESA S/C INTERFACE
Ion ESA Electron ESA 16 Anodes 8 Anodes
Ion and Electron ESAs are packaged together.
180 deg x 6 deg field of view
Sensors have different anode patterns.
THEMIS ESA SWT ESA-5 UCB, Aug 6 - 8 2007
ESA Data Types
THEMIS produces four basic ESA data products for each species with resolution that depends upon instrument mode:
Full distributions – Low cadence (~32 or 128 spin resolution), high resolution energy-angle (32E x 88A) distributions, taken continuously over the orbit.
Burst distributions – High cadence (every spin), high resolution energy-angle (32E x 88A) triggered snapshots (~4 minutes).
Reduced distributions – High cadence (every spin), lower resolution (32E x 1A i+&e-, 32E x 6A e-, or 24E x 50A i+) distributions taken continuously over the orbit.
Onboard Moments – High cadence (every spin) density, velocity, pressure, heat flux.
THEMIS ESA SWT ESA-6 UCB, Aug 6 - 8 2007
ESA Data Types
Typical 88 solid-angle map used for sorting full and burst data
THEMIS ESA SWT ESA-7 UCB, Aug 6 - 8 2007
ESA Data Analysis Software 1
Data structure at right is loaded into IDL memory by the below routines.
thm_load_esa_pkt.pro – creates 6 IDL ESA data structures containing time, counts, energy & angle arrays, geometric factors, etc.
thm_load_esa_pot.pro – adds the spacecraft potential to the ESA data structures.
thm_load_esa_mag.pro – adds the magnetic field to the ESA data structures.
PROJECT_NAME STRING 'THEMIS' SPACECRAFT STRING 'c' DATA_NAME STRING 'IESA 3D Reduced' APID INT 455 UNITS_NAME STRING 'compressed' UNITS_PROCEDURE STRING 'thm_convert_esa_units' VALID BYTE Array[27909] TIME DOUBLE Array[27909] END_TIME DOUBLE Array[27909] DELTA_T DOUBLE Array[27909] INTEG_T DOUBLE Array[27909] DT_ARR FLOAT Array[32, 88, 8] CS_PTR LONG Array[27909] CS_IND INT Array[27909] CONFIG1 BYTE Array[27909] CONFIG2 BYTE Array[27909] AN_IND INT Array[27909] EN_IND INT Array[27909] MD_IND INT Array[27909] NENERGY INT Array[6] ENERGY FLOAT Array[32, 6] DENERGY FLOAT Array[32, 6] EFF FLOAT Array[32, 6] NBINS INT Array[8] THETA FLOAT Array[32, 88, 8] DTHETA FLOAT Array[32, 88, 8] PHI FLOAT Array[32, 88, 8] DPHI FLOAT Array[32, 88, 8] PHI_OFFSET FLOAT Array[27909] DOMEGA FLOAT Array[32, 88, 8] GF FLOAT Array[32, 88, 8] GEOM_FACTOR FLOAT 0.00110000 DEAD FLOAT 1.60000e-007 MASS FLOAT 0.0104389 CHARGE FLOAT 1.00000 SC_POT FLOAT Array[27909] B_GSE FLOAT Array[27909, 3] MAGF FLOAT Array[27909, 3] DAT0 BYTE Array[6, 16] DAT1 BYTE Array[13753, 32] DAT2 BYTE Array[1, 96] DAT3 BYTE Array[1, 192] DAT4 BYTE Array[1, 1152] DAT5 BYTE Array[14150, 1200]
THEMIS ESA SWT ESA-8 UCB, Aug 6 - 8 2007
ESA Data Analysis Software 2
Commands to load & plot ESA data: startdate = '2007-07-31/0:00'sc='b'ndays=1thm_inittimespan,startdate,ndaysthm_load_state,probe=scthm_load_esa_pkt,probe=scthm_load_esa_mag,sc=scthm_load_esa_pot,sc=sc
tplot,[‘thb_pe??_en_counts’]
Default plots are in “counts”. Note discontinuity in ion 24 energy mode.Calibrated data in energy flux do not have this discontinuity.
