Merge pull request #338 from alanbjohnston/beta-ft

FoxTelem updates and reset configuration

config

@@ -350,7 +350,7 @@ if [ "$1" = "" ]; then
 
 elif [ "$1" = "-i" ]; then
 
-	reboot=1
+	restart=1
 
 elif [ "$1" = "-a" ]; then
 
@@ -807,8 +807,9 @@ elif [ "$1" = "-d" ]; then
 #			reboot=1
 			sudo systemctl restart command
 			if [[ $(arecord -l | grep card) ]]; then
-				echo "restarting cubesatsim software"
+				restart=1
-				sudo systemctl restart cubesatsim
+###				echo "restarting cubesatsim software"
+###				sudo systemctl restart cubesatsim
 			fi
 ##			sudo reboot now	
 		fi
@@ -1363,6 +1364,39 @@ elif [ "$1" = "-L" ]; then
 		echo "Not updating mic level"
 	fi
 
+elif [ "$1" = "-g" ]; then
+
+	echo "Are you sure you want to reset the CubeSatSim configration back to the default settings?"
+	echo
+
+	read rset
+	echo
+	
+	if [ "$rset" = "y" ] || [ "$rset" = "yes" ]  ; then
+
+		echo "Resetting"
+
+		echo "AMSAT 0 0 0 no 3 434.9 435 no 0 0" > /home/pi/CubeSatSim/sim.cfg
+	
+		sudo echo "f" > /home/pi/CubeSatSim/.mode
+	
+		sudo rm /home/pi/CubeSatSim/battery_saver > /dev/null 2>&1
+	
+		sudo rm /home/pi/CubeSatSim/command_control > /dev/null 2>&1
+	
+		sudo rm /home/pi/CubeSatSim/command_control_direwolf > /dev/null 2>&1
+	
+		sudo rm /home/pi/CubeSatSim/beacon_off > /dev/null 2>&1
+	
+	        sudo echo "0" > /home/pi/CubeSatSim/command_count.txt
+	
+		reboot=1
+	else
+
+		echo "Not resetting"
+
+	fi
+
 elif [ "$1" = "-h" ]; then
 
 	echo "config OPTION"
@@ -1398,6 +1432,8 @@ elif [ "$1" = "-h" ]; then
 	echo "   -D     Change Transmit Commands state APRS or DTMF"
 	echo "   -o     Change telemetry beacon transmit state"
 	echo "   -L     Change microphone level for command and control"
+	echo "   -g     Reset configration back to default settings"
+
 	echo
 	exit
 

main.c

@@ -24,54 +24,6 @@
 //#define HAB  // uncomment to change APRS icon from Satellite to Balloon and only BAT telemetry
 
 int main(int argc, char * argv[]) {
-
-  char resbuffer[1000];
-//  const char testStr[] = "cat /proc/cpuinfo | grep 'Revision' | awk '{print $3}' | sed 's/^1000//' | grep '9000'";
-  const char testStr[] = "cat /proc/cpuinfo | grep 'Revision' | awk '{print $3}' | sed 's/^1000//'";
-  FILE *file_test = sopen(testStr);  // see if Pi Zero 2  
-  fgets(resbuffer, 1000, file_test);
-  fprintf(stderr, "Pi test result: %s\n", resbuffer);
-  fclose(file_test);	
-
-  FILE * uptime_file = fopen("/proc/uptime", "r");
-  fscanf(uptime_file, "%f", & uptime_sec);
-  printf("Uptime sec: %f \n", uptime_sec);	  
-  fclose(uptime_file);
-  
-  fprintf(stderr, " %x ", resbuffer[0]);
-  fprintf(stderr, " %x \n", resbuffer[1]);	
-  if ((resbuffer[0] != '9') || (resbuffer[1] != '0') || (resbuffer[2] != '0') || (resbuffer[3] != '0')) 
-  {
-    // voltageThreshold = 3.7;
-    fprintf(stderr, "Pi Zero not detected (could be Pi Zero 2)\n");
-    pi_zero_2_offset = 500;
-    if (uptime_sec < 30.0) {
-	FILE * rpitx_stop = popen("sudo systemctl start rpitx", "r");
-  	pclose(rpitx_stop);   
-        fprintf(stderr, "Sleep 5 sec");    
-	sleep(5);  // try sleep at start to help boot
-    }
-  }
-  else {
-    fprintf(stderr,"Pi Zero detected\n");
-    FILE * command_file = fopen("/home/pi/CubeSatSim/command_control", "r");
-    if (command_file == NULL) {
-	    pi_zero_2_offset = 500;
-	    fprintf(stderr,"Command and control is OFF\n");
-    } else {
-	    command_file = fopen("/home/pi/CubeSatSim/command_control_direwolf", "r");
-	    if (command_file == NULL)  {
-		    pi_zero_2_offset = 500;
-		    fprintf(stderr,"Command and control Carrier (squelch) is ON\n");
-	    }
-    }
-    if (uptime_sec < 30.0) {
-	FILE * rpitx_stop = popen("sudo systemctl start rpitx", "r");
-  	pclose(rpitx_stop);
-	fprintf(stderr,"Sleep 10 sec");    
-    	sleep(10);
-    }
-  }
 	
