GALILEO
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Galileo Table of Contents Page.
The Galileo Energetic Particles Detector
Galileo EPD Handbook
Chapter 2. EPD Software
EPD SBAND Mission Software Requirements (continued)
Source: S. Jaskulek, various dates
Appendix B. EPD Accumulator Hardware Addresses
Table B-2. Map1 Accumulator Service Table
Rate Channels: | |||||||||||||||||||||
A1 | A2 | E1 | F2 | TP1 | TP2 | TO1 | TO2 | TS1 | STARTS | ||||||||||||
A0 | A3 | A4 | A5 | A6 | A7 | A8 | E0 | E2 | E3 | F0 | F1 | AS | TP3 | TA1 | TA2 | TO3 | TO4 | TS2 | TH1 | TACS | KTS |
F3 | B0 | B1 | B2 | DC0 | DC1 | DC2 | DC3 | BS | CS | DS | EB1 | EB2 | FB1 | FB2 | TS3 | ||||||
(terminator) | |||||||||||||||||||||
Resulting MAP1 load to memory: | |||||||||||||||||||||
10 | 01 | 08 | 0B | 52 | 51 | 4B | 4A | 43 | 4F | ||||||||||||
00 | 11 | 02 | 12 | 03 | 13 | 04 | 18 | 19 | 09 | 0A | 1A | 0C | 50 | 55 | 4D | 48 | 45 | 52 | 41 | 53 | 4E |
1B | 14 | 15 | 05 | 16 | 06 | 17 | 07 | 0D | 1C | 1D | 0E | 1E | 0F | 1F | 40 | ||||||
C1 |
Table B-3. MAP2 Accumulator Service Table
Rate Channels: | ||||||||||||||||||||||
A1 | A2 | A3 | A4 | A5 | E1 | F2 | TP1 | TP2 | TA1 | TO1 | TO2 | TO3 | TS1 | TS2 | STARTS | |||||||
A0 | A6 | A7 | A8 | E0 | E2 | E3 | F0 | F1 | F3 | B0 | B1 | B2 | BS | EB1 | FB1 | TP3 | TA2 | TO4 | TS3 | TH1 | TACS | KTS |
DC0 | DC1 | DC2 | DC3 | AS | CS | DS | EB2 | FB2 | ||||||||||||||
(terminator) | ||||||||||||||||||||||
Resulting MAP2 load to memory: | ||||||||||||||||||||||
10 | 01 | 11 | 02 | 12 | 08 | 0B | 52 | 51 | 55 | 4B | 4A | 48 | 43 | 42 | 4F | |||||||
00 | 03 | 13 | 04 | 18 | 19 | 09 | OA | 1A | 1B | 14 | 15 | 05 | 0D | OE | 0F | 50 | 4D | 45 | 40 | 41 | 53 | 4E |
16 | 06 | 17 | 07 | 0C | 1C | 1D | 1E | 1F | ||||||||||||||
C1 |
Table B-4. Record Mode Accumulator Service Table
Rate Channels: | |||||||||||||||||||||||||
BS | CS | DS | EB1 | EB2 | FB2 | TO2 | TO1 | CN0 | KTS | TO4 | TA1 | STARTS | |||||||||||||
JAS | KS | JBS | FB1 | TAC | TO3 | CH3 | CH4 | TH1 | CM3 | CM4 | CM5 | CN1 | CA1 | CA3 | CA4 | CM1 | DC3 | B0 | B1 | B2 | A8 | DC0 | DC1 | DC2 | TP1 |
TS1 | TA2 | CH1 | TS3 | TP2 | TP3 | TS2 | A6 | A7 | F2 | F3 | F1 | A3 | A4 | A5 | A2 | E2 | E3 | F0 | E0 | E1 | A0 | A1 | |||
Resulting Record Mode (C-Format) load to memory: | |||||||||||||||||||||||||
0D | 1C | 1D | OE | 1E | 1F | 4A | 4B | 47 | 4E | 45 | 55 | 4F | |||||||||||||
44 | 5F | 5E | 0F | 53 | 48 | 58 | 49 | 41 | 5B | 4C | 5C | 57 | 54 | 46 | 56 | 5A | 07 | 14 | 15 | 05 | 04 | 16 | 06 | 17 | 52 |
43 | 4D | 5D | 40 | 51 | 50 | 42 | 03 | 13 | 0B | 1B | 1A | 11 | 02 | 12 | 01 | 19 | 09 | 0A | 18 | 08 | 00 | 10 | |||
C1 |
Next: Appendix C. EPD Software Patch Hook Values
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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.
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.