THEMIS ESA SWT ESA-9 UCB, Aug 6 - 8 2007
ESA Data Analysis Software 2
Once the data are loaded, use these routines to return an ESA data structure at a single time. get_thc_peir.pro
p – particle (f – fields)e – ESA (s – SST)i – ion (e - electron)r – reduced (f-full,b-burst)
Routines that operate on structures
n_3d_new.prov_3d_new.pro
Loop routines for time series plotsget_2dt.proget_en_spec.pro
Example IDL commands
t=‘2007-5-5/12:31’dat=get_thc_peir(t)dat=get_thc_peir() dat=get_thc_peir(/ad)dat=get_thc_peir(/re)
print,n_3d_new(dat)print,n_3d_new(dat,energy=[0,20])
get_2dt,’n_3d_new’,’thc_peir’get_en_spec,’thc_peir’,name=‘test’
THEMIS ESA SWT ESA-10 UCB, Aug 6 - 8 2007
ESA Plot Types and Units 1
Once the data are loaded, there are several plotting routines.
dat=get_thb_peif()
spec3d,dat
spec3d,dat,units=‘df’
Each angle bin is a different color curve.
For 3-D angle maps use:
plot3d,dat
THEMIS ESA SWT ESA-11 UCB, Aug 6 - 8 2007
ESA Plot Types and Units 2
Plot3d acting on data structure “dat” produces the below plot.Example IDL command: plot3d,dat,/zero
Magnetic field indicated by plus and diamond
THEMIS ESA SWT ESA-12 UCB, Aug 6 - 8 2007
ESA Plot Types and Units 3
IDL routines for time series plots
get_en_spec
get_2dt
THEMIS ESA SWT ESA-13 UCB, Aug 6 - 8 2007
ESA In-Flight Calibration
ESA in-flight calibration and instrument maintenance requires:
1. Getting the timing straightened out - finished2. MCP Bias Voltage determination - ongoing3. Sunlight contamination - minimal4. Spacecraft potential correction - in place5. Dead-time corrections - in place6. Energy efficiency corrections - in progress7. Relative efficiency corrections - TBD8. Absolute efficiency - TBD9. Electron-Ion cross calibration - TBD10. Inter-spacecraft cross calibrations - TBD
THEMIS ESA SWT ESA-14 UCB, Aug 6 - 8 2007
ESA MCP detector tests
A121 preamps allow simple determination of MCP bias voltage requirements. Toggling the gain should change efficiency by factor of ~ 2-3 for proper MCP bias voltage.
Electron sensor (panel 3&4) above showed efficiency changes of ~4 so MCP bias voltage was raised 50V. The gain test repeated to the right confirms proper operation. Bias voltage changes (not shown) are also toggled to expose any significant losses near threshold.
THEMIS ESA SWT ESA-15 UCB, Aug 6 - 8 2007
Sunlight & Photo-electrons
No measureable direct sunlight contamination. Spacecraft photo-electrons must be eliminated.Photo-electrons are produced in the aperture, on the spacecraft and on langmuir probes.
sc_pot=20V
sc_pot=11V
Wire boom photo-e
sc_pot=45V
Axial boom photo-e
Wire boom photo-e
s/c photo-e
THEMIS ESA SWT ESA-16 UCB, Aug 6 - 8 2007
Correcting for s/c potential
Thm_load_esa_pot.pro
Software currently assumes s/c potential is 1.15 times the measured average spin plane boom potential (V1234) plus 1 volt contact potential. 1.15 calibration factor determined from density comparisons.
Similar to simulations conducted by Cully.
s/c potential corrections are important for electrons and cold ions.
THEMIS ESA SWT ESA-17 UCB, Aug 6 - 8 2007
Correcting for dead time
Total dead-time is a combination of “preamplifier dead-time” and “detector dead-time”, which is difficult to calibrate and depends on MCP bias voltage and preamplifier threshold.
For the above case, high density results in significant electron ESA deadtime. This allowed an estimate of total deadtime (~0.16 us) by eliminating the slope in the Ni/Ne density ratio (right, bottom panel).
