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Merge pull request #63 from alanbjohnston/rel-cand

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Changes for FoxTelem 1.09 and also +Z to -X mapping bug
pull/77/head
alanbjohnston 5 years ago committed by GitHub
parent 4552282810 a2309c00a7
commit 03de1bb41f
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GPG Key ID: 4AEE18F83AFDEB23
19 changed files with 576 additions and 156 deletions
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59
afsk/main.c
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@ -7,7 +7,6 @@
*
* This program is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or/
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful,
@ -22,6 +21,7 @@
#include <fcntl.h>
#include <stdlib.h>
#include <stdio.h>
#include <unistd.h>
#include <string.h>
#include "status.h"
@ -317,7 +317,10 @@ if (vB4)
snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(0));
}
else if (vB5)
{
{
map[MINUS_X] = PLUS_Z;
map[PLUS_Z] = MINUS_X;
if (access("/dev/i2c-11", W_OK | R_OK) >= 0) { // Test if I2C Bus 11 is present
printf("/dev/i2c-11 is present\n\n");
snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(11));
@ -875,15 +878,18 @@ int get_tlm_fox() {
short int rs_frame[rsFrames][223];
unsigned char parities[rsFrames][parityLen], inputByte;
int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16;
int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; //
int PSUVoltage = 0, PSUCurrent = 0;
int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0;
int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0;
int posXi = 0, negXi = 0, posYi = 0, negYi = 0, posZi = 0, negZi = 0;
int head_offset = 0;
// int xAngularVelocity = (-0.69)*(-10)*(-10) + 45.3 * (-10) + 2078, yAngularVelocity = (-0.69)*(-6)*(-6) + 45.3 * (-6) + 2078, zAngularVelocity = (-0.69)*(6)*(6) + 45.3 * (6) + 2078; // XAxisAngularVelocity
int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0
// int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0
int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0
int RXTemperature = 0;
int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000;
int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048-1501;
short int buffer_test[bufLen];
int buffSize;
@ -1000,12 +1006,12 @@ if (firstTime != ON)
if (mode == BPSK)
h[6] = 99;
posXi = (int)current[map[PLUS_X]] + 2048;
posYi = (int)current[map[PLUS_Y]] + 2048;
posZi = (int)current[map[PLUS_Z]] + 2048;
negXi = (int)current[map[MINUS_X]] + 2048;
negYi = (int)current[map[MINUS_Y]] + 2048;
negZi = (int)current[map[MINUS_Z]] + 2048;
posXi = (int)(current[map[PLUS_X]] + 0.5) + 2048;
posYi = (int)(current[map[PLUS_Y]] + 0.5) + 2048;
posZi = (int)(current[map[PLUS_Z]] + 0.5) + 2048;
negXi = (int)(current[map[MINUS_X]] + 0.5) + 2048;
negYi = (int)(current[map[MINUS_Y]] + 0.5) + 2048;
negZi = (int)(current[map[MINUS_Z]] + 0.5) + 2048;
posXv = (int)(voltage[map[PLUS_X]] * 100);
posYv = (int)(voltage[map[PLUS_Y]] * 100);
@ -1014,9 +1020,9 @@ if (firstTime != ON)
negYv = (int)(voltage[map[MINUS_Y]] * 100);
negZv = (int)(voltage[map[MINUS_Z]] * 100);
batt_c_v = (int)(voltage[map[BAT]] * 100);
battCurr = (int)current[map[BAT]] + 2048;
battCurr = (int)(current[map[BAT]] + 0.5) + 2048;
PSUVoltage = (int)(voltage[map[BUS]] * 100);
PSUCurrent = (int)current[map[BUS]] + 2048;
PSUCurrent = (int)(current[map[BUS]] + 0.5) + 2048;
if (payload == ON)
STEMBoardFailure = 0;
@ -1104,16 +1110,23 @@ if (payload == ON)
gyroZ = atof(token);
printf("gyroZ %f \n", gyroZ);
}
xAngularVelocity = (-0.69)*(gyroX)*(gyroX) + 45.3 * (gyroX) + 2078;
yAngularVelocity = (-0.69)*(gyroY)*(gyroY) + 45.3 * (gyroY) + 2078;
zAngularVelocity = (-0.69)*(gyroZ)*(gyroZ) + 45.3 * (gyroZ) + 2078;
xAngularVelocity = (int)(gyroX + 0.5) + 2048;
yAngularVelocity = (int)(gyroY + 0.5) + 2048;
zAngularVelocity = (int)(gyroZ + 0.5) + 2048;
}
encodeA(b, 0 + head_offset, batt_a_v);
encodeB(b, 1 + head_offset, batt_b_v);
encodeA(b, 3 + head_offset, batt_c_v);
encodeB(b, 4 + head_offset,xAccel); // Xaccel
encodeA(b, 6 + head_offset,yAccel); //Yaccel
encodeB(b, 7 + head_offset,zAccel); //Zaccel
encodeA(b, 9 + head_offset, battCurr);
encodeB(b, 10 + head_offset,temp); // Temp
if (mode == FSK)
{
@ -1149,16 +1162,24 @@ if (payload == ON)
}
encodeA(b, 30 + head_offset,PSUVoltage);
encodeB(b, 46 + head_offset,PSUCurrent);
encodeA(b, 33 + head_offset,pressure); // Pressure
encodeB(b, 34 + head_offset,altitude); // Altitude
encodeA(b, 36 + head_offset, RXTemperature);
encodeA(b, 39 + head_offset, IHUcpuTemp);
encodeB(b, 40 + head_offset, xAngularVelocity);
encodeA(b, 42 + head_offset, yAngularVelocity);
encodeB(b, 43 + head_offset, zAngularVelocity);
encodeA(b, 45 + head_offset, sensor1);
encodeB(b, 46 + head_offset,PSUCurrent);
encodeA(b, 48 + head_offset, sensor2);
encodeB(b, 49 + head_offset, sensor3);
encodeB(b, 51 + head_offset, STEMBoardFailure);
encodeA(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure * 2 + groundCommandCount * 256);
encodeB(b, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed* 2);
short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)];
short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)];