   printf("\n\nCubeSatSim v1.3.2 starting...\n\n");
 
@@ -95,7 +47,7 @@ int main(int argc, char * argv[]) {
   fprintf(stderr,"Config file /home/pi/CubeSatSim/sim.cfg contains %s %d %f %f %s %d %s %s %s %d %d\n", 
 	  call, reset_count, lat_file, long_file, sim_yes, squelch, tx, rx, hab_yes, rx_pl, tx_pl);
 
-  fprintf(stderr, "Transmit on %s Receive on %s\n", tx, rx);
+  fprintf(stderr, "Transmit on %s MHz Receive on %s MHz\n", tx, rx);
 
 //  program_radio();  // do in rpitx instead
 	
@@ -126,6 +78,71 @@ int main(int argc, char * argv[]) {
   if (strcmp(hab_yes, "yes") == 0) {
 	  hab_mode = TRUE;
 	  fprintf(stderr, "HAB mode is ON\n");
+  }	
+	
+  FILE * command_file = fopen("/home/pi/CubeSatSim/command_control", "r");
+  if (command_file == NULL) {	  	
+	    fprintf(stderr,"Command and control is OFF\n");
+	    c2cStatus = 0;
+  } else {
+	    command_file = fopen("/home/pi/CubeSatSim/command_control_direwolf", "r");
+	    if (command_file == NULL)  {
+		    fprintf(stderr,"Command and control Carrier (squelch) is ON\n");
+		    c2cStatus = 1;
+	    } else {
+		    fprintf(stderr,"Command and control DTMF or APRS is ON\n");
+		    c2cStatus = 2;
+	    }
+  }	
+  printf("c2cStatus: %d \n", c2cStatus);
+	
+  char resbuffer[1000];
+//  const char testStr[] = "cat /proc/cpuinfo | grep 'Revision' | awk '{print $3}' | sed 's/^1000//' | grep '9000'";
+  const char testStr[] = "cat /proc/cpuinfo | grep 'Revision' | awk '{print $3}' | sed 's/^1000//'";
+  const char test2Str[] = "cat /proc/cpuinfo | grep 'Revision' | awk '{print $3}' | sed 's/^1000//' | grep '902120'";	
+  FILE *file_test = sopen(testStr);  // see if Pi Zero 2  
+  fgets(resbuffer, 1000, file_test);
+  fprintf(stderr, "Pi Zero test result: %s\n", resbuffer);
+  fclose(file_test);	
+
+  FILE * uptime_file = fopen("/proc/uptime", "r");
+  fscanf(uptime_file, "%f", & uptime_sec);
+  printf("Uptime sec: %f \n", uptime_sec);	  
+  fclose(uptime_file);
+  
+//  fprintf(stderr, "hex:  %x %x %x %x \n", resbuffer[0], resbuffer[1], resbuffer[2], resbuffer[3]);
+  if ((resbuffer[0] != '9') || (resbuffer[1] != '0') || (resbuffer[2] != '0') || (resbuffer[3] != '0')) 
+  {
+    // voltageThreshold = 3.7;
+//    if ((resbuffer[0] != '9') || (resbuffer[1] != '0') || (resbuffer[2] != '2') || (resbuffer[3] != '1'))
+    FILE *file2_test = sopen(test2Str);  // see if Pi Zero 2  
+    fgets(resbuffer, 1000, file2_test);
+    fprintf(stderr, "Pi Zero 2 test result: %s\n", resbuffer);
+    fclose(file2_test);	  
+    if (strlen(resbuffer) > 5) 	
+      fprintf(stderr, "Pi Zero 2 detected\n");
+    else
+      fprintf(stderr, "Not a Pi Zero or Pi Zero 2\n");
+	    
+    pi_zero_2_offset = 500;
+    if (uptime_sec < 30.0) {
+	FILE * rpitx_stop = popen("sudo systemctl start rpitx", "r");
+  	pclose(rpitx_stop);   
+        fprintf(stderr, "Sleep 5 sec");    
+	sleep(5);  // try sleep at start to help boot
+    }
+  }
+  else {
+    fprintf(stderr,"Pi Zero detected\n");
+    if ((c2cStatus == 0) || (c2cStatus == 1))  {
+      pi_zero_2_offset = 500;
+    }
+    if (uptime_sec < 30.0) {
+      FILE * rpitx_stop = popen("sudo systemctl start rpitx", "r");
+      pclose(rpitx_stop);
+      fprintf(stderr,"Sleep 10 sec");    
+      sleep(10);
+    }
   }
 	
