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Merge branch 'master-version-21' into pi-sensors-auto

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pi-sensors-auto
Alan Johnston 4 weeks ago committed by GitHub
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gpl.txt → LICENSE
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README.md
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# CubeSatSim
The CubeSat Simulator https://github.com/alanbjohnston/CubeSatSim/wiki is a low cost satellite emulator that runs on solar panels and batteries, transmits UHF radio telemetry, has a 3D printed frame, and can be extended by additional sensors and modules. This project is sponsored by the not-for-profit [Radio Amateur Satellite Corporation, AMSAT®](https://amsat.org).
The CubeSat Simulator https://github.com/alanbjohnston/CubeSatSim/wiki is a low cost satellite emulator that runs on solar panels and batteries, transmits UHF radio telemetry, has a 3D printed frame, and can be extended by additional sensors and modules. This project is sponsored by the not-for-profit [Radio Amateur Satellite Corporation, AMSAT®](https://amsat.org) https://CubeSatSim.org
<img width="500" alt="CubeSatSim v2" src="https://CubeSatSim.org/v2/cubesatsim%20v2%20complete.png">
The three custom PCBs are the Main, Battery and Solar boards. Information including schematics and gerbers is in https://CubeSatSim.org/hardware
<img width="200" alt="cubesatsim-main-v2 0 1_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/b3178fc979a88031f06365590ba47a358158fd73/hardware/v2.0/cubesatsim-main-v2.0_top.png"> <img width="200" alt="cubesatsim-battery-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/b3178fc979a88031f06365590ba47a358158fd73/hardware/v2.0/cubesatsim-battery-v2.0.1_top.png"> <img width="200" alt="cubesatsim-solar-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/b3178fc979a88031f06365590ba47a358158fd73/hardware/v2.0/cubesatsim-solar-v2.0.1_top.png">
<img width="200" alt="cubesatsim-main-v2 0 1_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/628fd65edbb01fb772a9f223605d969a0aad14bd/hardware/v2.1/cubesatsim-main-v2.1.0_top.png"> <img width="200" alt="cubesatsim-battery-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/4d079b486116180071c4dbf64ae2464518a63bdd/hardware/v2.1/cubesatsim-battery-v2.1.0_top.png"> <img width="200" alt="cubesatsim-solar-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/c904c66d7c8fb44a3d088d0cbebf24903cf3572c/hardware/v2.1/cubesatsim-solar-v2.1.0_top.png">
For information about the AMSAT STEM education program based on the CubeSatSim, see https://CubeSatSim.org/EducatorsGuide
For STEM activities to do with the CubeSatSim, see the https://CubeSatSim.org/ActivityGuides
There are several hardware versions and software branches to go with them - see below for information.

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config
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@ -1799,9 +1799,10 @@ elif [ "$1" = "-h" ]; then
echo " -R Change the Commands Count in the file command_count.txt"
echo " -B Change Safe Mode (battery saver mode) manually"
echo " -q Change the Squelch setting for command receiver"
echo " -Q Read the current Squelch for 10 seconds"
echo " -F Change the RX and TX frequency"
echo " -H Change the Balloon (HAB) mode"
echo " -p Display payload sensor data"
echo " -p Display payload sensor data for 3 seconds"
echo " -v Display voltage and current data"
echo " -P Change the PL (Private Line) CTCSS/CDCSS codes for RX and TX"
echo " -A Transmit APRS control packets to control another CubeSatSim"

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Here is the source for the 2U Connector part: https://cad.onshape.com/documents/eecb39d3cd81220d3a56ce06/v/fdc9aca356206986ef6440e6/e/f881e9547bb3cd4fd653d041
You can export it in other formats
You will also need two additional frame sides
Here's how to upgrade a 1U CubeSatSim https://github.com/alanbjohnston/CubeSatSim/wiki/Upgrading-to-2U

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@ -9,3 +9,5 @@ The source is availale at:
https://cad.onshape.com/documents/ba47819ff100597297d1d967/w/f19409ec7cd5459afb429cb9/e/a0e0cc37dee6fb879c4bcc2b
https://cad.onshape.com/documents/1515e31c7fa5f6258ef39ae7/w/36f6069826ee0c0263f8d85e/e/2b7801717a8e1af3df455057
https://cad.onshape.com/documents/188300bd4469521b14597507/w/546e1730182c1520c46b050d/e/ceef7084a00eb9b26c486bb6
To make a 2U frame, also print the 2U connector part in https://github.com/alanbjohnston/CubeSatSim/tree/master/hardware/frame/v2.0/2u and print two additional side parts. See https://github.com/alanbjohnston/CubeSatSim/wiki/Upgrading-to-2U for more information.

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hardware/lite/v2/README.md
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Here is information about the CubeSatSim Lite v2 hardware
cubesatsim-Lite_2.0.1_gerbers.zip -- All gerber files used to fabricate PCBs
cubesatsim-Lite_2.0.1_schematic.pdf -- Schematic
cubesatsim-Lite_2.0.1.mnt -- SMD file
cubesatsim-lLite_2.0.1_pcb.png -- image of board
cubesatsim-Lite_2.0.1_bom.csv.txt -- Bill of Materials (BOM)
For more information see https://github.com/alanbjohnston/CubeSatSim/wiki/CubeSatSim-Lite

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JP1 44.68 53.87 0 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP2 23.14 59.97 0 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP3 21.74 56.03 270 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP6 33.99 59.61 0 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP7 16.00 63.09 90 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK

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C1 8.36 61.93 0 18pF C0603
C2 10.03 61.90 0 16pF C0603
C3 56.06 58.32 90 18pF C0603
C4 55.47 62.84 270 16pF C0603
C7 49.23 56.57 0 DNI/47uF C0603
C8 50.47 47.68 270 DNI/100nF C0603
E1 3.63 53.23 270 ANT-916-CHP-T XDCR_ANT-916-CHP-T
E2 61.39 53.21 270 ANT-916-CHP-T XDCR_ANT-916-CHP-T
J1 32.55 66.61 0 CONN_20X2 2X20
J13 9.25 45.02 180 SJ1-2503A CONN_SJ1-2503A
J14 55.07 45.08 180 SJ1-2503A CONN_SJ1-2503A
L1 9.22 59.44 180 13nH L0603
L2 56.24 60.55 270 13nH L0603
LED5 19.08 42.09 270 GREEN LED-0603
LED6 43.94 41.91 270 BLUE LED-0603
R2 46.63 62.48 180 DNI/1k R0603
R4 51.18 62.51 180 DNI/1k R0603
R10 12.70 41.91 90 DNI/1k 0603-RES
R11 51.66 41.91 90 DNI/100 0603-RES
R16 13.79 60.22 0 DNI/68 R0805
R17 18.44 60.33 270 DNI/180 R0603
R18 26.67 60.22 180 DNI/68 R0805
R21 48.90 51.23 0 DNI/100 R0603
R22 55.14 51.99 0 DNI/220 R0603
S2 7.80 51.82 90 DTSM-6 DTSM-6
U6 32.94 51.75 270 SR105U SR_FRS_0W5