5
afsk/telem.c
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@ -105,12 +105,13 @@ int main(int argc, char *argv[]) {
if (digitalRead(26) != HIGH)
{
printf("vB5 Present\n"); // Don't print normal board detection
map[MINUS_X] = PLUS_Z;
map[PLUS_Z] = MINUS_X;
snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(3));
printf("New Bus String: %s \n", busStr);
/*
if (test_i2c_bus(0) != OFF)
if (test_i2c_b0) != OFF)
strcpy(busStr,"1 ");
else
strcpy(busStr,"-1 ");

13
spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type1_HEALTH.frame
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@ -0,0 +1,13 @@
number_of_payloads=6
payload0.name=rttelemetry
payload0.length=78
payload1.name=rttelemetry
payload1.length=78
payload2.name=rttelemetry
payload2.length=78
payload3.name=rttelemetry
payload3.length=78
payload4.name=rttelemetry
payload4.length=78
payload5.name=wodtelemetry
payload5.length=78

13
spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame
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@ -0,0 +1,13 @@
number_of_payloads=6
payload0.name=rttelemetry
payload0.length=78
payload1.name=rttelemetry
payload1.length=78
payload2.name=rttelemetry
payload2.length=78
payload3.name=maxtelemetry
payload3.length=78
payload4.name=mintelemetry
payload4.length=78
payload5.name=wodtelemetry
payload5.length=78

61
spacecraft/FoxTelem_1.09m/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,4,2,4,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,7,2,4,Current,+X solar Panel current
15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,4,Current,+Y solar Panel current
16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,4,Current,+Z solar Panel current
17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,4,Current,-X solar Panel current
18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,4,Current,-Y solar Panel current
19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,4,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,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,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,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,MAX,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
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 4 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 4 Current +X solar Panel current
17 15 MAX posYi 12 mA cubesatsim_current NONE 8 2 4 Current +Y solar Panel current
18 16 MAX posZi 12 mA cubesatsim_current NONE 9 2 4 Current +Z solar Panel current
19 17 MAX negXi 12 mA cubesatsim_current NONE 10 2 4 Current -X solar Panel current
20 18 MAX negYi 12 mA cubesatsim_current NONE 11 2 4 Current -Y solar Panel current
21 19 MAX negZi 12 mA cubesatsim_current NONE 12 2 4 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 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 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 Sensor1 12 raw cubesatsim_sensor1|INT NONE 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 MAX PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MAX Sensor2 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 MAX Sensor3 12 signed raw cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
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_1.09m/CubeSatSim_PSK_mintelemetry.csv
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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,4,2,4,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,7,2,4,Current,+X solar Panel current
15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,4,Current,+Y solar Panel current
16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,4,Current,+Z solar Panel current
17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,4,Current,-X solar Panel current
18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,4,Current,-Y solar Panel current
19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,4,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,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,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,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
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 4 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 4 Current +X solar Panel current
17 15 MIN posYi 12 mA cubesatsim_current NONE 8 2 4 Current +Y solar Panel current
18 16 MIN posZi 12 mA cubesatsim_current NONE 9 2 4 Current +Z solar Panel current
19 17 MIN negXi 12 mA cubesatsim_current NONE 10 2 4 Current -X solar Panel current
20 18 MIN negYi 12 mA cubesatsim_current NONE 11 2 4 Current -Y solar Panel current
21 19 MIN negZi 12 mA cubesatsim_current NONE 12 2 4 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 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 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 Sensor1 12 raw cubesatsim_sensor1|INT NONE 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 MIN PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MIN Sensor2 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 MIN Sensor3 12 signed raw cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
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_1.09m/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,4,2,4,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,7,2,4,Current,+X solar panel current
15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar panel current
16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar panel current
17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar panel current
18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar panel current
19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,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,bar,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,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload extra Sensor 1
31,realTime,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload extra Sensor 2
33,realTime,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload extra Sensor 3
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 4 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 4 Current +X solar panel current
17 15 realTime posYi 12 mA cubesatsim_current +Y Panel 8 2 4 Current +Y solar panel current
18 16 realTime posZi 12 mA cubesatsim_current +Z Panel 9 2 4 Current +Z solar panel current
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 4 Current -X solar panel current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 4 Current -Y solar panel current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 4 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 bar 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 Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload extra Sensor 1
33 31 realTime PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 realTime Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload extra Sensor 2
35 33 realTime Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload extra Sensor 3
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

