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CubeSatSim
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alanbjohnston 5 years ago committed by GitHub
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5
README.md
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@ -4,7 +4,7 @@ The CubeSat Simulator https://github.com/alanbjohnston/CubeSatSim/wiki is a low
There are several hardware versions and software branches to go with them - see below for information. There are several hardware versions and software branches to go with them - see below for information.
See the Wiki Software Install page for more details: https://github.com/alanbjohnston/CubeSatSim/wiki/Software-Install. The software runs on any Raspberry Pi including the Raspberry Pi 4B, 3B, 3B+, Pi Zero or Pi Zero W. See the Wiki Software Install page for more details: https://github.com/alanbjohnston/CubeSatSim/wiki/2.-Software-Install. The software runs on any Raspberry Pi including the Raspberry Pi 4B, 3B, 3B+, Pi Zero or Pi Zero W.
There are two ways to get the CubeSatSim software for your Pi. There are two ways to get the CubeSatSim software for your Pi.
@ -17,12 +17,13 @@ The other option is to start with any Raspberry Pi OS (Rasbian) image and run th
- pi-power-button - pi-power-button
- Direwolf - Direwolf
- rpitx - rpitx
- cpulimit
- python3-pip - python3-pip
- python-smbus - python-smbus
## Disk Image Option Steps ## Disk Image Option Steps
See the Wiki Software Install page for details: https://github.com/alanbjohnston/CubeSatSim/wiki/Software-Install. See the Wiki Software Install page for details: https://github.com/alanbjohnston/CubeSatSim/wiki/2.-Software-Install.
## Installation Script Option Steps ## Installation Script Option Steps

810
afsk/main.c
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4
arduino/Payload_BME280_MPU6050_XS.ino
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@ -81,6 +81,8 @@ void setup() {
Serial.println(((float)eeprom_word_read(2)) / 100.0, DEC); Serial.println(((float)eeprom_word_read(2)) / 100.0, DEC);
Serial.println(((float)eeprom_word_read(3)) / 100.0, DEC); Serial.println(((float)eeprom_word_read(3)) / 100.0, DEC);
} }
pinMode(greenLED, OUTPUT);
pinMode(blueLED, OUTPUT);
} }
void loop() { void loop() {
@ -271,7 +273,7 @@ void blink(int length)
#if defined __AVR_ATmega32U4__ #if defined __AVR_ATmega32U4__
digitalWrite(RXLED, HIGH); // set the RX LED OFF digitalWrite(RXLED, HIGH); // set the RX LED OFF
TXLED0; //TX LED is not tied to a normally controlled pin so a macro is needed, turn LED OFF TXLED0; //TX LED macro to turn LED ON
#endif #endif
} }

