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GALILEO

The Galileo Energetic Particles Detector

 

Galileo EPD Handbook

 

Chapter 2. EPD Software

 

New EPD Format and Implementation (continued)

Source: S. Jaskulek, May 11, 1993

 

TABLE 31. Rate Channel Assignments for EPD LEMMS Sensor; Channel Map 2

 

Energy Range Channel 16 sec.
+Cal
6 sec.
+Cal
Omni 
+Cal
Total
Channels
LEMMS (MeV)
0.022-0.042 keV A0   1   7
0.042-0.065 A1 1     17
0.065-0.120 A2 1     17
0.120-0.280 A3 1     17
0.280-0.515 A4 1     17
0.515-0.825 A5 1     17
0.825-1.68 A6   1   7
1.68-3.20 A7   1   7
3.50-12.4 (Z>=2) A8   1   7
 
0.015-0.029 E0   1   7
0.029-0.042 E1 1     17
0.042-0.055 E2   1   7
0.055-0.093 E3   1   7
 
0.093-0.188 F0   1   7
0.174-0.304 F1   1   7
0.304-0.527 F2 1     17
0.527-0.884 F3   1   7
 
3.20-10.1 (z=1) B0   1   7
1.5-10.5 (e-) B1   1   7
16.0-100 (z=2) B2   1   7
 
14.5-33.5 (z>=1) DC0     1 2
51-59 (z>=1) DC1     1 2
>=2.0 (e-) DC2     1 2
>=11 (e-) DC3     1 2
 
A singles AS     1 2
B singles BS   1   7
C singles CS     1 2
D singles DS     1 2
Background EB1   1   7
Background EB2     1 2
Background FB1   1   7
Background FB2     1 2
 
LEMMS Total   7 16 9 249

 

TABLE 32. Rate Channel Assignments for EPD CMS Sensor; Channel Map 2

 

Energy Range Channel 16 sec.
+Cal
6 sec.
+Cal
Omni 
+Cal
Total
Channels
TOF x E (MeV)
0.08-0.22 (H) TP1 1     17
0.22-0.54 (H) TP2 1     17
0.54-1.25 (H) TP3   1   7
0.027-0.155 (He) TA1 1     17
0.155-1.0 (He) TA2   1   7
0.012-0.026 (CNO) TO1 1     17
0.026-0.051 (CNO) TO2 1     17
0.051-0.112 (CNO) TO3 1     17
0.112-0.562 (CNO) TO4   1   7
0.016-0.030 (S) TS1 1     17
0.030-0.062 (S) TS2 1     17
0.062-0.31 (S) TS3   1   7
0.02-0.20 (Fe) TH1   1   7
TAC Singles TACS   1   7
KT Singles KTS   1   7
Start Singles STARTS 1     17
Delta E x E
0.19-0.49 (He) CA1        
0.49-0.68 (He) CA3        
0.68-1.4 (He) CA4        
0.16-0.55 (CNO) CM1        
0.55-1.1 (CNO) CM3        
1.1-2.9 (CNO) CM4        
2.9-10.7 (CNO) CM5        
1.0-2.2 (Na) CN0        
2.2-11.7 (Na) CN1        
0.22-0.33 (Fe) CH1        
0.33-0.67 (Fe) CH3        
0.67-1.3 (Fe) CH4        
1.3-15.0 (Fe) CH5        
Ja Singles JAS        
Jb Singles JBS        
K Singles KS        
 
CMS Total   9 7   202
Total Channels   16 23 9 451

 

TABLE 33. EPD Science Record Format vs. Format Number

 

Format Number Telem.
Alloc.,
bps
Accum.
Period
Cycles
Rate
Channels
Channel 
Map
CMS PHA
Events
Hskpg/Status
Bits
Telem. Out,
bps
1,2,3,4,5 5 6 356 1 12 40 5.08
6,8 10 3 356 1 12 40 10.16
7 15 2 451 1 12 40 15.24
9,10 20 2 451 2 24 40 20.03
11 30 1 356 1 12 40 30.48
12 40 1 451 2 24 40 40.07

 

TABLE 34. EPD Rate Channel Packet

 

Byte # Description
1
b0: Update Flag    (MSB)
1: new
0:old
b1, b2: Spin Quadrant
00: A
01: B
10: C
11: D
b3: New Spin
0: same
1: new
b4: MAP ID (0=MAP1, 1=MAP2)
b5-b7: Motor Position    (LSB)
000: Pos. 0
...
111: Pos. 7
2,3,4 Rate Channel 1 (24 bits)
5,6,7 Rate Channel 2 (24 bits)
8,9,10 Rate Channel 3 (24 bits)
... ...
143,144,145 Rate Channel 48 (24 bits)
146 HV Monitor Value
147-151 Housekeeping/Status
152-211 12 PHA events (20 bits each) and 30 bytes of filler or
24 PHA events (20 bits each)

 

Once the data is retrieved by the CDS, it must sequentially go through the 24-bit rate channel values and add them to the proper rate channel bins defined in the CDS memory. The addition algorithm for this may be fairly simple (see Appendix A (of the EPD Sband Mission Software Requirements document) for more details), but determining which bin to address is not so straightforward.  This task will be addressed in section 7 (of the Sband document).

 

The motor position, spin quadrant, and motor direction (in the science record status byte), all represent the values present during the quadrant that was just completed.  In other words, the motor and spin parameters match up with the rate channel data that is also present in the data for that minor frame. One could expect, therefore, that in a minor frame data packet in which the "new spin flag" is set, the spin quadrant will equal "D."

 

 

Next: EPD SBand Mission Software Requirements

 

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Updated 8/23/19, Cameron Crane

QUICK FACTS

Manufacturer: The Galileo Spacecraft was manufactured by the Jet Propulsion Laboratory, Messerschmitt-Bölkow-Blohm, General Electric, and the Hughes Aircraft Company.

Mission Duration: Galileo was planned to have a mission duration of around 8 years, but was kept in operation for 13 years, 11 months, and 3 days, until it was destroyed in a controlled impact with Jupiter on September 21, 2003.

Destination: Galileo's destination was Jupiter and its moons, which it orbitted for 7 years, 9 months, and 13 days.