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"Part";"Value";"Device";"Package";"Description";"";
"C1";"18pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C2";"16pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C3";"18pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C4";"16pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C5";"47uF";"CAPPTH";"CAP-PTH-SMALL";"Capacitor";"";
"C6";"100nF";"CAPPTH";"CAP-PTH-SMALL";"Capacitor";"";
"C7";"DNI/47uF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C8";"DNI/100nF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"E1";"ANT-916-CHP-T";"ANT-916-CHP-T";"XDCR_ANT-916-CHP-T";"868MHz ISM, LoRa, Sensor Networks, SigFox Chip RF Antenna 863MHz ~ 873MHz 0.5dBi Solder Surface Mount Check prices";"";
"E2";"ANT-916-CHP-T";"ANT-916-CHP-T";"XDCR_ANT-916-CHP-T";"868MHz ISM, LoRa, Sensor Networks, SigFox Chip RF Antenna 863MHz ~ 873MHz 0.5dBi Solder Surface Mount Check prices";"";
"J1";"CONN_20X2";"CONN_20X2";"2X20";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J2";"";"CONN_021X02_NO_SILK";"1X02_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J6";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"J10";"DNI/Sparkfun QWIIC Breakout";"CONN_041X04_NO_SILK";"1X04_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J12";"DNI/1x4 pin header";"CONN_041X04_NO_SILK";"1X04_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J13";"SJ1-2503A";"SJ1-2503A";"CONN_SJ1-2503A";"";"";
"J14";"SJ1-2503A";"SJ1-2503A";"CONN_SJ1-2503A";"";"";
"J15";"";"CONN_06NO_SILK_NO_POP";"1X06_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP1";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP2";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP3";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP6";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP7";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"L1";"13nH";"SMD-FERRITE-CHIP-120-OHM-500MA(0603)";"L0603";"303030001";"";
"L2";"13nH";"SMD-FERRITE-CHIP-120-OHM-500MA(0603)";"L0603";"303030001";"";
"LED3";"Green 5mm";"LED3MM";"LED3MM";"LED";"";
"LED4";"Blue 5mm";"LED3MM";"LED3MM";"LED";"";
"LED5";"GREEN";"LED-GREEN0603";"LED-0603";"Green SMD LED";"";
"LED6";"BLUE";"LED-BLUE0603";"LED-0603";"Blue SMD LED";"";
"R1";"1K";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R2";"DNI/1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R3";"1K";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R4";"DNI/1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R7";"1k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R8";"DNI/100";"RESISTOR0603";"0603-RES";"Resistor";"";
"R10";"DNI/1k";"RESISTOR0603-RES";"0603-RES";"Resistor";"";
"R11";"100";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R13";"68";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R14";"180";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R15";"68";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R16";"DNI/68";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R17";"DNI/180";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R18";"DNI/68";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R19";"100";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R20";"220";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R21";"DNI/100";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R22";"DNI/220";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"S1";"RA-SPST";"RA-SPST";"RA-SPST";"";"";
"S2";"DTSM-6";"DTSM-6";"DTSM-6";"";"";
"U1";"SR105U";"SR_FRS_0W5";"SR_FRS_0W5";"";"";
"X2";"SMA-VERT";"SMA-VERT";"SMA-VERT";"";"";
"X3";"SMA-VERT";"SMA-VERT";"SMA-VERT";"";"";

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@ -10,4 +10,4 @@ cubesatsim-lite-0.5_pcb.png -- image of board
cubesatsim-lite-0.5.csv.txt -- Bill of Materials (BOM)
For more information see https://github.com/alanbjohnston/CubeSatSim/wiki/CubeSatSim-Lite
For more information see https://github.com/alanbjohnston/CubeSatSim/wiki/CubeSatSim-Lite-Beta-vB5

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hardware/v2.1/cubesatsim-battery-v2.1.0_bom.csv.txt
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"Part";"Value";"Device";"Package";"Description";"";
"BT1";"1024";"1024";"BAT_1024";"Check availability";"";
"BT2";"1012";"1012";"BAT_1012";"Check availability";"";
"C1";"DNI/0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"F1";"PTC";"PTCPTH";"PTC";"Resettable Fuse PTC";"";
"J1";"CONN_20X2";"CONN_20X2";"2X20";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP1";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP2";"";"CONN_01";"1X01";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP3";"";"CONN_01";"1X01";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP4";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP5";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP6";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP7";"";"CONN_01";"1X01";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP8";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP10";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP11";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP13";"";"CONN_01";"1X01";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP14";"";"CONN_01";"1X01";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"R1";"DNI/R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R2";"10k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R3";"10k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"U1";"INA219 purple board";"INA219";"INA219";"";"";
"U2";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";

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D1 63.55 60.58 0 BYW27-400 D-2.5
D2 72.01 10.49 0 1N5817 D-2.5
D3 66.45 10.62 180 1N4148 D-2.5
D8 59.31 7.52 270 DNI/5V1 Zener 1W ZDIO-2.5
D10 77.50 10.46 0 1N5817 D-2.5
JP1 72.17 8.66 180 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP2 24.73 60.99 0 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP3 16.08 58.12 270 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP4 59.36 56.39 180 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP5 75.08 56.48 270 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP6 26.21 35.94 180 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
JP7 15.95 62.24 90 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP8 47.28 30.91 180 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP9 44.21 61.82 180 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP10 63.61 56.54 0 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
JP11 14.63 52.17 180 JUMPER-SMT_2_NC_TRACE_SILK SMT-JUMPER_2_NC_TRACE_SILK
U7 36.42 49.89 0 DRA818V DORJI_DRA818V
X1 71.86 61.21 270 SC1464-ND PG203J

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C1 18.75 76.02 270 18pF C0603
C2 18.69 71.88 270 16pF C0603
C3 16.38 10.11 180 18pF C0603
C4 20.68 10.16 180 16pF C0603
C7 55.60 56.62 0 DNI/47uF C0603
C8 59.00 47.55 270 DNI/100nF C0603
C10 66.83 3.91 270 DNI/100nF C0603
D5 63.42 62.53 0 DNI/1N4007FL SOD-123FL
D6 72.16 8.69 180 DNI/B5817WS SOD-323F
D7 66.47 8.84 0 DNI/4148WS SOD-323F
E1 6.80 76.35 180 ANT-916-CHP-T XDCR_ANT-916-CHP-T
E2 19.18 3.81 0 ANT-916-CHP-T XDCR_ANT-916-CHP-T
F2 63.68 57.18 180 DNI/MF-FSML100/8-2 0603
J1 32.55 66.61 0 CONN_20X2 2X20
J8 36.17 72.01 0 Sparkfun USB-C Breakout 1X06_NO_SILK
J9 36.35 74.15 180 DNI/USB4105-GF-A or GT-USB-7010B USB-C-16P-2LAYER-PADS
J13 8.92 31.68 0 SJ1-2503A CONN_SJ1-2503A
J14 15.95 31.76 0 SJ1-2503A CONN_SJ1-2503A
L1 16.76 73.94 90 13nH L0603
L2 18.49 12.17 180 13nH L0603
R2 54.00 62.26 0 DNI/1k R0603
R4 58.39 62.26 180 DNI/1k R0603
R5 29.46 76.45 180 DNI/5.1k R0603
R6 43.18 76.48 0 DNI/5.1k R0603
R10 64.26 72.06 0 DNI/1k R0603
R11 24.16 72.06 0 DNI/100 R0603
R12 47.55 72.42 0 DNI/220 R0603
R16 20.07 60.05 0 DNI/68 R0805
R17 24.71 60.15 270 DNI/180 R0603
R18 32.94 60.20 180 DNI/68 R0805
R21 55.42 51.26 0 DNI/100 R0603
R22 59.33 44.63 0 DNI/220 R0603
R25 67.59 40.77 90 DNI/4.7k R0603
R26 76.53 40.79 90 DNI/4.7k R0603
R28 61.98 8.81 0 DNI/10k R0603
R31 3.86 44.37 0 DNI/220 R0603
R32 3.40 60.55 180 DNI/1k R0603
U1 54.36 27.48 270 Raspberry Pi Pico PICO-PKG-NO_DEBUG
U6 39.24 51.22 270 SR105U SR_FRS_0W5