209
config
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@ -0,0 +1,209 @@
#!/bin/bash
# echo $1
if [ "$1" = "" ]; then
echo "Include a configuration option:"
echo
set -- "-h"
fi
if [ "$1" = "-i" ]; then
echo "Restarting CubeSatSim"
sudo systemctl restart cubesatsim
exit
elif [ "$1" = "-a" ]; then
echo "changing CubeSatSim to AFSK mode"
sudo echo "ARG1=a" > .mode
sudo systemctl restart cubesatsim
exit
elif [ "$1" = "-f" ]; then
echo "changing CubeSatSim to FSK mode"
sudo echo "ARG1=f" > .mode
sudo systemctl restart cubesatsim
exit
elif [ "$1" = "-b" ]; then
echo "changing CubeSatSim to BPSK mode"
sudo echo "ARG1=b" > .mode
sudo systemctl restart cubesatsim
exit
elif [ "$1" = "-s" ]; then
echo "changing CubeSatSim to SSTV mode"
sudo echo "ARG1=s" > .mode
sudo systemctl restart cubesatsim
exit
elif [ "$1" = "-h" ]; then
echo "config OPTION"
echo
echo "Changes CubeSatSim mode, resets, or modifies configuration file"
echo
echo " -h This help info"
echo " -a Change to AFSK/APRS mode"
echo " -f Change to FSK/DUV mode"
echo " -b Change to BPSK mode"
echo " -s Change to SSTV mode"
echo " -i Restarts CubeSatsim software"
echo " -c Change the CALLSIGN in the configuration file sim.cfg"
echo " -r Change the Resets Count in the configuration file sim.cfg"
echo " -l Change the Latitude and Longitude in the configuration file sim.cfg"
echo " Only used for APRS telemetry"
echo
exit
elif [ "$1" = "-c" ]; then
echo
echo "Editing the CALLSIGN in the"
echo "configuration file for CubeSatSim"
echo
echo "Return keeps current value."
# echo -e "Current sim.cfg configuration file:"
# echo
value=`cat /home/pi/CubeSatSim/sim.cfg`
echo "$value" > /dev/null
set -- $value
echo "Current value of CALLSIGN is"
echo $1
echo
# echo $1 $2 $3 $4
echo "Enter callsign in all capitals: "
read callsign
if [ -z $callsign ] ; then
callsign="$1"
echo "Keeping value of" $callsign
fi
echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
echo $callsign $2 $3 $4
echo $callsign $2 $3 $4 > /home/pi/CubeSatSim/sim.cfg
echo
echo "Restarting CubeSatSim with new configuraation file"
echo
sudo systemctl restart cubesatsim
elif [ "$1" = "-r" ]; then
echo
echo "Editing the Reset Count in the"
echo "configuration file for CubeSatSim"
echo
echo "Return keeps current value."
# echo -e "Current sim.cfg configuration file:"
# echo
value=`cat /home/pi/CubeSatSim/sim.cfg`
echo "$value" > /dev/null
set -- $value
echo
echo "Current value of Reset Count is"
echo $2
echo
# echo $1 $2 $3 $4
echo -e "Enter Reset Count (integer): "
read resets
if [ -z $resets ] ; then
resets="$2"
echo "Keeping value of" $resets
fi
if ! [[ $resets =~ ^[0-9]+$ ]] ; then
echo "Error: not an integer!"
resets="$2"
echo "Keeping value of" $resets
fi
echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
echo $1 $resets $3 $4
echo $1 $resets $3 $4 > /home/pi/CubeSatSim/sim.cfg
echo
echo "Restarting CubeSatSim with new configuraation file"
echo
sudo systemctl restart cubesatsim
elif [ "$1" = "-l" ]; then
echo
echo "Editing latitude and longitude in the"
echo "configuration file for CubeSatSim"
echo "(Only used for APRS telemetry)"
echo
echo "Return keeps current value."
# echo -e "Current sim.cfg configuration file:"
# echo
value=`cat /home/pi/CubeSatSim/sim.cfg`
echo "$value" > /dev/null
set -- $value
echo
echo "Current value of latitude is"
echo $3
echo
# echo $1 $2 $3 $4
echo -e "Enter latitude (decimal degrees, positive is north): "
read lat
if [ -z $lat ] ; then
lat="$3"
echo "Keeping value of" $lat
fi
if ! [[ $lat =~ ^[+-]?[0-9]+([.][0-9]+)?$ ]] ; then
echo "Error: not a number!"
lat="$3"
echo "Keeping value of" $lat
fi
echo
echo "Current value of longitude is"
echo $4
echo
echo -e "Enter longitude (decimal degrees, positive is east): "
read long
if [ -z $long ] ; then
long="$4"
echo "Keeping value of" $long
fi
if ! [[ $long =~ ^[+-]?[0-9]+([.][0-9]+)?$ ]] ; then
echo "Error: not a number!"
long="$4"
echo "Keeping value of" $long
fi
echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
echo $1 $2 $lat $long
echo $1 $2 $lat $long > /home/pi/CubeSatSim/sim.cfg
echo
echo "Restarting CubeSatSim with new configuraation file"
echo
sudo systemctl restart cubesatsim
fi
# sudo systemctl restart cubesatsim

5
demo.sh
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@ -15,8 +15,9 @@ if [[ ("$1" = "a" ) || (("$1" = "c") && ("$(($y %4))" = 3)) ]]; then
echo "Mode is continuous AFSK" echo "Mode is continuous AFSK"
/home/pi/CubeSatSim/radioafsk afsk /home/pi/CubeSatSim/radioafsk afsk
elif [[ ("$1" = "b" ) || (("$1" = "c") && ("$(($y %4))" = 1)) ]]; then elif [[ ("$1" = "b" ) || (("$1" = "c") && ("$(($y %4))" = 1)) ]]; then
echo "Mode is continuous BPSK" echo "Mode is continuous BPSK"
/home/pi/CubeSatSim/radioafsk bpsk sudo cpulimit -l 2.5 -b -P radioafsk
/home/pi/CubeSatSim/radioafsk bpsk
elif [[ ("$1" = "s" ) || (("$1" = "c") && ("$(($y %4))" = 2)) ]]; then elif [[ ("$1" = "s" ) || (("$1" = "c") && ("$(($y %4))" = 2)) ]]; then
echo "Mode is continuous SSTV" echo "Mode is continuous SSTV"
while true; do sleep 5; done while true; do sleep 5; done

9
log
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@ -0,0 +1,9 @@
#!/bin/bash
echo -e "\nLog file script for CubeSatSim\n"
sudo journalctl -u cubesatsim > log.txt
cat log.txt
echo -e "\nLog file also saved as /home/pi/CubeSatSim/log.txt"