62
spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv
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61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,WOD,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,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current
7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage
9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage
10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage
11,WOD,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage
12,WOD,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage
13,WOD,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage
14,WOD,posXi,12,mA,cubesatsim_current,+X Panel,7,2,4,Current,+X solar Panel current
15,WOD,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar Panel current
16,WOD,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar Panel current
17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current
18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current
19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current
20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage
21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude
24,WOD,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,WOD,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication
26,WOD,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU
27,WOD,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
28,WOD,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
29,WOD,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,WOD,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,WOD,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
38,WOD,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,WOD,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,WOD,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,WOD,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
42,WOD,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
43,WOD,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
44,WOD,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
45,WOD,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
46,WOD,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
47,WOD,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
48,WOD,rf6,12,-,0,NONE,0,0,0,None,None
49,WOD,rf7,12,-,0,NONE,0,0,0,None,None
50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused
53,WOD,WODTimeStampReset,16,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected
54,WOD,pad1,17,-,0,NONE,0,0,0,NONE,Filler
55,WOD,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,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
57,WOD,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
58,WOD,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
59,WOD,WODTimeStampUpTime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected
60,WOD,pad2,3,-,0,NONE,0,0,0,NONE,Filler
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 WOD BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A Battery A voltage (0-2.5V scale)
3 1 WOD 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 WOD 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 WOD SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 WOD SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 WOD SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 WOD battCurr 12 mA cubesatsim_current Battery 4 2 4 Current Total Battery DC current
9 7 WOD Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 WOD posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X solar Panel voltage
11 9 WOD posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y solar Panel voltage
12 10 WOD posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z solar Panel voltage
13 11 WOD negXv 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X solar Panel voltage
14 12 WOD negYv 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y solar Panel voltage
15 13 WOD negZv 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z solar Panel voltage
16 14 WOD posXi 12 mA cubesatsim_current +X Panel 7 2 4 Current +X solar Panel current
17 15 WOD posYi 12 mA cubesatsim_current +Y Panel 8 2 4 Current +Y solar Panel current
18 16 WOD posZi 12 mA cubesatsim_current +Z Panel 9 2 4 Current +Z solar Panel current
19 17 WOD negXi 12 mA cubesatsim_current -X Panel 10 2 4 Current -X solar Panel current
20 18 WOD negYi 12 mA cubesatsim_current -Y Panel 11 2 4 Current -Y solar Panel current
21 19 WOD negZi 12 mA cubesatsim_current -Z Panel 12 2 4 Current -Z solar Panel current
22 20 WOD PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage
23 21 WOD spin 12 rpm 12 Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 WOD Pressure 12 bar cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 WOD Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor Altitude
26 24 WOD Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 WOD rssi 12 dBm 14 Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 WOD IHUcpuTemp 12 C cubesatsim_temperature Computer Hardware 2 1 3 Temperature Internal Temperature of IHU
29 27 WOD SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation Angular Veolcity around X Axis
30 28 WOD SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 WOD SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 WOD Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 WOD PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 WOD Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 WOD Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 WOD STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload Board Failure Indicator
37 35 WOD Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 WOD PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 WOD PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 WOD I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 WOD I2CBus1Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 WOD I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 WOD CameraFailure 1 - 17 Computer Hardware 2 5 0 Camera Camera failure indicator
44 42 WOD GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 43 WOD RxAntDeploy 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 WOD TxAntDeploy 2 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 WOD ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
48 46 WOD ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
49 47 WOD ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
50 48 WOD rf6 12 - 0 NONE 0 0 0 None None
51 49 WOD rf7 12 - 0 NONE 0 0 0 None None
52 50 WOD MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
53 51 WOD LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
54 52 WOD pad 4 - 34 NONE 0 0 0 None Unused
55 53 WOD WODTimeStampReset 16 - 1 NONE 0 0 0 MAX Timestamp Uptime Time Whole Orbit Data was collected
56 54 WOD pad1 17 - 0 NONE 0 0 0 NONE Filler
57 55 WOD 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 WOD swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
59 57 WOD hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
60 58 WOD swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
61 59 WOD WODTimeStampUpTime 25 s 1 NONE 0 0 0 MAX Timestamp Uptime Time Whole Orbit Data was collected
62 60 WOD pad2 3 - 0 NONE 0 0 0 NONE Filler

13
spacecraft/FoxTelem_1.09m/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