94
hardware/v2.1/cubesatsim-main-v2.1.0_bom.csv.txt
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"Part";"Value";"Device";"Package";"Description";"";
"C1";"18pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C2";"16pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C3";"18pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C4";"16pF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C5";"47uF";"CAPPTH";"CAP-PTH-SMALL";"Capacitor";"";
"C6";"100nF";"CAPPTH";"CAP-PTH-SMALL";"Capacitor";"";
"C7";"DNI/47uF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C8";"DNI/100nF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"C9";"100nF";"CAPPTH";"CAP-PTH-SMALL";"Capacitor";"";
"C10";"DNI/100nF";"CERAMIC-10PF-50V-5%-NPO(0603)";"C0603";"302010097";"";
"D1";"BYW27-400";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D2";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D3";"1N4148";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D5";"DNI/1N4007FL";"DIODE_SOD-123FL";"SOD-123FL";"Diode";"";
"D6";"DNI/B5817WS";"DIODESOD-323F";"SOD-323F";"Diode";"";
"D7";"DNI/4148WS";"DIODESOD-323F";"SOD-323F";"Diode";"";
"D8";"DNI/5V1 Zener 1W";"ZENER-DIODEZD-2.5";"ZDIO-2.5";"Z-Diode";"";
"D10";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"E1";"ANT-916-CHP-T";"ANT-916-CHP-T";"XDCR_ANT-916-CHP-T";"868MHz ISM, LoRa, Sensor Networks, SigFox Chip RF Antenna 863MHz ~ 873MHz 0.5dBi Solder Surface Mount Check prices";"";
"E2";"ANT-916-CHP-T";"ANT-916-CHP-T";"XDCR_ANT-916-CHP-T";"868MHz ISM, LoRa, Sensor Networks, SigFox Chip RF Antenna 863MHz ~ 873MHz 0.5dBi Solder Surface Mount Check prices";"";
"F1";"RHEF100-2";"PTCPTH";"PTC";"Resettable Fuse PTC";"";
"F2";"DNI/MF-FSML100/8-2";"PTC0603";"0603";"Resettable Fuse PTC";"";
"J1";"CONN_20X2";"CONN_20X2";"2X20";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J4";"MPU6050";"M08NO_SILK_FEMALE_PTH";"1X08_NO_SILK@1";"Header 8";"";
"J5";"BME280";"M04NO_SILK_ALL_ROUND";"1X04_NO_SILK_ALL_ROUND";"Header 4";"";
"J6";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"J7";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"J8";"Sparkfun USB-C Breakout";"CONN_06NO_SILK_FEMALE_PTH";"1X06_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J9";"DNI/USB4105-GF-A or GT-USB-7010B";"USB_C_2-LAYER_PADS";"USB-C-16P-2LAYER-PADS";"USB Type C 16Pin Connector";"";
"J10";"DNI/Sparkfun QWIIC Breakout";"CONN_041X04_NO_SILK";"1X04_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J12";"DNI/1x4 pin header";"CONN_041X04_NO_SILK";"1X04_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J13";"SJ1-2503A";"SJ1-2503A";"CONN_SJ1-2503A";"";"";
"J14";"SJ1-2503A";"SJ1-2503A";"CONN_SJ1-2503A";"";"";
"J15";"";"CONN_06NO_SILK_NO_POP";"1X06_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP1";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP2";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP3";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP4";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP5";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP6";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP7";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP8";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP9";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP10";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP11";"JUMPER-SMT_2_NC_TRACE_SILK";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"L1";"13nH";"SMD-FERRITE-CHIP-120-OHM-500MA(0603)";"L0603";"303030001";"";
"L2";"13nH";"SMD-FERRITE-CHIP-120-OHM-500MA(0603)";"L0603";"303030001";"";
"LED1";"White 5mm";"LED3MM";"LED3MM";"LED";"";
"LED2";"Yellow 5mm";"LED3MM";"LED3MM";"LED";"";
"LED3";"Green 5mm";"LED3MM";"LED3MM";"LED";"";
"LED4";"Blue 5mm";"LED3MM";"LED3MM";"LED";"";
"LED5";"Red 5mm";"LED3MM";"LED3MM";"LED";"";
"R1";"1K";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R2";"DNI/1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R3";"1K";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R4";"DNI/1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R5";"DNI/5.1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R6";"DNI/5.1k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R7";"1k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R8";"100";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R9";"220";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R10";"DNI/1k";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R11";"DNI/100";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R12";"DNI/220";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R13";"68";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R14";"180";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R15";"68";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R16";"DNI/68";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R17";"DNI/180";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R18";"DNI/68";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R19";"100";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R20";"220";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R21";"DNI/100";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R22";"DNI/220";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R23";"4.7k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R24";"4.7k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R25";"DNI/4.7k";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R26";"DNI/4.7k";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R27";"10K";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R28";"DNI/10k";"R-EU_R0603";"R0603";"RESISTOR, European symbol";"";
"R29";"220";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R30";"1k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R31";"DNI/220";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R32";"DNI/1k";"SMD-RES-1.2K-1%-1/10W(0603)";"R0603";"301010206";"";
"R33";"DNI/4.7k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"R34";"DNI/4.7k";"RESISTORPTH-1/4W-VERT";"AXIAL-0.1";"Resistor";"";
"S1";"RA-SPST";"RA-SPST";"RA-SPST";"";"";
"U1";"Raspberry Pi Pico";"RASPBERRY_PICO-NO_DEBUG";"PICO-PKG-NO_DEBUG";"";"";
"U6";"SR105U";"SR_FRS_0W5";"SR_FRS_0W5";"";"";
"U7";"DRA818V";"DRA818V";"DORJI_DRA818V";"Check availability";"";
"X1";"SC1464-ND";"PG203J";"PG203J";"MIC/HEADPHONE JACK";"";
"X2";"SMA-VERT";"SMA-VERT";"SMA-VERT";"";"";
"X3";"SMA-VERT";"SMA-VERT";"SMA-VERT";"";"";

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hardware/v2.1/cubesatsim-solar-v2.1.0.mnb
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D1 37.58 48.87 180 1N5817 D-2.5
D2 37.66 42.52 180 1N5817 D-2.5
D3 37.50 35.95 180 1N5817 D-2.5
D4 42.94 48.94 0 1N5817 D-2.5
D5 42.94 42.42 0 1N5817 D-2.5
D6 42.79 36.07 0 1N5817 D-2.5
JP9 1.35 57.85 270 VDD-EN SMT-JUMPER_2_NC_TRACE_SILK
JP18 24.75 62.60 180 JUMPER-SMT_2_NO_SILK SMT-JUMPER_2_NO_SILK
U5 71.44 19.89 90 INA219 purple board INA219
U6 8.59 48.95 270 INA219 purple board INA219
U7 8.46 20.29 270 INA219 purple board INA219
U8 71.36 48.21 90 INA219 purple board INA219