354
python/voltcurrent.py
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@ -1,20 +1,22 @@
"""Sample code and test for adafruit_in219""" """Sample code and test for adafruit_in219"""
# Reads all voltage and current sensors for two I2C buses # Reads all voltage and current sensors for two I2C buses
import time
import sys import sys
#import board #import board
import busio import busio
from adafruit_extended_bus import ExtendedI2C as I2C from adafruit_extended_bus import ExtendedI2C as I2C
from adafruit_ina219 import INA219 from adafruit_ina219 import INA219
from adafruit_ina219 import ADCResolution, BusVoltageRange
if __name__ == "__main__": if __name__ == "__main__":
# print 'Length: ', len(sys.argv) # print 'Length: ', len(sys.argv)
buses = [1, 3] # default I2C buses buses = [1, 3] # default I2C buses
config = False config = False
one = two = three = four = five = six = seven = eight = 0
if (len(sys.argv)) > 1: if (len(sys.argv)) > 1:
# print("There are arguments!") # print("There are arguments!", file=sys.stderr)
# if (('a' == sys.argv[1]) or ('afsk' in sys.argv[1])): # if (('a' == sys.argv[1]) or ('afsk' in sys.argv[1])):
buses[0] = int(sys.argv[1], base=10) buses[0] = int(sys.argv[1], base=10)
if (len(sys.argv)) > 2: if (len(sys.argv)) > 2:
@ -22,45 +24,325 @@ if __name__ == "__main__":
if (len(sys.argv)) > 3: if (len(sys.argv)) > 3:
if sys.argv[3] == "c": if sys.argv[3] == "c":
config = True config = True
from adafruit_ina219 import ADCResolution, BusVoltageRange
# print(buses[0])
# print(buses[1])
addresses = [0x40, 0x41, 0x44, 0x45] #INA219 addresses on the bus addresses = [0x40, 0x41, 0x44, 0x45] #INA219 addresses on the bus
# print("buses: ", buses, " addr: ", addresses) # print("buses: ", buses, " addr: ", addresses, file=sys.stderr)
for x in buses:
try: # config
i2c_bus = I2C(x) # Device is /dev/i2c-x
for y in addresses: # for x in buses:
# print(x,y) # try:
try: # i2c_bus = I2C(x) # Device is /dev/i2c-x
# for y in addresses:
# print(x,y)
# try:
# Create library object using Extended Bus I2C port # Create library object using Extended Bus I2C port
# print("bus: ", x, " addr: ", y) # print("bus: ", x, " addr: ", y)
if x == 0 and y == 0x45: # if x == 0 and y == 0x45:
# print("Reading INA219 in MoPower Board") # print("Reading INA219 in MoPower Board")
i2c_bus = I2C(1) # i2c_bus = I2C(1)
ina219 = INA219(i2c_bus, 0x4a) # ina219 = INA219(i2c_bus, 0x4a)
else: # else:
ina219 = INA219(i2c_bus, y) # ina219 = INA219(i2c_bus, y)
# print("ina219 test")
# print("ina219 test")
if config: # print("Configuring")
# print("Configuring")
# optional : change configuration to use 32 samples averaging for both bus voltage and shunt voltage # optional : change configuration to use 32 samples averaging for both bus voltage and shunt voltage
ina219.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S # ina219.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
ina219.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S # ina219.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
# optional : change voltage range to 16V # optional : change voltage range to 16V
ina219.bus_voltage_range = BusVoltageRange.RANGE_16V # ina219.bus_voltage_range = BusVoltageRange.RANGE_16V
# except:
# print("Python Error 2", file=sys.stderr, flush=True)
# except:
# print("Python Error 1", file=sys.stderr, flush=True)
# No try checking yet
# if buses[0] == 0 and addresses[0] == 0x45:
# print("Reading INA219 in MoPower Board")
# ina219_one = INA219(I2C(1), 0x4a)
# else:
if (buses[0] != -1):
try:
i2c_one = I2C(buses[0])
try:
ina219_one = INA219(i2c_one, addresses[0])
ina219_one.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_one.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_one.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
one = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
one = 0
try:
ina219_two = INA219(i2c_one, addresses[1])
ina219_two.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_two.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_two.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
two = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
two = 0
try:
ina219_three = INA219(i2c_one, addresses[2])
ina219_three.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_three.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_three.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
three = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
three = 0
try:
ina219_four= INA219(i2c_one, addresses[3])
ina219_four.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_four.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_four.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
four = 1
except:
four = 0
# print("Python Error 3", file=sys.stderr, flush=True)
except:
print("Python Error 5", file=sys.stderr, flush=True)
if (buses[1] != -1):
try:
i2c_two = I2C(buses[1])
# print(i2c_two)
try:
ina219_five = INA219(i2c_two, addresses[0])
ina219_five.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_five.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_five.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
five = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
five = 0
try:
ina219_six = INA219(i2c_two, addresses[1])