 //  FILE * rpitx_stop = popen("sudo systemctl stop rpitx", "r");
@@ -700,6 +717,7 @@ int main(int argc, char * argv[]) {
               token = strtok(NULL, space);
             }
           }
+
           printf("\n");
 //	  if (sensor[GPS1] != 0) {     		
 	  if ((sensor[GPS1] > -90.0) && (sensor[GPS1] < 90.0) && (sensor[GPS1] != 0.0))  { 
@@ -875,8 +893,11 @@ int main(int argc, char * argv[]) {
     FILE * fp = fopen("/home/pi/CubeSatSim/telem_string.txt", "w");
     if (fp != NULL)  {	  
 //    	printf("Writing telem_string.txt\n");
-	if (batteryVoltage != 4.5)    
+	if (batteryVoltage != 4.5)
-    		fprintf(fp, "BAT %4.2fV %5.1fmA\n", batteryVoltage, batteryCurrent);	
+		if (c2cStatus == 0)
+    			fprintf(fp, "BAT %4.2fV %4.0fmA\n", batteryVoltage, batteryCurrent);
+		else
+    			fprintf(fp, "BAT %4.2fV %4.0fmA C\n", batteryVoltage, batteryCurrent);	// show command and control is on		
 	else
     		fprintf(fp, "\n");	// don't show voltage and current if it isn't a sensor value
 		
@@ -891,6 +912,28 @@ int main(int argc, char * argv[]) {
 //    fprintf(stderr, "INFO: Getting TLM Data\n");
     #endif
 
+    FILE * command_file = fopen("/home/pi/CubeSatSim/command_control", "r");
+    if (command_file == NULL) {
+	    if (c2cStatus != 0) {
+	      fprintf(stderr,"Command and control is OFF\n");
+	      c2cStatus = 0;
+	    }
+    } else {
+	    command_file = fopen("/home/pi/CubeSatSim/command_control_direwolf", "r");
+	    if (command_file == NULL)  {
+	      if (c2cStatus != 1) {
+		    fprintf(stderr,"Command and control Carrier (squelch) is ON\n");
+		    c2cStatus = 1;
+	      }
+	    } else {
+		if (c2cStatus != 2) {
+		    fprintf(stderr,"Command and control DTMF or APRS is ON\n");
+		    c2cStatus = 2;
+		}
+	    }
+    }	
+  // printf("c2cStatus: %d \n", c2cStatus);	  
+	  
     if ((mode == AFSK) || (mode == CW)) {
       get_tlm();
       sleep(25);
@@ -1084,7 +1127,7 @@ void get_tlm(void) {
    if (mode == CW) {
     int channel;
     for (channel = 1; channel < 7; channel++) {
-      sprintf(tlm_str, "echo ' %d%d%d %d%d%d %d%d%d %d%d%d ' > cw%1d.txt",
+      sprintf(tlm_str, "echo -n ' %d%d%d %d%d%d %d%d%d %d%d%d ' > cw%1d.txt",
         channel, upper_digit(tlm[channel][1]), lower_digit(tlm[channel][1]),
         channel, upper_digit(tlm[channel][2]), lower_digit(tlm[channel][2]),
         channel, upper_digit(tlm[channel][3]), lower_digit(tlm[channel][3]),
@@ -1098,6 +1141,10 @@ void get_tlm(void) {
         pclose(cw_file);	     
 