29
hardware/v2.1/cubesatsim-solar-v2.1.0.mnt
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C2 17.54 37.77 0 0.1µF 0603
C3 17.41 21.59 0 0.1µF 0603
C4 17.56 11.14 0 0.1µF 0603
C5 17.53 50.09 0 0.1µF 0603
C6 61.82 19.28 180 0.1µF 0603
C7 62.06 38.65 180 0.1µF 0603
D7 42.95 38.00 0 1A/23V/620mV SOD-323
D8 43.08 44.40 0 1A/23V/620mV SOD-323
D9 43.43 50.75 0 1A/23V/620mV SOD-323
D10 37.72 50.67 180 1A/23V/620mV SOD-323
D11 37.62 37.92 180 1A/23V/620mV SOD-323
D12 37.90 44.40 180 1A/23V/620mV SOD-323
J1 32.55 66.61 0 CONN_20X2 2X20
R1 11.58 43.79 270 R100 R0805
R2 11.68 15.01 270 R100 R0805
R5 24.84 14.99 90 R100 R0805
R6 24.87 43.84 270 R100 R0805
R9 68.07 25.10 90 R100 R0805
R10 68.19 53.47 90 R100 R0805
R11 42.91 62.08 0 DNI-4.7k R0603
R12 36.87 62.08 0 DNI-4.7k R0603
U2 17.53 44.60 0 INA219AIDR D0008A_N
U3 48.65 48.20 90 INA219 purple board INA219
U4 30.84 48.90 270 INA219 purple board INA219
U10 17.45 26.75 0 INA219AIDR D0008A_N
U11 17.68 16.66 0 INA219AIDR D0008A_N
U12 17.50 55.36 0 INA219AIDR D0008A_N
U13 61.72 24.82 0 INA219AIDR D0008A_N
U14 61.58 44.20 0 INA219AIDR D0008A_N

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hardware/v2.1/cubesatsim-solar-v2.1.0_bom.csv.txt
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"Part";"Value";"Device";"Package";"Description";"";
"C2";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"C3";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"C4";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"C5";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"C6";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"C7";"0.1µF";"CAP_CERAMIC0603";"0603";"Ceramic Capacitors";"";
"D1";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D2";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D3";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D4";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D5";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D6";"1N5817";"DIODE-D-2.5";"D-2.5";"DIODE";"";
"D7";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"D8";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"D9";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"D10";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"D11";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"D12";"1A/23V/620mV";"DIODE-SCHOTTKY-BAT20J";"SOD-323";"Schottky diode";"";
"J1";"CONN_20X2";"CONN_20X2";"2X20";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"J5";"DNI/Sparkfun QWIIC Breakout";"CONN_041X04_NO_SILK";"1X04_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP1";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP2";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP3";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP4";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP5";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP6";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP7";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP8";"Micro JST";"CONN_021X02_NO_SILK";"1X02_NO_SILK";"Multi connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP9";"VDD-EN";"JUMPER-SMT_2_NC_TRACE_SILK";"SMT-JUMPER_2_NC_TRACE_SILK";"Normally closed trace jumper";"";
"JP10";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP11";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP12";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP13";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP14";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP15";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP16";"";"CONN_01PTH_NO_SILK_YES_STOP";"1X01_NO_SILK";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP17";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP18";"JUMPER-SMT_2_NO_SILK";"JUMPER-SMT_2_NO_SILK";"SMT-JUMPER_2_NO_SILK";"Normally open jumper";"";
"JP19";"";"CONN_01PTH_NO_SILK_YES_STOP";"1X01_NO_SILK";"Single connection point. Often used as Generic Header-pin footprint for 0.1 inch spaced/style header connections";"";
"JP20";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP21";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP22";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP23";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP24";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP25";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"JP26";"Micro JST";"M02JST-PTH-VERT";"JST-2-PTH-VERT";"Standard 2-pin 0.1" header. Use with";"";
"R1";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R2";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R3";"4.7k";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R4";"4.7k";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R5";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R6";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R7";"DNI-4.7k";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R8";"DNI-4.7k";"RESISTORPTH-1/4W-VERT-KIT";"AXIAL-0.1EZ";"Resistor";"";
"R9";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R10";"R100";"R-US_R0805";"R0805";"RESISTOR, American symbol";"";
"R11";"DNI-4.7k";"R-US_R0603";"R0603";"RESISTOR, American symbol";"";
"R12";"DNI-4.7k";"R-US_R0603";"R0603";"RESISTOR, American symbol";"";
"U2";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";
"U3";"INA219 purple board";"INA219";"INA219";"";"";
"U4";"INA219 purple board";"INA219";"INA219";"";"";
"U5";"INA219 purple board";"INA219";"INA219";"";"";
"U6";"INA219 purple board";"INA219";"INA219";"";"";
"U7";"INA219 purple board";"INA219";"INA219";"";"";
"U8";"INA219 purple board";"INA219";"INA219";"";"";
"U10";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";
"U11";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";
"U12";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";
"U13";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";
"U14";"INA219AIDR";"INA219AIDR";"D0008A_N";"";"";

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33
hardware/v2.1/readme.md
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@ -0,0 +1,33 @@
<img width="200" alt="cubesatsim-main-v2 0 1_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/628fd65edbb01fb772a9f223605d969a0aad14bd/hardware/v2.1/cubesatsim-main-v2.1.0_top.png"> <img width="200" alt="cubesatsim-battery-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/4d079b486116180071c4dbf64ae2464518a63bdd/hardware/v2.1/cubesatsim-battery-v2.1.0_top.png"> <img width="200" alt="cubesatsim-solar-v2 0_top" src="https://github.com/alanbjohnston/CubeSatSim/blob/c904c66d7c8fb44a3d088d0cbebf24903cf3572c/hardware/v2.1/cubesatsim-solar-v2.1.0_top.png">
Here is information about the CubeSatSim PCBs, version v2.1
There are 3 boards: Main, Solar, and Battery
Here's what the files are:
*_gerbers.zip -- All gerber files used to fabricate PCBs along with .TXT drill file
*_schematic.pdf -- Schematic
*_pcb.png -- View of board
*_pour.png -- View of board with fill
*_top.png -- Top view of PCB generated by gerbers
*_bottom.png -- Bottom view of PCB generated by gerbers
*.mnt -- top SMD component placement data
*.mnb -- bottom SMD component placement data
*_bom.csv.txt -- Bill of Materials in CSV format
I use PCBWay to fabricate PCBs https://pcbway.com
Here is the bill of materials: https://CubeSatSim.org/bom
Wiki instructions: https://github.com/alanbjohnston/CubeSatSim/wiki/

2
install
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@ -192,6 +192,8 @@ sudo raspi-config nonint do_legacy 0
sudo sed -i 's/console=tty1 r/console=tty1 maxcpus=1 r/g' /boot/cmdline.txt # single core if Pi Zero 2
sudo sed -i 's/maxcpus=2/maxcpus=1/g' /boot/cmdline.txt # single core if Pi Zero 2
sudo sed -i 's/#dtparam=i2c_arm=on/dtparam=i2c_arm=on/g' /boot/config.txt
if [[ $(grep 'dtoverlay=i2c-gpio,bus=3,i2c_gpio_delay_us=1,i2c_gpio_sda=23,i2c_gpio_scl=24' /boot/config.txt) ]]; then