ina219_six.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_six.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_six.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
six = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
six = 0
try:
ina219_seven = INA219(i2c_two, addresses[2])
ina219_seven.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_seven.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_seven.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
seven = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
seven = 0
try:
ina219_eight = INA219(i2c_two, addresses[3])
ina219_eight.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_eight.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_eight.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
eight = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
eight = 0
except:
print("Python Error 5", file=sys.stderr, flush=True)
while (True):
error = 0
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_one.bus_voltage), "{:6.3f} ".format(ina219_one.current) , end = '')
except:
try:
ina219_one = INA219(i2c_one, addresses[0])
ina219_one.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_one.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_one.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_one.bus_voltage), "{:6.3f} ".format(ina219_one.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_two.bus_voltage), "{:6.3f} ".format(ina219_two.current) , end = '')
except:
try:
ina219_two = INA219(i2c_one, addresses[1])
ina219_two.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_two.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_two.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_two.bus_voltage), "{:6.3f} ".format(ina219_two.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
bus_voltage = ina219.bus_voltage # voltage on V- (load side)
# shunt_voltage = ina219.shunt_voltage # voltage between V+ and V- across the shunt try:
current = ina219.current # current in mA time.sleep(0.01)
if x == 0 and y == 0x45: print("{:6.3f} ".format(ina219_three.bus_voltage), "{:6.3f} ".format(ina219_three.current) , end = '')
current = current * 10 except:
# INA219 measure bus voltage on the load side. So PSU voltage = bus_voltage + shunt_voltage
# print("{:6.3f}".format(bus_voltage + shunt_voltage)) try:
print("{:6.3f} ".format(bus_voltage), "{:6.3f} ".format(current) , end = '') ina219_three = INA219(i2c_one, addresses[2])
except: ina219_three.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '') time.sleep(0.001)
ina219_three.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_three.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_three.bus_voltage), "{:6.3f} ".format(ina219_three.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_four.bus_voltage), "{:6.3f} ".format(ina219_four.current) , end = '')
except:
try:
ina219_four= INA219(i2c_one, addresses[3])
ina219_four.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_four.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_four.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_four.bus_voltage), "{:6.3f} ".format(ina219_four.current) , end = '')
error = 1
except:
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_five.bus_voltage), "{:6.3f} ".format(ina219_five.current) , end = '')
except:
try:
ina219_five = INA219(i2c_two, addresses[0])
ina219_five.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_five.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_five.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_five.bus_voltage), "{:6.3f} ".format(ina219_five.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_six.bus_voltage), "{:6.3f} ".format(ina219_six.current) , end = '')
except:
try:
ina219_six = INA219(i2c_two, addresses[1])
ina219_six.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_six.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_six.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_six.bus_voltage), "{:6.3f} ".format(ina219_six.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_seven.bus_voltage), "{:6.3f} ".format(ina219_seven.current) , end = '')
except:
try:
ina219_seven = INA219(i2c_two, addresses[2])
ina219_seven.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_seven.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_seven.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_seven.bus_voltage), "{:6.3f} ".format(ina219_seven.current) , end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
try:
time.sleep(0.01)
print("{:6.3f} ".format(ina219_eight.bus_voltage), "{:6.3f} ".format(ina219_eight.current), end = '')
except: except:
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
# pass try:
print(" ") ina219_eight = INA219(i2c_two, addresses[3])
ina219_eight.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_eight.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S # 1S
time.sleep(0.001)
ina219_eight.bus_voltage_range = BusVoltageRange.RANGE_16V
time.sleep(0.01)
print("{:6.3f} ".format(ina219_eight.bus_voltage), "{:6.3f} ".format(ina219_eight.current), end = '')
error = 1
except:
# print("Python Error 3", file=sys.stderr, flush=True)
print("{:6.3f} ".format(0), "{:6.3f} ".format(0), end = '')
if (error == 0):
print(" ")
else:
print("Python Error Recovered!")
inp = input()
# print(inp)

