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18
README.md
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# CubeSatSim
This is the beta release for the new CubeSatSim hardware.
### The hardware files are here:
https://CubeSatSim.org/hardware-beta
<img height=200 width=200 src="https://github.com/alanbjohnston/CubeSatSim/blob/7bdc7b40408baa588a83d360d2112190a803403d/hardware/beta-v1.3.2/cubesatsim-battery-b1.3.2.1b_top.png"><img height=200 width=200 src="https://github.com/alanbjohnston/CubeSatSim/blob/beta/hardware/beta-v1.3.2/cubesatsim-STEM-b1.3.2.1_top.png"><img height=200 width=200 src="https://github.com/alanbjohnston/CubeSatSim/blob/beta/hardware/beta-v1.3.2/cubesatsim-solar-b1.3.2._top.png">
### The wiki instructions are here:
https://github.com/alanbjohnston/CubeSatSim/wiki/v1.3.2-0.-Home.
### The Bill of Materials (BOM) is here:
https://CubeSatSim.org/bom-beta.
### Information about the latest beta software release is here:
https://github.com/alanbjohnston/CubeSatSim/releases
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).
There are several hardware versions and software branches to go with them - see below for information.
@ -44,6 +28,8 @@ See the Wiki Software Install page for details: [https://github.com/alanbjohnsto
CubeSatSim runs on the Bullseye or Buster version of Raspberry Pi OS (Desktop or Lite), although a Pi Zero or Pi Zero W should only run Lite. Your Pi will need to have internet access to update settings and install packages.
*Note:* CubeSatSim expects to be installed as the `pi` user and references many paths in `/home/pi/*`. Installing as a different user will result in configuration files not saving along with many other issues.
To get the software follow these steps:
`sudo apt-get install -y git`

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install
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cd pi-power-button
git checkout v2.0
git checkout master
./script/install

48
spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
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47,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,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,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,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status
46,RT,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
47 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 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 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 C2CStatus 2 - COMMAND_STATUS Computer Software 3 5 0 Command Control Command & Control Status
46 RT Pad 56 - 0 NONE 0 0 0 NONE NONE
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