126
main.c
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@ -1642,40 +1642,40 @@ void get_tlm_fox() {
encodeA(b_max, 39 + head_offset, (int)(other_max[IHU_TEMP] * 10 + 0.5));
encodeB(b_max, 31 + head_offset, ((int)(other_max[SPIN] * 10)) + 2048);
if (sensor_min[TEMP] != 1000.0) // make sure values are valid
{
encodeB(b_max, 4 + head_offset, (int)(sensor_max[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b_max, 6 + head_offset, (int)(sensor_max[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b_max, 7 + head_offset, (int)(sensor_max[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
encodeB(b_max, 40 + head_offset, (int)(sensor_max[GYRO_X] + 0.5) + 2048);
encodeA(b_max, 42 + head_offset, (int)(sensor_max[GYRO_Y] + 0.5) + 2048);
encodeB(b_max, 43 + head_offset, (int)(sensor_max[GYRO_Z] + 0.5) + 2048);
encodeA(b_max, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure
encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] * 10.0 + 0.5)); // Altitude
// encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1] * 10 + 0.5) + 2048);
encodeB(b_max, 10 + head_offset, (int)(sensor_max[TEMP] * 10 + 0.5));
encodeA(b_max, 45 + head_offset, (int)(sensor_max[HUMI] * 10 + 0.5));
encodeA(b_max, 48 + head_offset, (int)(sensor_max[DTEMP] * 10 + 0.5) + 2048);
encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1]));
encodeA(b_max, 0 + head_offset, (int)(sensor_max[XS2]));
encodeB(b_max, 1 + head_offset, (int)(sensor_max[XS3]));
}
else
{
encodeB(b_max, 4 + head_offset, 2048); // 0
encodeA(b_max, 6 + head_offset, 2048); // 0
encodeB(b_max, 7 + head_offset, 2048); // 0
encodeB(b_max, 40 + head_offset, 2048);
encodeA(b_max, 42 + head_offset, 2048);
encodeB(b_max, 43 + head_offset, 2048);
encodeA(b_max, 48 + head_offset, 2048);
// encodeB(b_max, 49 + head_offset, 2048);
}
if (sensor_min[TEMP] != 1000.0) // make sure values are valid
{
encodeB(b_max, 4 + head_offset, (int)(sensor_max[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b_max, 6 + head_offset, (int)(sensor_max[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b_max, 7 + head_offset, (int)(sensor_max[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
encodeA(b_max, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure
encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] / 10.0 + 0.5)); // Altitude
encodeB(b_max, 40 + head_offset, (int)(sensor_max[GYRO_X] + 0.5) + 2048);
encodeA(b_max, 42 + head_offset, (int)(sensor_max[GYRO_Y] + 0.5) + 2048);
encodeB(b_max, 43 + head_offset, (int)(sensor_max[GYRO_Z] + 0.5) + 2048);
encodeA(b_max, 48 + head_offset, (int)(sensor_max[DTEMP] * 10 + 0.5) + 2048);
// encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1] * 10 + 0.5) + 2048);
encodeB(b_max, 10 + head_offset, (int)(sensor_max[TEMP] * 10 + 0.5));
encodeA(b_max, 45 + head_offset, (int)(sensor_max[HUMI] * 10 + 0.5));
encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1]));
encodeA(b_max, 0 + head_offset, (int)(sensor_max[XS2]));
encodeB(b_max, 1 + head_offset, (int)(sensor_max[XS3]));
}
else
{
encodeB(b_max, 4 + head_offset, 2048); // 0
encodeA(b_max, 6 + head_offset, 2048); // 0
encodeB(b_max, 7 + head_offset, 2048); // 0
encodeB(b_max, 40 + head_offset, 2048);
encodeA(b_max, 42 + head_offset, 2048);
encodeB(b_max, 43 + head_offset, 2048);
encodeA(b_max, 48 + head_offset, 2048);
// encodeB(b_max, 49 + head_offset, 2048);
}
encodeA(b_min, 12 + head_offset, (int)(voltage_min[map[PLUS_X]] * 100));
encodeB(b_min, 13 + head_offset, (int)(voltage_min[map[PLUS_Y]] * 100));
encodeA(b_min, 15 + head_offset, (int)(voltage_min[map[PLUS_Z]] * 100));
@ -1698,22 +1698,48 @@ void get_tlm_fox() {
encodeB(b_min, 31 + head_offset, ((int)(other_min[SPIN] * 10)) + 2048);
encodeB(b_min, 37 + head_offset, (int)(other_min[RSSI] + 0.5) + 2048);
encodeA(b_min, 39 + head_offset, (int)(other_min[IHU_TEMP] * 10 + 0.5));
if (sensor_min[TEMP] != 1000.0) // make sure values are valid
{
encodeB(b_min, 4 + head_offset, (int)(sensor_min[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b_min, 6 + head_offset, (int)(sensor_min[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b_min, 7 + head_offset, (int)(sensor_min[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
encodeA(b_min, 33 + head_offset, (int)(sensor_min[PRES] + 0.5)); // Pressure
encodeB(b_min, 34 + head_offset, (int)(sensor_min[ALT] / 10.0 + 0.5)); // Altitude
encodeB(b_min, 40 + head_offset, (int)(sensor_min[GYRO_X] + 0.5) + 2048);
encodeA(b_min, 42 + head_offset, (int)(sensor_min[GYRO_Y] + 0.5) + 2048);
encodeB(b_min, 43 + head_offset, (int)(sensor_min[GYRO_Z] + 0.5) + 2048);
encodeA(b_min, 48 + head_offset, (int)(sensor_min[DTEMP] * 10 + 0.5) + 2048);
// encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1] * 10 + 0.5) + 2048);
encodeB(b_min, 10 + head_offset, (int)(sensor_min[TEMP] * 10 + 0.5));
encodeA(b_min, 45 + head_offset, (int)(sensor_min[HUMI] * 10 + 0.5));
encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1]));
encodeA(b_min, 0 + head_offset, (int)(sensor_min[XS2]));
encodeB(b_min, 1 + head_offset, (int)(sensor_min[XS3]));
}
else
{
encodeB(b_min, 4 + head_offset, 2048); // 0
encodeA(b_min, 6 + head_offset, 2048); // 0
encodeB(b_min, 7 + head_offset, 2048); // 0
encodeB(b_min, 40 + head_offset, 2048);
encodeA(b_min, 42 + head_offset, 2048);
encodeB(b_min, 43 + head_offset, 2048);
encodeA(b_min, 48 + head_offset, 2048);
// encodeB(b_min, 49 + head_offset, 2048);
}
}
encodeA(b, 30 + head_offset, BAT2Voltage);
if (sensor_min[TEMP] != 1000.0) // make sure values are valid
{
encodeB(b_min, 4 + head_offset, (int)(sensor_min[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b_min, 6 + head_offset, (int)(sensor_min[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b_min, 7 + head_offset, (int)(sensor_min[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
encodeB(b_min, 40 + head_offset, (int)(sensor_min[GYRO_X] + 0.5) + 2048);
encodeA(b_min, 42 + head_offset, (int)(sensor_min[GYRO_Y] + 0.5) + 2048);
encodeB(b_min, 43 + head_offset, (int)(sensor_min[GYRO_Z] + 0.5) + 2048);
encodeA(b_min, 33 + head_offset, (int)(sensor_min[PRES] + 0.5)); // Pressure
encodeB(b_min, 34 + head_offset, (int)(sensor_min[ALT] * 10.0 + 0.5)); // Altitude
encodeB(b_min, 10 + head_offset, (int)(sensor_min[TEMP] * 10 + 0.5));
encodeA(b_min, 45 + head_offset, (int)(sensor_min[HUMI] * 10 + 0.5));
encodeA(b_min, 48 + head_offset, (int)(sensor_min[DTEMP] * 10 + 0.5) + 2048);
// encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1] * 10 + 0.5) + 2048);
encodeB(b, 31 + head_offset, ((int)(other[SPIN] * 10)) + 2048);
encodeA(b, 33 + head_offset, (int)(sensor[PRES] + 0.5)); // Pressure
encodeB(b, 34 + head_offset, (int)(sensor[ALT] / 10.0 + 0.5)); // Altitude
encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1]));
@ -1796,6 +1822,8 @@ void get_tlm_fox() {
encodeA(b, 51 + head_offset, status);
encodeB(b, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed * 2 + c2cStatus * 4);
encodeA(b, 53 + head_offset, groundCommandCount);
if (mode == BPSK) {
encodeA(b_max, 51 + head_offset, status);
encodeA(b_min, 51 + head_offset, status);

