CubeSatSim/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv

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