     }
+    if (c2cStatus != 0) {	   
+      FILE *file_append = sopen("echo 'C' >> cw6.txt");
+      fclose(file_append);
+    }
   } else {  // APRS
 
       sprintf(tlm_str, "BAT %4.2f %5.1f ", voltage[map[BAT]] , current[map[BAT]] ); 
@@ -1107,10 +1154,9 @@ void get_tlm(void) {
     printf(" Response from STEM Payload board:: %s\n", sensor_payload);
 //    printf(" Str so far: %s\n", str);   
 	  
-    if (mode != CW) {
+    if (mode != CW) 
         strcat(str, sensor_payload); // append to telemetry string for transmission
-//	printf(" Str so far: %s\n", str);    
+
-    }
     if (mode == CW) {
 
 //      char cw_str2[1000];
@@ -1359,8 +1405,8 @@ void get_tlm_fox() {
 
     // read payload sensor if available
 
-    encodeA(b, 0 + head_offset, batt_a_v);
+//    encodeA(b, 0 + head_offset, batt_a_v);  // replaced by XS2 and XS3 below
-    encodeB(b, 1 + head_offset, batt_b_v);
+//    encodeB(b, 1 + head_offset, batt_b_v);
     encodeA(b, 3 + head_offset, batt_c_v);
 
     encodeB(b, 4 + head_offset, (int)(sensor[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
@@ -1423,8 +1469,8 @@ void get_tlm_fox() {
       encodeB(b_max, 37 + head_offset, (int)(other_max[RSSI] + 0.5) + 2048);	    
       encodeA(b_max, 39 + head_offset, (int)(other_max[IHU_TEMP] * 10 + 0.5));
       encodeB(b_max, 31 + head_offset, ((int)(other_max[SPIN] * 10)) + 2048);
-	    
+
-      if (sensor_min[0] != 1000.0) // make sure values are valid
+      if (sensor_min[TEMP] != 1000.0) // make sure values are valid
       {	        	    
 	      encodeB(b_max, 4 + head_offset, (int)(sensor_max[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
 	      encodeA(b_max, 6 + head_offset, (int)(sensor_max[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
@@ -1437,9 +1483,13 @@ void get_tlm_fox() {
 	      encodeB(b_max, 43 + head_offset, (int)(sensor_max[GYRO_Z] + 0.5) + 2048);
 
 	      encodeA(b_max, 48 + head_offset, (int)(sensor_max[DTEMP] * 10 + 0.5) + 2048);
-	      encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1] * 10 + 0.5) + 2048);
+//	      encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS1] * 10 + 0.5) + 2048);
 	      encodeB(b_max, 10 + head_offset, (int)(sensor_max[TEMP] * 10 + 0.5)); 	
 	      encodeA(b_max, 45 + head_offset, (int)(sensor_max[HUMI] * 10 + 0.5));
+
+	      encodeB(b_max, 49 + head_offset, (int)(sensor[XS1]));
+	      encodeA(b_max, 0 + head_offset, (int)(sensor[XS2]));
+	      encodeB(b_max, 1 + head_offset, (int)(sensor[XS3]));
       }	  
       else
       {	        	    
@@ -1452,7 +1502,7 @@ void get_tlm_fox() {
 	      encodeB(b_max, 43 + head_offset, 2048);
 
 	      encodeA(b_max, 48 + head_offset, 2048);
-	      encodeB(b_max, 49 + head_offset, 2048);
+//	      encodeB(b_max, 49 + head_offset, 2048);
       }	  	      
       encodeA(b_min, 12 + head_offset, (int)(voltage_min[map[PLUS_X]] * 100));
       encodeB(b_min, 13 + head_offset, (int)(voltage_min[map[PLUS_Y]] * 100));
@@ -1477,7 +1527,7 @@ void get_tlm_fox() {
       encodeB(b_min, 37 + head_offset, (int)(other_min[RSSI] + 0.5) + 2048);	    
       encodeA(b_min, 39 + head_offset, (int)(other_min[IHU_TEMP] * 10 + 0.5));
 	    