1
rpitx.py
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@ -109,6 +109,7 @@ if __name__ == "__main__":
else: else:
print("FSK") print("FSK")
system("sudo nc -l 8080 | csdr convert_i16_f | csdr gain_ff 7000 | csdr convert_f_samplerf 20833 | sudo /home/pi/rpitx/rpitx -i- -m RF -f 434.9e3") system("sudo nc -l 8080 | csdr convert_i16_f | csdr gain_ff 7000 | csdr convert_f_samplerf 20833 | sudo /home/pi/rpitx/rpitx -i- -m RF -f 434.9e3")
else: else:
print("No Band Pass Filter so no telemetry transmit. See http://cubesatsim.org/wiki for instructions on how to build the BPF.") print("No Band Pass Filter so no telemetry transmit. See http://cubesatsim.org/wiki for instructions on how to build the BPF.")
while 1: while 1:

61
spacecraft/FoxTelem_11a/CubeSatSim_PSK_maxtelemetry.csv
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@ -0,0 +1,61 @@
60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
6,MAX,battCurr,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature
8,MAX,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage
9,MAX,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage
10,MAX,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage
11,MAX,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage
12,MAX,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage
13,MAX,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage
14,MAX,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X solar Panel current
15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y solar Panel current
16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z solar Panel current
17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X solar Panel current
18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y solar Panel current
19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z solar Panel current
20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply 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,Pressure,STEM Payload Sensor Pressure
23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,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,Temperature,Internal Temperature of IHU
27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,Humidity
31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MAX,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,MAX,Sensor2,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
37,MAX,rf6,12,-,0,NONE,0,0,0,None,None
38,MAX,rf7,12,-,0,NONE,0,0,0,None,None
39,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
40,MAX,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
41,MAX,pad,4,-,34,NONE,0,0,0,None,Unused
42,MAX,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
43,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
44,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
45,MAX,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator
46,MAX,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator
47,MAX,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator
48,MAX,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator
49,MAX,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator
50,MAX,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
51,MAX,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status
52,MAX,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status
53,MAX,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator
54,MAX,pad1,1,-,0,NONE,0,0,0,NONE,Filler
55,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
56,MAX,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
57,MAX,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
58,MAX,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
59,MAX,pad2,28,-,0,NONE,0,0,0,NONE,Filler
1 60 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MAX BATT_A_V 12 V 4 NONE 4 1 3 Cell A Battery pair A voltage (0-2.5V scale)
3 1 MAX BATT_B_V 12 V 4 NONE 4 2 3 Cell A + B Battery pairs A+B voltage (0-3.3V scale)
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MAX battCurr 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temp STEM Payload Sensor Temperature
10 8 MAX posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X solar Panel voltage
11 9 MAX posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y solar Panel voltage
12 10 MAX posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z solar Panel voltage
13 11 MAX negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X solar Panel voltage
14 12 MAX negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y solar Panel voltage
15 13 MAX negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z solar Panel voltage
16 14 MAX posXi 12 mA cubesatsim_current NONE 7 2 3 Current +X solar Panel current
17 15 MAX posYi 12 mA cubesatsim_current NONE 8 2 3 Current +Y solar Panel current
18 16 MAX posZi 12 mA cubesatsim_current NONE 9 2 3 Current +Z solar Panel current
19 17 MAX negXi 12 mA cubesatsim_current NONE 10 2 3 Current -X solar Panel current
20 18 MAX negYi 12 mA cubesatsim_current NONE 11 2 3 Current -Y solar Panel current
21 19 MAX negZi 12 mA cubesatsim_current NONE 12 2 3 Current -Z solar Panel current
22 20 MAX PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Board Voltage Power Supply 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 Pressure STEM Payload Sensor Pressure
25 23 MAX Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude 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 Temperature Internal Temperature of IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 Humidity Humidity
33 31 MAX PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MAX Sensor1 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 33 MAX Sensor2 12 signed raw cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
36 34 MAX ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
37 35 MAX ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
38 36 MAX ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
39 37 MAX rf6 12 - 0 NONE 0 0 0 None None
40 38 MAX rf7 12 - 0 NONE 0 0 0 None None
41 39 MAX MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
42 40 MAX LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
43 41 MAX pad 4 - 34 NONE 0 0 0 None Unused
44 42 MAX IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
45 43 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload Board Failure Indicator
46 44 MAX Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
47 45 MAX expFailure2 1 - 17 NONE 6 7 0 Exp 2 Experiment 2 Failure Indicator
48 46 MAX expFailure3 1 - 17 NONE 6 8 0 Exp 3 Experiment 3 Failure Indicator
49 47 MAX I2CfailureBatt 1 - 17 NONE 2 2 0 Battery I2C Battery I2C Bus failure indicator
50 48 MAX I2CfailurePSU1 1 - 17 NONE 2 3 0 PSU1 I2C PSU2 I2C Bus failure indicator
51 49 MAX I2CfailurePSU2 1 - 17 NONE 2 4 0 PSU2 I2C PSU2 I2C Bus failure indicator
52 50 MAX TLMresets 4 - 1 NONE 2 6 0 Ground Resets Number of times command stations reset stored telemetry
53 51 MAX RxAntDeploy 1 - 16 NONE 1 3 0 RX Antenna 2m Antenna status
54 52 MAX TxAntDeploy 2 - 16 NONE 1 2 0 TX Antenna 70cm Antenna status
55 53 MAX I2CfailureRF 1 - 17 NONE 2 5 0 RF I2C RF I2C Bus failure indicator
56 54 MAX pad1 1 - 0 NONE 0 0 0 NONE Filler
57 55 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
58 56 MAX swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
59 57 MAX hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
60 58 MAX swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
61 59 MAX pad2 28 - 0 NONE 0 0 0 NONE Filler