62
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv
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@ -0,0 +1,62 @@
61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MAX,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,MAX,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage
3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,MAX,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current
7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,MAX,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X solar panel Voltage
9,MAX,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,MAX,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,MAX,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X solar panel Voltage
12,MAX,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,MAX,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z solar panel Voltage
14,MAX,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X solar panel Current
15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y solar panel Current
16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z solar panel Current
17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X solar panel Current
18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y solar panel Current
19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z solar panel Current
20,MAX,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage
21,MAX,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MAX,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,MAX,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,MAX,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
26,MAX,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi
27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis
28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,BME280 Humidity
31,MAX,BAT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current
32,MAX,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,MAX,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
35,MAX,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,MAX,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator
37,MAX,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator
38,MAX,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,MAX,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,MAX,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,MAX,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator
42,MAX,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
43,MAX,RxAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
44,MAX,TxAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
45,MAX,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status
46,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
47,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
48,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
49,MAX,rf6,12,-,0,NONE,0,0,0,None,None
50,MAX,rf7,12,-,0,NONE,0,0,0,None,None
51,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
52,MAX,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
53,MAX,pad,4,-,34,NONE,0,0,0,None,Unused
54,MAX,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
55,MAX,pad1,1,-,0,NONE,0,0,0,NONE,Filler
56,MAX,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
57,MAX,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
58,MAX,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
59,MAX,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
60,MAX,pad2,27,-,0,NONE,0,0,0,NONE,Filler byets
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MAX Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MAX Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MAX BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 MAX posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 MAX posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 MAX posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 MAX negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 MAX negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 MAX negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 MAX posXi 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X solar panel Current
17 15 MAX posYi 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y solar panel Current
18 16 MAX posZi 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z solar panel Current
19 17 MAX negXi 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X solar panel Current
20 18 MAX negYi 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y solar panel Current
21 19 MAX negZi 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z solar panel Current
22 20 MAX BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MAX spin 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MAX Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 MAX Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 MAX Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MAX rssi 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MAX IHUcpuTemp 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity BME280 Humidity
33 31 MAX BAT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MAX DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MAX Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 MAX SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MAX SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MAX PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MAX I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MAX I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MAX GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MAX RxAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MAX TxAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MAX C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MAX ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
49 47 MAX ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
50 48 MAX ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
51 49 MAX rf6 12 - 0 NONE 0 0 0 None None
52 50 MAX rf7 12 - 0 NONE 0 0 0 None None
53 51 MAX MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
54 52 MAX LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
55 53 MAX pad 4 - 34 NONE 0 0 0 None Unused
56 54 MAX IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
57 55 MAX pad1 1 - 0 NONE 0 0 0 NONE Filler
58 56 MAX wodSize 8 000s 36 NONE 3 3 0 WOD Stored Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
59 57 MAX swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
60 58 MAX hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
61 59 MAX swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 MAX pad2 27 - 0 NONE 0 0 0 NONE Filler byets

62
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv
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61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MIN,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,MIN,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage
3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,MIN,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X solar panel Voltage
9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X solar panel Voltage
12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z solar panel Voltage
14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X solar panel Current
15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y solar panel Current
16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z solar panel Current
17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X solar panel Current
18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y solar panel Current
19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z solar panel Current
20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage
21,MIN,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MIN,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,MIN,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,MIN,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi
27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis
28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,BME280 Humidity
31,MIN,BAT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current
32,MIN,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,MIN,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
35,MIN,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,MIN,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator
37,MIN,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator
38,MIN,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,MIN,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,MIN,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,MIN,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator
42,MIN,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
43,MIN,RxAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
44,MIN,TxAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
45,MIN,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status
46,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
47,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
48,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
49,MIN,rf6,12,-,0,NONE,0,0,0,None,None
50,MIN,rf7,12,-,0,NONE,0,0,0,None,None
51,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
52,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
53,MIN,pad,4,-,34,NONE,0,0,0,None,Unused
54,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
55,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler
56,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
57,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
58,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
59,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
60,MIN,pad2,27,-,0,NONE,0,0,0,NONE,Filler
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MIN Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 MIN posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 MIN posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 MIN posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 MIN negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 MIN negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 MIN negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 MIN posXi 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X solar panel Current
17 15 MIN posYi 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y solar panel Current
18 16 MIN posZi 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z solar panel Current
19 17 MIN negXi 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X solar panel Current
20 18 MIN negYi 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y solar panel Current
21 19 MIN negZi 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z solar panel Current
22 20 MIN BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MIN spin 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 MIN Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MIN rssi 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MIN IHUcpuTemp 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity BME280 Humidity
33 31 MIN BAT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MIN DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MIN Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 MIN SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MIN SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MIN PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MIN RxAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MIN TxAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MIN C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MIN ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
49 47 MIN ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
50 48 MIN ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
51 49 MIN rf6 12 - 0 NONE 0 0 0 None None
52 50 MIN rf7 12 - 0 NONE 0 0 0 None None
53 51 MIN MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
54 52 MIN LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
55 53 MIN pad 4 - 34 NONE 0 0 0 None Unused
56 54 MIN IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
57 55 MIN pad1 1 - 0 NONE 0 0 0 NONE Filler
58 56 MIN wodSize 8 000s 36 NONE 3 3 0 WOD Stored Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
59 57 MIN swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
60 58 MIN hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
61 59 MIN swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 MIN pad2 27 - 0 NONE 0 0 0 NONE Filler