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spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv
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39,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MAX,BATT_A_V,12,V,4,NONE,0,0,0,NONE,Battery pair A high voltage raw value (0-2.5V scale)
1,MAX,BATT_B_V,12,V,4,NONE,0,0,0,NONE,Battery pair B high voltage raw value (0-3.3V scale)
2,MAX,BATT_C_V,12,V,4,NONE,0,0,0,NONE,Battery pair C high voltage raw value (0-5.0V scale)
3,MAX,BATT_A_T,12,C,8,NONE,0,0,0,NONE,Battery pair A high temperature raw value
4,MAX,BATT_B_T,12,C,8,NONE,0,0,0,NONE,Battery pair B high temperature raw value
5,MAX,BATT_C_T,12,C,8,NONE,0,0,0,NONE,Battery pair C high temperature raw value
6,MAX,TOTAL_BATT_I,12,mA,9,NONE,0,0,0,NONE,Battery DC high current raw value
7,MAX,BATTBoardTemperature,12,C,8,NONE,0,0,0,NONE,High PC Board Temperature of BATT raw value
8,MAX,PANEL_PLUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME?
9,MAX,PANEL_MINUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME?
10,MAX,PANEL_PLUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME?
11,MAX,PANEL_MINUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME?
12,MAX,PANEL_PLUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME?
13,MAX,PANEL_MINUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME?
14,MAX,PANEL_PLUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME?
15,MAX,PANEL_MINUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME?
16,MAX,PANEL_PLUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME?
17,MAX,PANEL_MINUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME?
18,MAX,PANEL_PLUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME?
19,MAX,PANEL_MINUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME?
20,MAX,PSUTemperature,12,C,7,NONE,0,0,0,NONE,PSU card high temperature raw value
21,MAX,SPIN,12,rpm,12,NONE,0,0,0,NONE,Highest calculated spin rate RPM using solar cells
22,MAX,TXPACurrent,12,mA,10,NONE,0,0,0,NONE,Transmit power amplifier high current raw value
23,MAX,TXTemperature,12,C,7,NONE,0,0,0,NONE,Transmitter card high temperature raw value
24,MAX,RXTemperature,12,C,7,NONE,0,0,0,NONE,Receiver card high temperature raw value
25,MAX,RSSI,12,dBm,14,NONE,0,0,0,NONE,High Received Signal Strength Indication raw value
26,MAX,IHUTemperature,12,C,15,NONE,0,0,0,NONE,High CPU Temperature of IHU raw value
27,MAX,SatelliteXAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle
28,MAX,SatelliteYAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle
29,MAX,SatelliteZAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle
30,MAX,EXP4Temperature,12,C,7,NONE,0,0,0,NONE,LBand Uplink card temperature raw value
31,MAX,PSUCurrent,12,mA,22,NONE,0,0,0,NONE,PSU DC high current
32,MAX,IHUHardErrorData,32,-,19,NONE,2,8,0,Hard Error,Diagnostic Data on IHU Hard Errors
33,MAX,MaxTimestampResetCount,16,-,1,NONE,0,0,0,NONE,Total number of times IHU has reset since initial on-orbit startup
34,MAX,MaxTimestampUptime,25,-,1,NONE,0,0,0,NONE,This is the IHU uptime in seconds since the last reset
35,MAX,SafeModeIndication,1,-,21,NONE,2,10,0,Safe Mode,State: 1 = Safe Mode Active
36,MAX,AutoSafeModeActive,1,-,21,NONE,2,11,0,Auto Safe Mode,State: 1 = Auto Safe Mode Active
37,MAX,AutoSafeModeAllowed,1,-,21,NONE,2,12,0,Auto Safe Allowed,State: 1 = Auto Safe Mode Allowed
38,MAX,Pad,20,-,0,NONE,0,0,0,NONE,NONE
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,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,MAX,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
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 39 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME SHOMAX_NAME DESCRIPTION
2 0 MAX BATT_A_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 0 0 3 NONE Cell A Battery pair A high voltage raw value (0-2.5V scale) Battery A voltage (0-2.5V scale)
3 1 MAX BATT_B_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 0 0 3 NONE Cell A+B Battery pair B high voltage raw value (0-3.3V scale) Battery A+B voltage (0-3.3V scale)
4 2 MAX BATT_C_V BATT_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 4 0 1 0 3 NONE Cell A+B+C Voltage Battery pair C high voltage raw value (0-5.0V scale) Battery A+B+C voltage (0-5.0V scale)
5 3 MAX BATT_A_T SatelliteXAxisAcceleration 12 C g 8 cubesatsim_acceleration|FLOAT2 NONE 0 7 0 4 0 3 NONE Acceleration Battery pair A high temperature raw value Acceleration around X Axis
6 4 MAX BATT_B_T SatelliteYAxisAcceleration 12 C g 8 cubesatsim_acceleration|FLOAT2 NONE 0 8 0 4 0 3 NONE Acceleration Battery pair B high temperature raw value Acceleration around Y Axis
7 5 MAX BATT_C_T SatelliteZAxisAcceleration 12 C g 8 cubesatsim_acceleration|FLOAT2 NONE 0 9 0 4 0 3 NONE Acceleration Battery pair C high temperature raw value Acceleration around Z Axis
8 6 MAX TOTAL_BATT_I 12 mA 9 cubesatsim_current NONE 0 4 0 2 0 3 NONE Current Battery DC high current raw value Total Battery DC current
9 7 MAX BATTBoardTemperature Temperature 12 C 8 cubesatsim_temperature NONE 0 6 0 2 0 3 NONE Temperature High PC Board Temperature of BATT raw value STEM Payload Sensor Temperature
10 8 MAX PANEL_PLUS_X_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 7 0 1 0 3 NONE Voltage #NAME? +X Panel
11 9 MAX PANEL_MINUS_X_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 10 0 1 0 3 NONE Voltage #NAME? -X Panel
12 10 MAX PANEL_PLUS_Y_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 8 0 1 0 3 NONE Voltage #NAME? +Y Panel
13 11 MAX PANEL_MINUS_Y_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 11 0 1 0 3 NONE Voltage #NAME? -Y Panel
14 12 MAX PANEL_PLUS_Z_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 9 0 1 0 3 NONE Voltage #NAME? +Z Panel
15 13 MAX PANEL_MINUS_Z_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 12 0 1 0 3 NONE Voltage #NAME? -Z Panel
16 14 MAX PANEL_PLUS_X_T PANEL_PLUS_X_I 12 C mA 6 cubesatsim_current NONE 0 7 0 2 0 3 NONE Current #NAME? +X Panel
17 15 MAX PANEL_MINUS_X_T PANEL_MINUS_X_I 12 C mA 6 cubesatsim_current NONE 0 10 0 2 0 3 NONE Current #NAME? -X Panel
18 16 MAX PANEL_PLUS_Y_T PANEL_PLUS_Y_I 12 C mA 6 cubesatsim_current NONE 0 8 0 2 0 3 NONE Current #NAME? +Y Panel
19 17 MAX PANEL_MINUS_Y_T PANEL_MINUS_Y_I 12 C mA 6 cubesatsim_current NONE 0 11 0 2 0 3 NONE Current #NAME? -Y Panel
20 18 MAX PANEL_PLUS_Z_T PANEL_PLUS_Z_I 12 C mA 6 cubesatsim_current NONE 0 9 0 2 0 3 NONE Current #NAME? +Z Panel
21 19 MAX PANEL_MINUS_Z_T PANEL_MINUS_Z_I 12 C mA 6 cubesatsim_current NONE 0 12 0 2 0 3 NONE Current #NAME? -Z Panel
22 20 MAX PSUTemperature PSUVoltage 12 C V 7 cubesatsim_voltage|FLOAT2 NONE 0 5 0 1 0 3 NONE Voltage PSU card high temperature raw value Power Supply Voltage
23 21 MAX SPIN 12 rpm 12 cubesatsim_rpm NONE 0 3 0 1 0 3 NONE Spacecraft Spin Highest calculated spin rate RPM using solar cells Calculated spin rate using solar cells
24 22 MAX TXPACurrent Pressure 12 mA bar 10 cubesatsim_pressure NONE 0 6 0 3 0 3 NONE Pressure Transmit power amplifier high current raw value STEM Payload Sensor Pressure
25 23 MAX TXTemperature Altitude 12 C m 7 cubesatsim_altitude NONE 0 6 0 4 0 3 NONE Altitude Transmitter card high temperature raw value STEM Payload Sensor Altitude
26 24 MAX RXTemperature Resets 12 C - 7 12 NONE 0 3 0 2 0 3 NONE Reset Count Receiver card high temperature raw value Software Reset Count
27 25 MAX RSSI 12 dBm 14 cubesatsim_rssi|INT NONE 0 1 0 1 0 3 NONE RSSI High Received Signal Strength Indication raw value Received Signal Strength Indication
28 26 MAX IHUTemperature 12 C 15 cubesatsim_temperature NONE 0 2 0 1 0 3 NONE Temperature High CPU Temperature of IHU raw value Internal Temperature of IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 7 0 3 0 3 NONE Rotation Highest Raw Angle Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 8 0 3 0 3 NONE Rotation Highest Raw Angle Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 9 0 3 0 3 NONE Rotation Highest Raw Angle Angular Veolcity around Z Axis
32 30 MAX EXP4Temperature Sensor1 12 C raw 7 cubesatsim_sensor1|INT NONE 0 6 0 5 0 3 NONE Sensor 1 LBand Uplink card temperature raw value STEM Payload Extra Sensor 1
33 31 MAX PSUCurrent 12 mA 22 cubesatsim_current NONE 0 5 0 2 0 3 NONE Current PSU DC high current Power Supply DC Current
34 32 MAX IHUHardErrorData Sensor2 32 12 - signed raw 19 cubesatsim_sensor2|INT NONE 2 6 8 6 0 3 Hard Error Sensor 2 Diagnostic Data on IHU Hard Errors STEM Payload Extra Sensor 2
35 33 MAX MaxTimestampResetCount Sensor3 16 12 - signed scaled 1 cubesatsim_sensor3|FLOAT2 NONE 0 6 0 7 0 3 NONE Sensor 3 Total number of times IHU has reset since initial on-orbit startup STEM Payload Extra Sensor 3
36 34 MAX MaxTimestampUptime STEMPayloadStatus 25 1 - 1 17 NONE 0 6 0 1 0 NONE STEM Payload Status This is the IHU uptime in seconds since the last reset STEM Payload Board Status
37 35 MAX SafeModeIndication Nominal Mode 1 - 21 17 NONE 2 3 10 2 0 Safe Mode Nominal Mode State: 1 = Safe Mode Active Nominal Mode (Not Safe Mode)
38 36 MAX AutoSafeModeActive PayloadStatus1 1 - 21 17 NONE 2 6 11 7 0 Auto Safe Mode Exp 2 State: 1 = Auto Safe Mode Active STEM Payload status 1 failure indicator
39 37 MAX AutoSafeModeAllowed PayloadStatus2 1 - 21 17 NONE 2 6 12 8 0 Auto Safe Allowed Exp 3 State: 1 = Auto Safe Mode Allowed STEM Payload status 2 failure indicator
40 38 MAX Pad I2CBus0Failure 20 1 - 0 17 NONE 0 2 0 2 0 NONE I2C Bus 0 NONE 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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39,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MIN,BATT_A_V,12,V,4,NONE,0,0,0,NONE,Battery pair A low voltage raw value (0-2.5V scale)