THEMIS ESA SWT ESA-18 UCB, Aug 6 - 8 2007
Detector Energy Efficiency 1
Default ion efficiency assumes lab results from Funsten.
For log energy and 2 kV pre-acceleration, the efficiency is shown below.
Energy (eV)
THEMIS ESA SWT ESA-19 UCB, Aug 6 - 8 2007
Detector Energy Efficiency 2
Electron efficiency assumes:“Relative electron detection efficiency of microchannel plates from 0-3 keV”, R.R. Goruganthu and W. G. Wilson, Rev. Sci. Instrum. Vol. 55, No. 12 Dec 1984.
Efficiency formula: (1-exp(-k*delta/delta_max))/(1-exp(-k))
THEMIS ESA SWT ESA-20 UCB, Aug 6 - 8 2007
Detector Energy Efficiency 3
Ion efficiency corrected – work in progress:
Default ion efficiency produces a slope in the Ni/Ne ratio (right bottom).
Proposed ion efficiency eliminates this slope. Difference assumed to be due to fringing fields at the detector.
Default
Proposed
Energy (eV)
Energy (eV)
THEMIS ESA SWT ESA-21 UCB, Aug 6 - 8 2007
Detector Energy Efficiency 4
Electron efficiency: The proposed electron energy efficiency curve seems to produce more consistent electron-ion density ratios over a number of orbits. More investigation is needed, but difference appears to be due to secondary e- production in ESA.
Current e- efficiency Proposed e- efficiency
Energy (eV) Energy (eV)
THEMIS ESA SWT ESA-22 UCB, Aug 6 - 8 2007
ESA N,V Cross Calibration
Electron-Ion density ratios should agree at the ~5% level.
Ne should be less than Ni since Ni is calculated assuming H+.
Variations in calculated electron velocity are due to small density fluctuations during a s/c spin.
THEMIS ESA SWT ESA-23 UCB, Aug 6 - 8 2007
TBD Cross Calibrations
Relative Anode Calibrations.Absolute Sensitivity Calibrations.
Pressure Balance Tests.Corrections for Composition.
Cross Calibrations between spacecraft.Cross Calibrations with SSTs.-VxB vs E Cross Calibrations
THEMIS ESA SWT ESA-24 UCB, Aug 6 - 8 2007
ESA Data Problems
Early data had some table loading problems where counts were incorrectly mapped or ETC would freeze. Table loading bugs fixed ~April 27 and table freeze problem solved ~June 1.
THEMIS ESA SWT ESA-25 UCB, Aug 6 - 8 2007
ESA Data Problems
We occasionally still find bugs in the software, so if something looks wrong – it may be wrong . The below problem is under investigation.
THEMIS ESA SWT ESA-26 UCB, Aug 6 - 8 2007
EFI induced s/c charging
THEMIS ESA SWT ESA-27 UCB, Aug 6 - 8 2007
Cold Ions at Magnetopause
4 of 5 s/c observing cold ions at MP
Cold ion densities generally 1-2/cc, but can be in the 10-20/cc range (13 cases out of ~90)
Hot ion densities are ~0.1-0.3/cc.
tha
thb
thc
thd
the
THEMIS ESA SWT ESA-28 UCB, Aug 6 - 8 2007
Cold Ions at Magnetopause
Note the lack of cold ions except just inside the MP.
THEMIS ESA SWT ESA-29 UCB, Aug 6 - 8 2007
First Results – Cold Plasma
Cold ions become visible when the MP moves.
At times the He+ is observed with density about 1% of the H+ density.
To determine whether cold ions are plasmaspheric or conic outflow, check if velocity is along B or perpendicular to B.
THEMIS ESA SWT ESA-30 UCB, Aug 6 - 8 2007
First Results – Cold Plasma
Cold ions become visible when the MP moves with 3 min oscillations
THEMIS ESA SWT ESA-31 UCB, Aug 6 - 8 2007
Cold ions or conics?
Differences between electron and ion densities are often due to missed cold ions, but can also be due to ions with higher mass.
Conics often appear with a broader energy, are generally field aligned, and tend to be oxygen.