-      if (sensor_min[0] != 1000.0) // make sure values are valid
+      if (sensor_min[TEMP] != 1000.0) // make sure values are valid
       {	        
 	      encodeB(b_min, 4 + head_offset, (int)(sensor_min[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
 	      encodeA(b_min, 6 + head_offset, (int)(sensor_min[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
@@ -1490,9 +1540,13 @@ void get_tlm_fox() {
 	      encodeB(b_min, 43 + head_offset, (int)(sensor_min[GYRO_Z] + 0.5) + 2048);
 
 	      encodeA(b_min, 48 + head_offset, (int)(sensor_min[DTEMP] * 10 + 0.5) + 2048);
-	      encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1] * 10 + 0.5) + 2048);
+//	      encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS1] * 10 + 0.5) + 2048);
 	      encodeB(b_min, 10 + head_offset, (int)(sensor_min[TEMP] * 10 + 0.5)); 	    
 	      encodeA(b_min, 45 + head_offset, (int)(sensor_min[HUMI] * 10 + 0.5));
+
+	      encodeB(b_min, 49 + head_offset, (int)(sensor[XS1]));
+	      encodeA(b_min, 0 + head_offset, (int)(sensor[XS2]));
+	      encodeB(b_min, 1 + head_offset, (int)(sensor[XS3]));	      	      	      
     }      
       else
       {	        	    
@@ -1505,7 +1559,7 @@ void get_tlm_fox() {
 	      encodeB(b_min, 43 + head_offset, 2048);
 
 	      encodeA(b_min, 48 + head_offset, 2048);
-	      encodeB(b_min, 49 + head_offset, 2048);
+//	      encodeB(b_min, 49 + head_offset, 2048);
       }	 
     }    
     encodeA(b, 30 + head_offset, PSUVoltage);
@@ -1528,8 +1582,12 @@ void get_tlm_fox() {
 
     encodeB(b, 46 + head_offset, PSUCurrent);
     encodeA(b, 48 + head_offset, (int)(sensor[DTEMP] * 10 + 0.5) + 2048);
-    encodeB(b, 49 + head_offset, (int)(sensor[XS1] * 10 + 0.5) + 2048);
+//    encodeB(b, 49 + head_offset, (int)(sensor[XS1] * 10 + 0.5) + 2048);
-
+	  
+    encodeB(b, 49 + head_offset, (int)(sensor[XS1]));
+    encodeA(b, 0 + head_offset, (int)(sensor[XS2]));
+    encodeB(b, 1 + head_offset, (int)(sensor[XS3]));
+	  
     FILE * command_count_file = fopen("/home/pi/CubeSatSim/command_count.txt", "r");
     if (command_count_file != NULL) {	
       char count_string[10];	
@@ -1545,8 +1603,14 @@ void get_tlm_fox() {
       (i2c_bus0 == OFF) * 16 + (i2c_bus1 == OFF) * 32 + (i2c_bus3 == OFF) * 64 + (camera == OFF) * 128 + groundCommandCount * 256;
 
     encodeA(b, 51 + head_offset, status);
-    encodeB(b, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed * 2);
+    encodeB(b, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed * 2 + c2cStatus * 4);
-
+    if (mode == BPSK) {	  
+      encodeA(b_max, 51 + head_offset, status);
+      encodeA(b_min, 51 + head_offset, status);
+      encodeB(b_max, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed * 2 + c2cStatus * 4);
+      encodeB(b_min, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed * 2 + c2cStatus * 4);
+    }
+	  
     if (txAntennaDeployed == 0) {
       txAntennaDeployed = 1;
       printf("TX Antenna Deployed!\n");
@@ -1754,9 +1818,11 @@ void get_tlm_fox() {
 
     if (connect(sock, (struct sockaddr * ) & serv_addr, sizeof(serv_addr)) < 0) {
       printf("\nConnection Failed \n");
-      printf("Error: %s \n", strerror(errno));
+      printf("Error: %s restarting rpitx\n", strerror(errno));
       error = 1;
-      sleep(2.0);  // sleep if socket connection refused
+  	FILE * rpitx_restartf2 = popen("sudo systemctl restart rpitx", "r");
+  	pclose(rpitx_restartf2);	      
+        sleep(5);  // sleep if socket connection refused
 