1,MIN,BATT_B_V,12,V,4,NONE,0,0,0,NONE,Battery pair B low voltage raw value (0-3.3V scale)
2,MIN,BATT_C_V,12,V,4,NONE,0,0,0,NONE,Battery pair C low voltage raw value (0-5.0V scale)
3,MIN,BATT_A_T,12,T,8,NONE,0,0,0,NONE,Battery pair A low temperature raw value
4,MIN,BATT_B_T,12,T,8,NONE,0,0,0,NONE,Battery pair B low temperature raw value
5,MIN,BATT_C_T,12,T,8,NONE,0,0,0,NONE,Battery pair C low temperature raw value
6,MIN,TOTAL_BATT_I,12,mA,9,NONE,0,0,0,NONE,Battery DC low current raw value
7,MIN,BATTBoardTemperature,12,C,8,NONE,0,0,0,NONE,Low PC Board Temperature of BATT raw value
8,MIN,PANEL_PLUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME?
9,MIN,PANEL_MINUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME?
10,MIN,PANEL_PLUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME?
11,MIN,PANEL_MINUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME?
12,MIN,PANEL_PLUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME?
13,MIN,PANEL_MINUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME?
14,MIN,PANEL_PLUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME?
15,MIN,PANEL_MINUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME?
16,MIN,PANEL_PLUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME?
17,MIN,PANEL_MINUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME?
18,MIN,PANEL_PLUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME?
19,MIN,PANEL_MINUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME?
20,MIN,PSUTemperature,12,C,7,NONE,0,0,0,NONE,PSU card low temperature raw value
21,MIN,SPIN,12,rpm,12,NONE,0,0,0,NONE,Lowest calculated spin rate RPM using solar cells
22,MIN,TXPACurrent,12,mA,10,NONE,0,0,0,NONE,Transmit power amplifier low current raw value
23,MIN,TXTemperature,12,C,7,NONE,0,0,0,NONE,Transmitter card low temperature raw value
24,MIN,RXTemperature,12,C,7,NONE,0,0,0,NONE,Receiver card low temperature raw value
25,MIN,RSSI,12,dBm,14,NONE,0,0,0,NONE,Low Received Signal Strength Indication raw value
26,MIN,IHUTemperature,12,C,15,NONE,0,0,0,NONE,Low CPU Temperature of IHU raw value
27,MIN,SatelliteXAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle
28,MIN,SatelliteYAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle
29,MIN,SatelliteZAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle
30,MIN,EXP4Temperature,12,C,7,NONE,0,0,0,NONE,Experiment 4 card low temperature raw value
31,MIN,PSUCurrent,12,mA,11,NONE,0,0,0,NONE,PSU DC low current
32,MIN,IHUSoftErrorData,32,-,20,NONE,2,9,0,Soft Error,Diagnostic Data on IHU Soft Errors
33,MIN,MinTimestampResetCount,16,-,1,NONE,0,0,0,NONE,Total number of times IHU has reset since initial on-orbit startup
34,MIN,MinTimestampUptime,25,-,1,NONE,0,0,0,NONE,This is the IHU uptime in seconds since the last reset
35,MIN,SafeModeIndication,1,-,21,NONE,0,0,0,NONE,State: 1 = Safe Mode Active
36,MIN,AutoSafeModeActive,1,-,21,NONE,0,0,0,NONE,State: 1 = Auto Safe Mode Active
37,MIN,AutoSafeModeAllowed,1,-,21,NONE,0,0,0,NONE,State: 1 = Auto Safe Mode Allowed
38,MIN,Pad,20,-,0,NONE,0,0,0,NONE,NONE
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,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,MIN,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
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 39 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME SHOMIN_NAME DESCRIPTION
2 0 MIN BATT_A_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 0 0 3 NONE Cell A Battery pair A low voltage raw value (0-2.5V scale) Battery A voltage (0-2.5V scale)
3 1 MIN BATT_B_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 0 0 3 NONE Cell A+B Battery pair B low voltage raw value (0-3.3V scale) Battery A+B voltage (0-3.3V scale)
4 2 MIN BATT_C_V BATT_V 12 V 4 cubesatsim_voltage|FLOAT2 NONE 0 4 0 1 0 3 NONE Cell A+B+C Voltage Battery pair C low voltage raw value (0-5.0V scale) Battery A+B+C voltage (0-5.0V scale)
5 3 MIN BATT_A_T SatelliteXAxisAcceleration 12 T g 8 cubesatsim_acceleration|FLOAT2 NONE 0 7 0 4 0 3 NONE Acceleration Battery pair A low temperature raw value Acceleration around X Axis
6 4 MIN BATT_B_T SatelliteYAxisAcceleration 12 T g 8 cubesatsim_acceleration|FLOAT2 NONE 0 8 0 4 0 3 NONE Acceleration Battery pair B low temperature raw value Acceleration around Y Axis
7 5 MIN BATT_C_T SatelliteZAxisAcceleration 12 T g 8 cubesatsim_acceleration|FLOAT2 NONE 0 9 0 4 0 3 NONE Acceleration Battery pair C low temperature raw value Acceleration around Z Axis
8 6 MIN TOTAL_BATT_I 12 mA 9 cubesatsim_current NONE 0 4 0 2 0 3 NONE Current Battery DC low current raw value Total Battery DC current
9 7 MIN BATTBoardTemperature Temperature 12 C 8 cubesatsim_temperature NONE 0 6 0 2 0 3 NONE Temperature Low PC Board Temperature of BATT raw value STEM Payload Sensor Temperature
10 8 MIN PANEL_PLUS_X_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 7 0 1 0 3 NONE Voltage #NAME? +X Panel
11 9 MIN PANEL_MINUS_X_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 10 0 1 0 3 NONE Voltage #NAME? -X Panel
12 10 MIN PANEL_PLUS_Y_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 8 0 1 0 3 NONE Voltage #NAME? +Y Panel
13 11 MIN PANEL_MINUS_Y_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 11 0 1 0 3 NONE Voltage #NAME? -Y Panel
14 12 MIN PANEL_PLUS_Z_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 9 0 1 0 3 NONE Voltage #NAME? +Z Panel
15 13 MIN PANEL_MINUS_Z_V 12 V 5 cubesatsim_voltage|FLOAT2 NONE 0 12 0 1 0 3 NONE Voltage #NAME? -Z Panel
16 14 MIN PANEL_PLUS_X_T PANEL_PLUS_X_I 12 C mA 6 cubesatsim_current NONE 0 7 0 2 0 3 NONE Current #NAME? +X Panel
17 15 MIN PANEL_MINUS_X_T PANEL_MINUS_X_I 12 C mA 6 cubesatsim_current NONE 0 10 0 2 0 3 NONE Current #NAME? -X Panel
18 16 MIN PANEL_PLUS_Y_T PANEL_PLUS_Y_I 12 C mA 6 cubesatsim_current NONE 0 8 0 2 0 3 NONE Current #NAME? +Y Panel
19 17 MIN PANEL_MINUS_Y_T PANEL_MINUS_Y_I 12 C mA 6 cubesatsim_current NONE 0 11 0 2 0 3 NONE Current #NAME? -Y Panel
20 18 MIN PANEL_PLUS_Z_T PANEL_PLUS_Z_I 12 C mA 6 cubesatsim_current NONE 0 9 0 2 0 3 NONE Current #NAME? +Z Panel
21 19 MIN PANEL_MINUS_Z_T PANEL_MINUS_Z_I 12 C mA 6 cubesatsim_current NONE 0 12 0 2 0 3 NONE Current #NAME? -Z Panel
22 20 MIN PSUTemperature PSUVoltage 12 C V 7 cubesatsim_voltage|FLOAT2 NONE 0 5 0 1 0 3 NONE Voltage PSU card low temperature raw value Power Supply Voltage
23 21 MIN SPIN 12 rpm 12 cubesatsim_rpm NONE 0 3 0 1 0 3 NONE Spacecraft Spin Lowest calculated spin rate RPM using solar cells Calculated spin rate using solar cells
24 22 MIN TXPACurrent Pressure 12 mA bar 10 cubesatsim_pressure NONE 0 6 0 3 0 3 NONE Pressure Transmit power amplifier low current raw value STEM Payload Sensor Pressure
25 23 MIN TXTemperature Altitude 12 C m 7 cubesatsim_altitude NONE 0 6 0 4 0 3 NONE Altitude Transmitter card low temperature raw value STEM Payload Sensor Altitude
26 24 MIN RXTemperature Resets 12 C - 7 12 NONE 0 3 0 2 0 3 NONE Reset Count Receiver card low temperature raw value Software Reset Count
27 25 MIN RSSI 12 dBm 14 cubesatsim_rssi|INT NONE 0 1 0 1 0 3 NONE RSSI Low Received Signal Strength Indication raw value Received Signal Strength Indication
28 26 MIN IHUTemperature 12 C 15 cubesatsim_temperature NONE 0 2 0 1 0 3 NONE Temperature Low CPU Temperature of IHU raw value Internal Temperature of IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 7 0 3 0 3 NONE Rotation Lowest Raw Angle Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 8 0 3 0 3 NONE Rotation Lowest Raw Angle Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps 13 cubesatsim_rotation|INT NONE 0 9 0 3 0 3 NONE Rotation Lowest Raw Angle Angular Veolcity around Z Axis
32 30 MIN EXP4Temperature Sensor1 12 C raw 7 cubesatsim_sensor1|INT NONE 0 6 0 5 0 3 NONE Sensor 1 Experiment 4 card low temperature raw value STEM Payload Extra Sensor 1
33 31 MIN PSUCurrent 12 mA 11 cubesatsim_current NONE 0 5 0 2 0 3 NONE Current PSU DC low current Power Supply DC Current
34 32 MIN IHUSoftErrorData Sensor2 32 12 - signed raw 20 cubesatsim_sensor2|INT NONE 2 6 9 6 0 3 Soft Error Sensor 2 Diagnostic Data on IHU Soft Errors STEM Payload Extra Sensor 2
35 33 MIN MinTimestampResetCount Sensor3 16 12 - signed scaled 1 cubesatsim_sensor3|FLOAT2 NONE 0 6 0 7 0 3 NONE Sensor 3 Total number of times IHU has reset since initial on-orbit startup STEM Payload Extra Sensor 3
36 34 MIN MinTimestampUptime STEMPayloadStatus 25 1 - 1 17 NONE 0 6 0 1 0 NONE STEM Payload Status This is the IHU uptime in seconds since the last reset STEM Payload Board Status
37 35 MIN SafeModeIndication Nominal Mode 1 - 21 17 NONE 0 3 0 2 0 NONE Nominal Mode State: 1 = Safe Mode Active Nominal Mode (Not Safe Mode)
38 36 MIN AutoSafeModeActive PayloadStatus1 1 - 21 17 NONE 0 6 0 7 0 NONE Exp 2 State: 1 = Auto Safe Mode Active STEM Payload status 1 failure indicator
39 37 MIN AutoSafeModeAllowed PayloadStatus2 1 - 21 17 NONE 0 6 0 8 0 NONE Exp 3 State: 1 = Auto Safe Mode Allowed STEM Payload status 2 failure indicator
40 38 MIN Pad I2CBus0Failure 20 1 - 0 17 NONE 0 2 0 2 0 NONE I2C Bus 0 NONE 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_1.09m/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,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,RT,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
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 Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 RT PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 RT Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 RT Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
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