61
spacecraft/FoxTelem_11a/CubeSatSim_PSK_mintelemetry.csv
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@ -0,0 +1,61 @@
60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
6,MIN,battCurr,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature
8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage
9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage
10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage
11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage
12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage
13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage
14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X solar Panel current
15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y solar Panel current
16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z solar Panel current
17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X solar Panel current
18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y solar Panel current
19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z solar Panel current
20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply 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,Pressure,STEM Payload Sensor Pressure
23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,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,Temperature,Internal Temperature of IHU
27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,Humidity
31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MIN,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,MIN,Sensor2,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
37,MIN,rf6,12,-,0,NONE,0,0,0,None,None
38,MIN,rf7,12,-,0,NONE,0,0,0,None,None
39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused
42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
43,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
44,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator
46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator
47,MIN,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator
48,MIN,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator
49,MIN,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator
50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
51,MIN,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status
52,MIN,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status
53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator
54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler
55,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
56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler
1 60 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN BATT_A_V 12 V 4 NONE 4 1 3 Cell A Battery pair A voltage (0-2.5V scale)
3 1 MIN BATT_B_V 12 V 4 NONE 4 2 3 Cell A + B Battery pairs A+B voltage (0-3.3V scale)
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MIN battCurr 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temp STEM Payload Sensor Temperature
10 8 MIN posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X solar Panel voltage
11 9 MIN posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y solar Panel voltage
12 10 MIN posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z solar Panel voltage
13 11 MIN negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X solar Panel voltage
14 12 MIN negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y solar Panel voltage
15 13 MIN negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z solar Panel voltage
16 14 MIN posXi 12 mA cubesatsim_current NONE 7 2 3 Current +X solar Panel current
17 15 MIN posYi 12 mA cubesatsim_current NONE 8 2 3 Current +Y solar Panel current
18 16 MIN posZi 12 mA cubesatsim_current NONE 9 2 3 Current +Z solar Panel current
19 17 MIN negXi 12 mA cubesatsim_current NONE 10 2 3 Current -X solar Panel current
20 18 MIN negYi 12 mA cubesatsim_current NONE 11 2 3 Current -Y solar Panel current
21 19 MIN negZi 12 mA cubesatsim_current NONE 12 2 3 Current -Z solar Panel current
22 20 MIN PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Board Voltage Power Supply 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 Pressure STEM Payload Sensor Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude 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 Temperature Internal Temperature of IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 Humidity Humidity
33 31 MIN PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MIN Sensor1 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 33 MIN Sensor2 12 signed raw cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
36 34 MIN ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
37 35 MIN ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
38 36 MIN ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
39 37 MIN rf6 12 - 0 NONE 0 0 0 None None
40 38 MIN rf7 12 - 0 NONE 0 0 0 None None
41 39 MIN MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
42 40 MIN LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
43 41 MIN pad 4 - 34 NONE 0 0 0 None Unused
44 42 MIN IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
45 43 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload Board Failure Indicator
46 44 MIN Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
47 45 MIN expFailure2 1 - 17 NONE 6 7 0 Exp 2 Experiment 2 Failure Indicator
48 46 MIN expFailure3 1 - 17 NONE 6 8 0 Exp 3 Experiment 3 Failure Indicator
49 47 MIN I2CfailureBatt 1 - 17 NONE 2 2 0 Battery I2C Battery I2C Bus failure indicator
50 48 MIN I2CfailurePSU1 1 - 17 NONE 2 3 0 PSU1 I2C PSU2 I2C Bus failure indicator
51 49 MIN I2CfailurePSU2 1 - 17 NONE 2 4 0 PSU2 I2C PSU2 I2C Bus failure indicator
52 50 MIN TLMresets 4 - 1 NONE 2 6 0 Ground Resets Number of times command stations reset stored telemetry
53 51 MIN RxAntDeploy 1 - 16 NONE 1 3 0 RX Antenna 2m Antenna status
54 52 MIN TxAntDeploy 2 - 16 NONE 1 2 0 TX Antenna 70cm Antenna status
55 53 MIN I2CfailureRF 1 - 17 NONE 2 5 0 RF I2C RF I2C Bus failure indicator
56 54 MIN pad1 1 - 0 NONE 0 0 0 NONE Filler
57 55 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
58 56 MIN swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
59 57 MIN hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
60 58 MIN swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
61 59 MIN pad2 28 - 0 NONE 0 0 0 NONE Filler