63
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv
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62,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,realTime,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,realTime,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,realTime,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current
7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,realTime,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,realTime,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,realTime,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage
12,realTime,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,realTime,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage
14,realTime,posXi,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X solar panel Current
15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y solar panel Current
16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z solar panel Current
17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X solar panel Current
18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y solar panel Current
19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z solar panel Current
20,realTime,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,realTime,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,realTime,Altitude,12,m,cubesatsim_altitude|INT,Experiments,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,realTime,rssi,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication
26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi
27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis
28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,realTime,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
31,realTime,BAT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,realTime,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,realTime,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
35,realTime,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,realTime,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator
37,realTime,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator
38,realTime,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,realTime,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator
42,realTime,GroundCommands,4,-,1,NONE,0,0,0,Ground Commands,Number of ground commands received
43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
44,realTime,TxAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
45,realTime,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status
46,realTime,GroundCommands2,10,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
47,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
48,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
49,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
50,realTime,rf6,12,-,0,NONE,0,0,0,None,None
51,realTime,rf7,12,-,0,NONE,0,0,0,None,None
52,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
53,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
54,realTime,pad,4,-,34,NONE,0,0,0,None,Unused
55,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
56,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler
57,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
58,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
59,realTime,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
60,realTime,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
61,realTime,pad2,17,-,0,NONE,0,0,0,NONE,Filler
1 62 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime Sensor 2 12 integer 1 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 realTime Sensor 3 12 integer 1 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 realTime BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 realTime SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 realTime SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 realTime SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 realTime BATT_I 12 mA cubesatsim_current Battery 4 2 3 Battery Current INA219 Battery Current
9 7 realTime Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 realTime posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 realTime posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 realTime posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 realTime negXv 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 realTime negYv 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 realTime negZv 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 realTime posXi 12 mA cubesatsim_current +X Panel 7 2 3 Current INA219 +X solar panel Current
17 15 realTime posYi 12 mA cubesatsim_current +Y Panel 8 2 3 Current INA219 +Y solar panel Current
18 16 realTime posZi 12 mA cubesatsim_current +Z Panel 9 2 3 Current INA219 +Z solar panel Current
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X solar panel Current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y solar panel Current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z solar panel Current
22 20 realTime BATT2_V 12 V cubesatsim_voltage|FLOAT2 Battery2 5 1 3 Battery2 Voltage INA219 Battery2 Voltage
23 21 realTime spin 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 realTime Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 realTime Altitude 12 m cubesatsim_altitude|INT Experiments 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 realTime Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 realTime rssi 12 dBm cubesatsim_rssi|INT Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 realTime IHUcpuTemp 12 C cubesatsim_temperature Computer Hardware 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 realTime SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 realTime SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 realTime SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 realTime Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity BME280 Humidity
33 31 realTime BAT2_I 12 mA cubesatsim_current Battery2 5 2 3 Battery2 Current INA219 Battery2 Current
34 32 realTime DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 realTime Sensor 1 12 integer 1 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 realTime STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 realTime SafeMode 1 - STATUS_ON_OFF Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 realTime SimulatedTelemetry 1 - STATUS_ON_OFF Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 realTime PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 realTime I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 realTime I2CBus1Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 realTime I2CBus3Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 realTime CameraFailure 1 - 17 Computer Hardware 2 4 0 Camera Camera failure indicator
44 42 realTime GroundCommands 4 - 1 NONE 0 0 0 Ground Commands Number of ground commands received
45 43 realTime RxAntenna 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 realTime TxAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 realTime C2CStatus 2 - COMMAND_STATUS Computer Software 3 5 0 Command Control Command & Control Status
48 46 realTime GroundCommands2 10 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
49 47 realTime ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
50 48 realTime ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
51 49 realTime ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
52 50 realTime rf6 12 - 0 NONE 0 0 0 None None
53 51 realTime rf7 12 - 0 NONE 0 0 0 None None
54 52 realTime MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
55 53 realTime LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
56 54 realTime pad 4 - 34 NONE 0 0 0 None Unused
57 55 realTime IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
58 56 realTime pad1 1 - 0 NONE 0 0 0 NONE Filler
59 57 realTime wodSize 8 000s 36 NONE 3 3 0 WOD Stored Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
60 58 realTime swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
61 59 realTime hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
62 60 realTime swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
63 61 realTime pad2 17 - 0 NONE 0 0 0 NONE Filler

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spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv
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CurveName,a,bx,cx^2,dx^3,ex^4,fx^5,Description
cubesatsim_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 sensors
cubesatsim_current,-2048,1,0,0,0,0,Converts positive and negative currents read from the INA219 sensors
cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi
cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation
cubesatsim_acceleration,-20.48,0.01,0,0,0,0,Converts positive and negative g acceleration
cubesatsim_altitude,0,10,0,0,0,0,Converts altitude
cubesatsim_pressure,0,1,0,0,0,0,Converts pressure
cubesatsim_sensor1,0,1,0,0,0,0,Conversion of Sensor 1
cubesatsim_sensor2,-2048,1,0,0,0,0,Conversion of Sensor 2
cubesatsim_sensor3,-20.48,0.01,0,0,0,0,Conversion of Sensor 3
cubesatsim_rpm,-204.8,0.1,0,0,0,0,Conversion of calculated RPM
cubesatsim_rssi,-2048,1,0,0,0,0,Conversion of Received Signal Strength
1 CurveName a bx cx^2 dx^3 ex^4 fx^5 Description
2 cubesatsim_voltage 0 0.01 0 0 0 0 Converts voltages read from the INA219 sensors
3 cubesatsim_current -2048 1 0 0 0 0 Converts positive and negative currents read from the INA219 sensors
4 cubesatsim_temperature 0 0.1 0 0 0 0 Converts temperature of Pi
5 cubesatsim_rotation -2048 1 0 0 0 0 Converts positive and negative dps rotation
6 cubesatsim_acceleration -20.48 0.01 0 0 0 0 Converts positive and negative g acceleration
7 cubesatsim_altitude 0 10 0 0 0 0 Converts altitude
8 cubesatsim_pressure 0 1 0 0 0 0 Converts pressure
9 cubesatsim_sensor1 0 1 0 0 0 0 Conversion of Sensor 1
10 cubesatsim_sensor2 -2048 1 0 0 0 0 Conversion of Sensor 2
11 cubesatsim_sensor3 -20.48 0.01 0 0 0 0 Conversion of Sensor 3
12 cubesatsim_rpm -204.8 0.1 0 0 0 0 Conversion of calculated RPM
13 cubesatsim_rssi -2048 1 0 0 0 0 Conversion of Received Signal Strength

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spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv
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47,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MAX,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,MAX,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage
3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,MAX,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current
7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature
8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X Panel Voltage
9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X Panel Voltage
10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y Panel Voltage
11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y Panel Voltage
12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z Panel Voltage
13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z Panel Voltage
14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X Panel Current
15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X Panel Current
16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y Panel Current
17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y Panel Current
18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z Panel Current
19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z Panel Current
20,MAX,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage
21,MAX,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MAX,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure
23,MAX,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude
24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,MAX,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
26,MAX,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU
27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis
28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis
29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis
30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity
31,MAX,BATT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current
32,MAX,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,MAX,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
35,MAX,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,MAX,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator
37,MAX,PayloadStatus1,1,-,17,NONE,0,0,0,Exp 3,STEM Payload status 1 failure indicator
38,MAX,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,MAX,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,MAX,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,MAX,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator
42,MAX,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
43,MAX,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
44,MAX,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
45,MAX,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status
46,MAX,Pad,56,-,0,NONE,0,0,0,NONE,NONE
1 47 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MAX Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MAX Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MAX BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 MAX PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X Panel Voltage
11 9 MAX PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X Panel Voltage
12 10 MAX PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 MAX PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 MAX PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 MAX PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 MAX PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X Panel Current
17 15 MAX PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X Panel Current
18 16 MAX PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y Panel Current
19 17 MAX PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y Panel Current
20 18 MAX PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z Panel Current
21 19 MAX PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z Panel Current
22 20 MAX BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MAX SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MAX Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 MAX Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 MAX Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MAX RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MAX IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 MAX BATT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MAX DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MAX Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MAX SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MAX SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MAX PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MAX I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MAX I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MAX GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MAX RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MAX TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MAX C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MAX Pad 56 - 0 NONE 0 0 0 NONE NONE