45
spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
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@ -1,45 +0,0 @@
44,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,3,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale)
3,RT,BATT_A_T,12,C,8,NONE,0,0,3,Temperature A,Battery pair A temperature
4,RT,BATT_B_T,12,C,8,NONE,0,0,3,Temperature B,Battery pair B temperature
5,RT,BATT_C_T,12,C,8,NONE,0,0,3,Temperature C,Battery pair C temperature
6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current
7,RT,BATTBoardTemperature,12,C,8,NONE,0,0,3,Board Temp,Battery Card Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel
11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,10,2,3,Voltage,-Y Panel
12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,8,2,3,Voltage,+Z Panel
13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,11,2,3,Voltage,-Z Panel
14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,6,1,3,Current,+X Panel
15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,9,1,3,Current,-X Panel
16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,7,1,3,Current,+Y Panel
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,10,1,3,Current,-Y Panel
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,8,1,3,Current,+Z Panel
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel
20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage
21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells
22,RT,TXPACurrent,12,mA,10,NONE,1,0,3,PA Current,Transmit power amplifier current
23,RT,TXTemperature,12,C,7,NONE,1,0,3,TX Temperature,Transmitter card temperature
24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature
25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication
26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,EXP4Temperature,12,C,7,NONE,5,0,0,EXP4 Temperature,Not used
31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current
32,RT,IHUDiagnosticData,32,-,18,NONE,2,7,0,Diagnostic Info,Diagnostic Data on IHU Performance
33,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status
34,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
35,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
36,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
37,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator
38,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator
39,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator
40,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
41,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status
42,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status
43,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE
1 44 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 RT BATT_A_V 12 V 4 NONE 0 0 3 Cell A Battery pair A voltage (0-2.5V scale)
3 1 RT BATT_B_V 12 V 4 NONE 0 0 3 Cell A + B Battery pairs A+B voltage (0-3.3V scale)
4 2 RT BATT_V 12 V cubesatsim_ina219_voltage Battery 3 1 3 Cell A + B + C Battery A+B+C voltage (0-5.0V scale)
5 3 RT BATT_A_T 12 C 8 NONE 0 0 3 Temperature A Battery pair A temperature
6 4 RT BATT_B_T 12 C 8 NONE 0 0 3 Temperature B Battery pair B temperature
7 5 RT BATT_C_T 12 C 8 NONE 0 0 3 Temperature C Battery pair C temperature
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_ina219_current Battery 3 2 3 Current Total Battery DC current
9 7 RT BATTBoardTemperature 12 C 8 NONE 0 0 3 Board Temp Battery Card Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_ina219_voltage +X Panel 6 2 3 Voltage +X Panel
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_ina219_voltage -X Panel 9 2 3 Voltage -X Panel
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_ina219_voltage +Y Panel 7 2 3 Voltage +YPanel
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_ina219_voltage -Y Panel 10 2 3 Voltage -Y Panel
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_ina219_voltage +Z Panel 8 2 3 Voltage +Z Panel
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_ina219_voltage -Z Panel 11 2 3 Voltage -Z Panel
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_ina219_current +X Panel 6 1 3 Current +X Panel
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_ina219_current -X Panel 9 1 3 Current -X Panel
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_ina219_current +Y Panel 7 1 3 Current +Y Panel
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_ina219_current -Y Panel 10 1 3 Current -Y Panel
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_ina219_current +Z Panel 8 1 3 Current +Z Panel
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_ina219_current -Z Panel 11 1 3 Current -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_ina219_voltage PSU 4 2 3 Board Voltage Power Supply Voltage
23 21 RT SPIN 12 rpm 12 Computer 2 2 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 RT TXPACurrent 12 mA 10 NONE 1 0 3 PA Current Transmit power amplifier current
25 23 RT TXTemperature 12 C 7 NONE 1 0 3 TX Temperature Transmitter card temperature
26 24 RT RXTemperature 12 C 7 Radio 1 1 3 RX Temperature Receiver card temperature
27 25 RT RSSI 12 dBm 14 Radio 1 2 3 RSSI Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer 2 1 3 Temperature Internal Temperature of IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation +X Panel 6 3 3 Rotation Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation +Y Panel 7 3 3 Rotation Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation +Z Panel 8 3 3 Rotation Angular Veolcity around Z Axis
32 30 RT EXP4Temperature 12 C 7 NONE 5 0 0 EXP4 Temperature Not used
33 31 RT PSUCurrent 12 mA cubesatsim_ina219_current PSU 4 1 3 Current Power Supply DC Current
34 32 RT IHUDiagnosticData 32 - 18 NONE 2 7 0 Diagnostic Info Diagnostic Data on IHU Performance
35 33 RT Experiment1FailureIndication 1 - 17 Experiments 5 1 0 STEM Payload Status STEM Payload Board Status
36 34 RT Experiment2FailureIndication 1 - 17 NONE 5 0 0 Not installed Not used
37 35 RT Experiment3FailureIndication 1 - 17 NONE 5 0 0 Not installed Not used
38 36 RT Experiment4FailureIndication 1 - 17 NONE 5 0 0 Not installed Not used
39 37 RT BATTI2CFailureIndications 1 - 17 Computer 2 3 0 Battery I2C Battery I2C Bus failure indicator
40 38 RT PSU1I2CFailureIndications 1 - 17 Computer 2 4 0 PSU1 I2C PSU2 I2C Bus failure indicator
41 39 RT PSU2I2CFailureIndications 1 - 17 Computer 2 5 0 PSU2 I2C PSU2 I2C Bus failure indicator
42 40 RT NumberofGroundCommandedTLMResets 4 - 1 Computer 2 6 0 Ground Resets Number of times command stations reset stored telemetry
43 41 RT RXAntenna 1 - 16 Radio 1 4 0 RX Antenna 70cm Antenna status
44 42 RT TXAntenna 1 - 16 Radio 1 3 0 TX Antenna 2m Antenna status
45 43 RT Pad 51 - 0 NONE 0 0 0 NONE NONE