61
spacecraft/FoxTelem_11a/CubeSatSim_PSK_rttelemetry.csv
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60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,realTime,battCurr,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current
7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload sensor temperature
8,realTime,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar panel voltage
9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar panel voltage
10,realTime,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar panel voltage
11,realTime,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar panel voltage
12,realTime,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar panel voltage
13,realTime,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar panel voltage
14,realTime,posXi,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X solar panel current
15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y solar panel current
16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z solar panel current
17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X solar panel current
18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y solar panel current
19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z solar panel current
20,realTime,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply 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,Pressure,STEM Payload sensor pressure
23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,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,Temperature,Internal temperature of IHU from Pi
27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular veolcity around X Axis
28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular veolcity around Y Axis
29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular veolcity around Z Axis
30,realTime,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
31,realTime,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,realTime,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload extra Sensor 1
33,realTime,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload extra Sensor 2
34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload, STEM Payload STEM Payload board failure indicator
35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,realTime,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,realTime,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,realTime,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
44,realTime,TxAntenna,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
46,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
47,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
48,realTime,rf6,12,-,0,NONE,0,0,0,None,None
49,realTime,rf7,12,-,0,NONE,0,0,0,None,None
50,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
51,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
52,realTime,pad,4,-,34,NONE,0,0,0,None,Unused
53,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler
55,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
56,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
57,realTime,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
58,realTime,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
59,realTime,pad2,28,-,0,NONE,0,0,0,NONE,Filler
1 60 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A Battery A voltage (0-2.5V scale)
3 1 realTime BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 2 3 Cell A+B Battery A+B voltage (0-3.3V scale)
4 2 realTime BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 realTime SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 realTime SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 realTime SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 realTime battCurr 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current
9 7 realTime Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temperature STEM Payload sensor temperature
10 8 realTime posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X solar panel voltage
11 9 realTime posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y solar panel voltage
12 10 realTime posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z solar panel voltage
13 11 realTime negXv 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X solar panel voltage
14 12 realTime negYv 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y solar panel voltage
15 13 realTime negZv 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z solar panel voltage
16 14 realTime posXi 12 mA cubesatsim_current +X Panel 7 2 3 Current +X solar panel current
17 15 realTime posYi 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y solar panel current
18 16 realTime posZi 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z solar panel current
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 3 Current -X solar panel current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 3 Current -Y solar panel current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 3 Current -Z solar panel current
22 20 realTime PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply 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 Pressure STEM Payload sensor pressure
25 23 realTime Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude 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 Temperature Internal temperature of IHU from Pi
29 27 realTime SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation Angular veolcity around X Axis
30 28 realTime SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular veolcity around Y Axis
31 29 realTime SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation Angular veolcity around Z Axis
32 30 realTime Humidity 12 % cubesatsim_temperature Experiments 6 5 3 Humidity Humidity
33 31 realTime PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 realTime Sensor1 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 1 STEM Payload extra Sensor 1
35 33 realTime Sensor2 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 2 STEM Payload extra Sensor 2
36 34 realTime STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload STEM Payload STEM Payload board failure indicator
37 35 realTime Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 realTime PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 realTime PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 realTime I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 realTime I2CBus1Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 realTime I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 realTime CameraFailure 1 - 17 Computer Hardware 2 5 0 Camera Camera failure indicator
44 42 realTime GroundCommands 4 - 1 Computer Software 3 3 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 2 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 realTime ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
48 46 realTime ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
49 47 realTime ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
50 48 realTime rf6 12 - 0 NONE 0 0 0 None None
51 49 realTime rf7 12 - 0 NONE 0 0 0 None None
52 50 realTime MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
53 51 realTime LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
54 52 realTime pad 4 - 34 NONE 0 0 0 None Unused
55 53 realTime IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
56 54 realTime pad1 1 - 0 NONE 0 0 0 NONE Filler
57 55 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 56 realTime swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
59 57 realTime hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
60 58 realTime swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
61 59 realTime pad2 28 - 0 NONE 0 0 0 NONE Filler