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spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv
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47,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MIN,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,MIN,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage
3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,MIN,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature
8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X Panel Voltage
9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X Panel Voltage
10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y Panel Voltage
11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y Panel Voltage
12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z Panel Voltage
13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z Panel Voltage
14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X Panel Current
15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X Panel Current
16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y Panel Current
17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y Panel Current
18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z Panel Current
19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z Panel Current
20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage
21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MIN,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure
23,MIN,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude
24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,MIN,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
26,MIN,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU
27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis
28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity
31,MIN,BATT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current
32,MIN,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,MIN,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
35,MIN,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,MIN,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator
37,MIN,PayloadStatus1,1,-,17,NONE,0,0,0,Exp 3,STEM Payload status 1 failure indicator
38,MIN,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,MIN,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,MIN,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,MIN,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator
42,MIN,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
43,MIN,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
44,MIN,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
45,MIN,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status
46,MIN,Pad,56,-,0,NONE,0,0,0,NONE,NONE
1 47 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MIN Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X Panel Voltage
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X Panel Voltage
12 10 MIN PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 MIN PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 MIN PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 MIN PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 MIN PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X Panel Current
17 15 MIN PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X Panel Current
18 16 MIN PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y Panel Current
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y Panel Current
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z Panel Current
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z Panel Current
22 20 MIN BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MIN SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MIN RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MIN IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 MIN BATT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MIN DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MIN Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MIN SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MIN SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MIN PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MIN RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MIN TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MIN C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MIN Pad 56 - 0 NONE 0 0 0 NONE NONE

49
spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv
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@ -0,0 +1,49 @@
48,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,RT,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,RT,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,RT,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X Panel Voltage
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X Panel Voltage
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y Panel Voltage
11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y Panel Voltage
12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z Panel Voltage
13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z Panel Voltage
14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X Panel Current
15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X Panel Current
16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y Panel Current
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y Panel Current
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z Panel Current
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z Panel Current
20,RT,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,RT,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure
23,RT,Altitude,12,m,cubesatsim_altitude|INT,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude
24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication
26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity
31,RT,BATT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,RT,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,RT,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status
35,RT,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,RT,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator
37,RT,PayloadStatus1,1,-,17,NONE,0,0,0,Exp 3,STEM Payload status 1 failure indicator
38,RT,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,RT,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator
42,RT,GroundCommands,4,-,1,NONE,0,0,0,Ground Commands,Number of ground commands received
43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
45,RT,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status
46,RT,GroundCommands2,10,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
47,RT,Pad,46,-,0,NONE,0,0,0,NONE,NONE
1 48 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 RT Sensor 2 12 integer 1 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 RT Sensor 3 12 integer 1 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 RT BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 RT BATT_I 12 mA cubesatsim_current Battery 4 2 3 Battery Current INA219 Battery Current
9 7 RT Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage INA219 +X Panel Voltage
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage INA219 -X Panel Voltage
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current INA219 +X Panel Current
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X Panel Current
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current INA219 +Y Panel Current
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y Panel Current
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current INA219 +Z Panel Current
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z Panel Current
22 20 RT BATT2_V 12 V cubesatsim_voltage|FLOAT2 Battery2 5 1 3 Battery2 Voltage INA219 Battery2 Voltage
23 21 RT SPIN 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 RT Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 RT Altitude 12 m cubesatsim_altitude|INT Experiments 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 RT Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 RT RSSI 12 dBm cubesatsim_rssi|INT Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer Hardware 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 RT BATT2_I 12 mA cubesatsim_current Battery2 5 2 3 Battery2 Current INA219 Battery2 Current
34 32 RT DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 RT Sensor 1 12 integer 1 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 RT SafeMode 1 - STATUS_ON_OFF Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 RT SimulatedTelemetry 1 - STATUS_ON_OFF Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 RT PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 RT I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 RT I2CBus1Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 RT CameraFailure 1 - 17 Computer Hardware 2 4 0 Camera Camera failure indicator
44 42 RT GroundCommands 4 - 1 NONE 0 0 0 Ground Commands Number of ground commands received
45 43 RT RXAntenna 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 RT TXAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 RT C2CStatus 2 - COMMAND_STATUS Computer Software 3 5 0 Command Control Command & Control Status
48 46 RT GroundCommands2 10 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
49 47 RT Pad 46 - 0 NONE 0 0 0 NONE NONE

7
spacecraft/FoxTelem_1.13i/README.md
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These files update the spacecraft files in FoxTelem version 1.13i or later and fix a bug in the payload altitude sensor display.
You can download them as a zip file: [foxtelem_spacecraft_files.zip](https://github.com/user-attachments/files/23393444/foxtelem_spacecraft_files.zip)
Extract (unzip foxtelem_spacecraft_files.zip) and copy into FoxTelem spacecraft folder, replacing existing files.
Next time you run FoxTelem, the CubeSatSim-FSK and CubeSatSim-BPSK spacecraft will be automatically updated.

2
stempayload/Payload_BME280_MPU6050_AIO/readme.MD
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@ -1,5 +1,7 @@
This code for the Raspberry Pi Pico W supports the built-in BME-280 and MPU-6050 sensors on the Main board and adds support for Adafruit.io
Here is a ZIP file of these files: https://github.com/user-attachments/files/21951798/Payload_BME280_MPU6050_AIO.zip
To use this code, you will need to create a Free account at https://io.adafruit.com
You will need to configure your Adafruit.io account information and your WiFi credentials in the edit_this_config_and_rename.h file

4
update
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@ -47,6 +47,8 @@ sudo sed -i 's/update to/update\nto/g' /etc/motd
sudo sed -i 's/console=tty1 r/console=tty1 maxcpus=1 r/g' /boot/cmdline.txt # single core if Pi Zero 2
sudo sed -i 's/maxcpus=2/maxcpus=1/g' /boot/cmdline.txt # single core if Pi Zero 2
cd /home/pi/CubeSatSim
git pull --no-rebase > .updated
@ -404,7 +406,7 @@ cd /home/pi/ssdv
# sudo apt-get update && sudo apt-get dist-upgrade -y
sudo apt-get update -y
sudo apt-get install -y libjpeg-dev zlib1g-dev libfreetype6-dev liblcms1-dev libopenjp2-7 libtiff5 python3-pil
sudo pip3 install adafruit-blinka RPI.GPIO adafruit-extended-bus adafruit-circuitpython-ina219 pillow
sudo pip3 install -y adafruit-blinka RPI.GPIO adafruit-extended-bus adafruit-circuitpython-ina219 pillow
fi

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