     // try again
       error = 0;
@@ -1778,9 +1844,11 @@ void get_tlm_fox() {
 
       if (connect(sock, (struct sockaddr * ) & serv_addr, sizeof(serv_addr)) < 0) {
         printf("\nConnection Failed \n");
-        printf("Error: %s \n", strerror(errno));
+        printf("Error: %s restarting rpitx\n", strerror(errno));
         error = 1;
- //       sleep(1.0);  // sleep if socket connection refused
+  	FILE * rpitx_restartf = popen("sudo systemctl restart rpitx", "r");
+  	pclose(rpitx_restartf);	      
+        sleep(5);  // sleep if socket connection refused
       }	    
     }
     if (error == 1)

main.h

@@ -152,7 +152,8 @@ int frameTime;
 long int newGpsTime;
 
 float axis[3], angle[3], volts_max[3], amps_max[3], batt, speed, period, tempS, temp_max, temp_min, eclipse;
-int i2c_bus0 = OFF, i2c_bus1 = OFF, i2c_bus3 = OFF, camera = OFF, sim_mode = FALSE, SafeMode = FALSE, rxAntennaDeployed = 0, txAntennaDeployed = 0;
+int i2c_bus0 = OFF, i2c_bus1 = OFF, i2c_bus3 = OFF, camera = OFF, sim_mode = FALSE, SafeMode = FALSE;
+int rxAntennaDeployed = 0, txAntennaDeployed = 0, c2cStatus = 0;
 int sim_config = FALSE; // sim mode not set by configuration
 double eclipse_time;
 

rpitx.py

@@ -363,7 +363,8 @@ if __name__ == "__main__":
 #			ser.write(b"AT+DMOSETGROUP=0,435.0000,434.9000,0,3,0,0\r\n")
 			ser.write(uhf_string.encode())
 			sleep(0.1)
-		ser.close()	
+		ser.close()
+		ser = serial.Serial("/dev/ttyAMA0", 115200) # reset back to 115200 for cubesatsim code for payload sensor data
 	except:
 		print("Error in serial write")
 	output(pd, 0)

spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_maxtelemetry.csv

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

spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_mintelemetry.csv

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

spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_rttelemetry.csv

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

spacecraft/FoxTelem_1.13e/CubeSatSim_maxtelemetry.csv

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

spacecraft/FoxTelem_1.13e/CubeSatSim_mintelemetry.csv

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

spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv

@@ -0,0 +1,48 @@
+47,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
+0,RT,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
+1,RT,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
+2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
+3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
+4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
+5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
+6,RT,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current
+7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature
+8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X Panel Voltage
+9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X Panel Voltage
+10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y Panel Voltage
+11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y Panel Voltage
+12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z Panel Voltage
+13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z Panel Voltage
+14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X Panel Current
+15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X Panel Current
+16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y Panel Current
+17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y Panel Current
+18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z Panel Current
+19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z Panel Current
+20,RT,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
+21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,RT,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure
+23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude
+24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication
+26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU
+27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis
+28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis
+29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis
+30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity
+31,RT,BATT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
+32,RT,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
+33,RT,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
+34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status
+35,RT,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
+36,RT,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator
+37,RT,PayloadStatus1,1,-,17,NONE,0,0,0,Exp 3,STEM Payload status 1 failure indicator
+38,RT,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
+39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
+40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
+41,RT,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator
+42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
+43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
+44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
+45,RT,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status
+46,RT,Pad,56,-,0,NONE,0,0,0,NONE,NONE