6
spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.MASTER → spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER
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@ -19,7 +19,7 @@ layout0.filename=FOX1A_debug.csv
layout0.name=DEBUG
layout1.filename=CubeSatSim_maxtelemetry.csv
layout1.name=maxtelemetry
layout2.filename=CubeSatSim_rttelemetryFM.csv
layout2.filename=CubeSatSim_rttelemetry.csv
layout2.name=rttelemetry
layout3.filename=CubeSatSim_mintelemetry.csv
layout3.name=mintelemetry
@ -46,9 +46,9 @@ passMeasurementsFileName=passmeasurements.csv
numberOfSources=1
source0.name=amsat.cubesat_simulator.ihu.duv
#source1.name=amsat.cubesat_simulator.ihu.highspeed
track=true
track=false
useIHUVBatt=true
user_mode=0
user_format=0
useConversionCoeffs=true
conversionCurvesFileName=cubesatsim_conversion_curves.csv
conversionCurvesFileName=CubeSatSim_conversion_curves.csv

15
spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat
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@ -0,0 +1,15 @@
#Fox 1 Telemetry Decoder User Spacecraft Properties
#Wed Nov 25 09:31:53 EST 2020
hasModeInHeader=false
maxFreqBoundkHz=434950.0
displayName=CubeSatSim-FSK
minFreqBoundkHz=434850.0
priority=1
memsRestValueY=2101
memsRestValueZ=2045
user_format=0
memsRestValueX=2087
name=CubeSatSim
track=false
telemetryDownlinkFreqkHz=434900.0
BATTERY_CURRENT_ZERO=-1.839