13
spacecraft/FoxTelem_11a/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,0,0.1,0,0,0,0,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 0.1 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

47
spacecraft/FoxTelem_11a/CubeSatSim_maxtelemetry.csv
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46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMAX_NAME,DESCRIPTION
0,MAX,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
1,MAX,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
6,MAX,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel
11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel
12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel
13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel
14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel
15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel
16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel
17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage
21,MAX,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MAX,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Sensor 1,STEM Payload Sensor Humidity
31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MAX,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,MAX,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
35,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,MAX,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,MAX,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 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,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,MAX,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,MAX,CameraFailure,1,-,17,NONE,2,5,0,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,Pad,58,-,0,NONE,0,0,0,NONE,NONE
1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMAX_NAME DESCRIPTION
2 0 MAX BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 1 MAX BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A+B Battery A+B voltage (0-3.3V scale)
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MAX TOTAL_BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 MAX PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel
11 9 MAX PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel
12 10 MAX PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y Panel
13 11 MAX PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y Panel
14 12 MAX PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z Panel
15 13 MAX PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z Panel
16 14 MAX PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current +X Panel
17 15 MAX PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current -X Panel
18 16 MAX PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current +Y Panel
19 17 MAX PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel
20 18 MAX PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel
21 19 MAX PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel
22 20 MAX PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Voltage Power Supply 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 bar cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 MAX Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude 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 IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 Temperature Internal Temperature of IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 Sensor 1 STEM Payload Sensor Humidity
33 31 MAX PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MAX Sensor1 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 33 MAX Sensor2 12 signed scaled cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MAX Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 MAX PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 MAX PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 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 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 5 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 Pad 58 - 0 NONE 0 0 0 NONE NONE

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spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv
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46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION
0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel
11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel
12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel
13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel
14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel
15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel
16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel
17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage
21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,STEM Payload Sensor Humidity
31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MIN,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,MIN,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
35,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,MIN,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 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,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,MIN,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,MIN,CameraFailure,1,-,17,NONE,2,5,0,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,Pad,58,-,0,NONE,0,0,0,NONE,NONE
1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMIN_NAME DESCRIPTION
2 0 MIN BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 1 MIN BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A+B Battery A+B voltage (0-3.3V scale)
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MIN TOTAL_BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel
12 10 MIN PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y Panel
13 11 MIN PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y Panel
14 12 MIN PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z Panel
15 13 MIN PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z Panel
16 14 MIN PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current +X Panel
17 15 MIN PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current -X Panel
18 16 MIN PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current +Y Panel
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel
22 20 MIN PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Voltage Power Supply 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 bar cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude 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 IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 Temperature Internal Temperature of IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 Humidity STEM Payload Sensor Humidity
33 31 MIN PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MIN Sensor1 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 33 MIN Sensor2 12 signed scaled cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MIN Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 MIN PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 MIN PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 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 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 5 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 Pad 58 - 0 NONE 0 0 0 NONE NONE

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spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
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46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,RT,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,RT,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel
11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel
12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel
13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel
14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel
15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel
16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel
20,RT,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply 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,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor 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,Temperature,Internal Temperature of IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,STEM Payload Sensor Humidity
31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,RT,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,RT,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload,STEM Payload Board Status
35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,RT,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,RT,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
38,RT,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,RT,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,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,Pad,58,-,0,NONE,0,0,0,NONE,NONE
1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 RT BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 1 RT BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A+B Battery A+B voltage (0-3.3V scale)
4 2 RT BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current
9 7 RT Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X Panel
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X Panel
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y Panel
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y Panel
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z Panel
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z Panel
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current +X Panel
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_current -X Panel 10 2 3 Current -X Panel
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y Panel
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_current -Y Panel 11 2 3 Current -Y Panel
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z Panel
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_current -Z Panel 12 2 3 Current -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply 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 bar cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 RT Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor 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 Temperature Internal Temperature of IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 Humidity STEM Payload Sensor Humidity
33 31 RT PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 RT Sensor1 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 33 RT Sensor2 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
36 34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload STEM Payload Board Status
37 35 RT Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 RT PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 RT PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 RT I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 RT I2CBus1Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 RT CameraFailure 1 - 17 Computer Hardware 2 5 0 Camera Camera failure indicator
44 42 RT GroundCommands 4 - 1 Computer Software 3 3 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 Pad 58 - 0 NONE 0 0 0 NONE NONE

2
systemd/cubesatsim.service
Unescape View File

@ -10,6 +10,8 @@ StandardOutput=inherit
StandardError=inherit StandardError=inherit
Restart=always Restart=always
User=root User=root
CPUAccounting=true
CPUQuota=5%
[Install] [Install]
WantedBy=default.target WantedBy=default.target

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