spacecraft/FoxTelem_1.13e/CubeSat_Simulator_DUV.MASTER

@@ -0,0 +1,59 @@
+#Fox 1 Telemetry Decoder Properties
+#Sat Apr 11 13:20:20 EST 2020
+#File named .dat should be in the logfiles directory and is loaded by FoxTelem
+#File named .MASTER should not be edited and is a backup copy in the installation directory 
+foxId=7
+displayName=CubeSatSim-FSK
+name=CubeSatSim
+model=0
+IHU_SN=7
+catalogNumber=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 DUV FSK telemetry. For more information see http://cubesatsim.org
+BATTERY_CURRENT_ZERO=-1.839
+EXP1=0
+EXP2=0
+EXP3=0
+EXP4=0
+numberOfLayouts=4
+layout0.filename=FOX1A_debug.csv
+layout0.name=DEBUG
+layout1.filename=CubeSatSim_maxtelemetry.csv
+layout1.name=maxtelemetry
+layout2.filename=CubeSatSim_rttelemetry.csv
+layout2.name=rttelemetry
+layout3.filename=CubeSatSim_mintelemetry.csv
+layout3.name=mintelemetry
+#layout4.filename=FOX1A_radtelemetry.csv
+#layout4.name=radtelemetry
+#layout5.filename=FOX1A_radtelemetry2.csv
+#layout5.name=radtelemetry2
+#layout5.parentLayout=radtelemetry
+lookupTable0.filename=FOX1A_rssiFM.tab
+numberOfLookupTables=3
+lookupTable0=RSSI
+lookupTable1.filename=FOX1A_ihuVBattSN7.tab
+lookupTable1=IHU_VBATT
+lookupTable2.filename=FOX1A_ihutempSN7.tab
+lookupTable2=IHU_TEMP
+numberOfStringLookupTables=2
+stringLookupTable0.filename=status_on_off.tab
+stringLookupTable0=STATUS_ON_OFF
+stringLookupTable1=COMMAND_STATUS
+stringLookupTable1.filename=command_status.tab
+telemetryDownlinkFreqkHz=434900	
+maxFreqBoundkHz=434950
+minFreqBoundkHz=434850
+measurementsFileName=measurements.csv
+memsRestValueX=2087
+memsRestValueY=2101
+memsRestValueZ=2045
+passMeasurementsFileName=passmeasurements.csv
+numberOfSources=1
+source0.name=amsat.cubesat_simulator.ihu.duv
+source0.formatName=FSK 200bps (Fox1)
+#source1.name=amsat.cubesat_simulator.ihu.highspeed
+track=false
+useIHUVBatt=true
+user_format=FSK 200bps (Fox1)
+useConversionCoeffs=true
+conversionCurvesFileName=CubeSatSim_conversion_curves.csv

spacecraft/FoxTelem_1.13e/CubeSat_Simulator_PSK.MASTER

@@ -0,0 +1,77 @@
+#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
+numberOfStringLookupTables=2
+stringLookupTable0.filename=status_on_off.tab
+stringLookupTable0=STATUS_ON_OFF
+stringLookupTable1=COMMAND_STATUS
+stringLookupTable1.filename=command_status.tab
+maxFreqBoundkHz=434950
+measurementsFileName=measurements.csv
+memsRestValueX=2129
+memsRestValueY=2131
+memsRestValueZ=2103
+minFreqBoundkHz=434850
+passMeasurementsFileName=passmeasurements.csv
+telemetryDownlinkFreqkHz=434900
+track=true
+useIHUVBatt=false
+numberOfSources=1
+source0.name=amsat.cubesat_simulator.ihu.bpsk
+user_format=0
+useConversionCoeffs=true
+conversionCurvesFileName=CubeSatSim_conversion_curves.csv

spacecraft/FoxTelem_1.13e/README.md

@@ -0,0 +1,3 @@
+These files are for FoxTelem version 1.13e in the spacecraft directory.
+
+You can download this version of FoxTelem here: https://www.g0kla.com/foxtelem/downloads/test/

spacecraft/FoxTelem_1.13e/command_status.tab

@@ -0,0 +1,3 @@
+0,OFF
+1,Carrier
+2,DTMF/APRS