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spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER
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@ -0,0 +1,72 @@
#Fox 1 Telemetry Decoder Properties
#Thu Apr 11 13:23:23 EST 2020
user_mode=4
foxId=99
IHU_SN=7
catalogNumber=0
model=0
mpptResistanceError=6.58
mpptSensorOffThreshold=1600
name=CubeSatSim
displayName=CubeSatSim-BPSK
BATTERY_CURRENT_ZERO=-1.834
hasImprovedCommandReceiver=true
EXP1=0
EXP2=0
EXP3=0
EXP4=0
description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org
numberOfFrameLayouts=5
frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame
frameLayout0.name=All WOD
frameLayout1.filename=CubeSatSim_PSK_Type1_HEALTH.frame
frameLayout1.name=Health
frameLayout2.filename=CubeSatSim_PSK_Type2_MINMAX.frame
frameLayout2.name=MinMax
frameLayout3.filename=FOX1E_Type3_REALTIME_BEACON.frame
frameLayout3.name=Realtime Beacon
frameLayout4.filename=FOX1E_Type4_WOD_BEACON.frame
frameLayout4.name=WOD Beacon
numberOfLayouts=9
layout0.filename=FOX1A_debug.csv
layout0.name=DEBUG
layout1.filename=CubeSatSim_PSK_maxtelemetry.csv
layout1.name=maxtelemetry
layout2.filename=CubeSatSim_PSK_rttelemetry.csv
layout2.name=rttelemetry
layout3.filename=CubeSatSim_PSK_mintelemetry.csv
layout3.name=mintelemetry
layout4.filename=FOX1E_radtelemetry.csv
layout4.name=radtelemetry
layout5.filename=FOX1E_radtelemetry2.csv
layout5.name=radtelemetry2
layout5.parentLayout=radtelemetry
layout6.filename=CubeSatSim_PSK_wodtelemetry.csv
layout6.name=wodtelemetry
layout7.filename=FOX1E_wodradtelemetry.csv
layout7.name=wodradtelemetry
layout8.filename=FOX1E_wodradtelemetry2.csv
layout8.name=wodradtelemetry2
layout8.parentLayout=wodradtelemetry
numberOfLookupTables=3
lookupTable0.filename=FOX1A_rssiFM.tab
lookupTable0=RSSI
lookupTable1.filename=FOX1E_ihuVBattSNx.tab
lookupTable1=IHU_VBATT
lookupTable2.filename=FOX1A_ihutempSN7.tab
lookupTable2=IHU_TEMP
maxFreqBoundkHz=434950
measurementsFileName=measurements.csv
memsRestValueX=2129
memsRestValueY=2131
memsRestValueZ=2103
minFreqBoundkHz=434850
passMeasurementsFileName=passmeasurements.csv
telemetryDownlinkFreqkHz=434900
track=false
useIHUVBatt=false
numberOfSources=1
source0.name=amsat.cubesat_simulator.ihu.bpsk
user_format=0
useConversionCoeffs=true
conversionCurvesFileName=CubeSatSim_conversion_curves.csv

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spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.dat
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@ -0,0 +1,17 @@
#Fox 1 Telemetry Decoder User Spacecraft Properties
#Wed Nov 25 09:32:32 EST 2020
hasModeInHeader=false
maxFreqBoundkHz=434950.0
mpptSensorOffThreshold=1600
displayName=CubeSatSim-BPSK
minFreqBoundkHz=434850.0
mpptResistanceError=6.58
priority=1
memsRestValueY=2131
memsRestValueZ=2103
user_format=0
memsRestValueX=2129
name=CubeSatSim
track=false
telemetryDownlinkFreqkHz=434900.0
BATTERY_CURRENT_ZERO=-1.834

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spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv
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@ -1,6 +0,0 @@
CurveName,a,bx,cx^2,dx^3,ex^4,fx^5,Description
cubesatsim_ina219_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 sensors
cubesatsim_ina219_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,-2048,0.01,0,0,0,0,Converts positive and negative g acceleration
1 CurveName a bx cx^2 dx^3 ex^4 fx^5 Description
2 cubesatsim_ina219_voltage 0 0.01 0 0 0 0 Converts voltages read from the INA219 sensors
3 cubesatsim_ina219_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 -2048 0.01 0 0 0 0 Converts positive and negative g acceleration

2
spacecraft/README.md
Unescape View File

@ -1,6 +1,6 @@
These files are for FoxTelem, the AMSAT software by Chris Thompson AC3CZ/G0KLA for decoding and displaying Fox-1 series CubeSat telemetry.
To use FoxTelem with the CubeSat Simulator, you will need to download the latest version number listed in this directory.
To use FoxTelem with the CubeSat Simulator, you will need to download the 1.09m version from:
https://www.g0kla.com/foxtelem/downloads/test/

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