diff --git a/README.md b/README.md
index 36eb3595..c2a98d64 100644
--- a/README.md
+++ b/README.md
@@ -4,7 +4,7 @@ The CubeSat Simulator https://github.com/alanbjohnston/CubeSatSim/wiki is a low
 
 There are several hardware versions and software branches to go with them - see below for information.
 
-See the Wiki Software Install page for more details: https://github.com/alanbjohnston/CubeSatSim/wiki/Software-Install. The software runs on any Raspberry Pi including the Raspberry Pi 4B, 3B, 3B+, Pi Zero or Pi Zero W.
+See the Wiki Software Install page for more details: https://github.com/alanbjohnston/CubeSatSim/wiki/2.-Software-Install. The software runs on any Raspberry Pi including the Raspberry Pi 4B, 3B, 3B+, Pi Zero or Pi Zero W.
 
 There are two ways to get the CubeSatSim software for your Pi.
 
@@ -17,12 +17,13 @@ The other option is to start with any Raspberry Pi OS (Rasbian) image and run th
 - pi-power-button
 - Direwolf
 - rpitx
+- cpulimit
 - python3-pip 
 - python-smbus
 
 ## Disk Image Option Steps
 
-See the Wiki Software Install page for details: https://github.com/alanbjohnston/CubeSatSim/wiki/Software-Install.
+See the Wiki Software Install page for details: https://github.com/alanbjohnston/CubeSatSim/wiki/2.-Software-Install.
 
 ## Installation Script Option Steps
 
diff --git a/afsk/main.c b/afsk/main.c
index 21a8d55d..e9acbc31 100644
--- a/afsk/main.c
+++ b/afsk/main.c
@@ -46,7 +46,6 @@
 #define B 2
 #define C 3
 #define D 4
-
 #define PLUS_X 0
 #define PLUS_Y 1
 #define BAT 2
@@ -55,7 +54,6 @@
 #define MINUS_Y 5
 #define PLUS_Z 6
 #define MINUS_Z 7
-
 #define TEMP 2
 #define PRES 3
 #define ALT 4
@@ -98,12 +96,14 @@ static int init_rf();
 int socket_open = 0;
 int sock = 0;
 int loop = -1, loop_count = 0;
-int firstTime = ON;
+int firstTime = ON; // 0;
 long start;
 int testCount = 0;
 long time_start;
-
+char cmdbuffer[1000];
+FILE * file1;
 short int buffer[2336400]; // max size for 10 frames count of BPSK
+FILE *sopen(const char *program);
 
 #define S_RATE	(48000) // (44100)
 
@@ -116,6 +116,8 @@ int rpitxStatus = -1;
 
 float amplitude; // = ; // 20000; // 32767/(10%amp+5%amp+100%amp)
 float freq_Hz = 3000; // 1200
+short int sin_samples;
+short int sin_map[16];
 
 int smaller;
 int flip_ctr = 0;
@@ -134,7 +136,8 @@ char call[5];
 
 int bitRate, mode, bufLen, rsFrames, payloads, rsFrameLen, dataLen, headerLen, syncBits, syncWord, parityLen, samples, frameCnt, samplePeriod;
 float sleepTime;
-int sampleTime = 0, frames_sent = 0;
+unsigned int sampleTime = 0;
+int frames_sent = 0;
 int cw_id = ON;
 int vB4 = FALSE, vB5 = FALSE, vB3 = FALSE, ax5043 = FALSE, transmit = FALSE, onLed, onLedOn, onLedOff, txLed, txLedOn, txLedOff, payload = OFF;
 float batteryThreshold = 3.0, batteryVoltage;
@@ -340,22 +343,48 @@ int main(int argc, char * argv[]) {
   strcpy(pythonStr, pythonCmd);
   strcat(pythonStr, busStr);
   strcat(pythonConfigStr, pythonStr);
-  strcat(pythonConfigStr, " c");
+  strcat(pythonConfigStr, " c");  
 
-  //   FILE* file1 = popen("python3 /home/pi/CubeSatSim/python/voltcurrent.py 1 11 c", "r");
-  FILE * file1 = popen(pythonConfigStr, "r");
-  char cmdbuffer[1000];
+  fprintf(stderr, "pythonConfigStr: %s\n", pythonConfigStr);
+	
+  file1 = sopen(pythonConfigStr);  // try new function
+  fgets(cmdbuffer, 1000, file1);
+  fprintf(stderr, "pythonStr result: %s\n", cmdbuffer);
+/*	
+  sleep(5);
+  fputc('\n', file1);
   fgets(cmdbuffer, 1000, file1);
-  //   printf("pythonStr result: %s\n", cmdbuffer);
-  pclose(file1);
+  printf("pythonStr result2: %s\n", cmdbuffer);	
+	
+  file1 = popen(pythonConfigStr, "w");
 
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr result: %s\n", cmdbuffer);
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr resulta: %s\n", cmdbuffer);
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr resultb: %s\n", cmdbuffer);	
+//  pclose(file1);  
+
+  sleep(5);
+  fputc('\n', file1);
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr result2: %s\n", cmdbuffer);	
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr result2a: %s\n", cmdbuffer);	
+
+  sleep(5);
+  fputc('\n', file1);
+  fgets(cmdbuffer, 1000, file1);
+  printf("pythonStr result2: %s\n", cmdbuffer);		
+*/
   // try connecting to Arduino payload using UART
 
   if (!ax5043 && !vB3) // don't test if AX5043 is present
   {
     payload = OFF;
 
-    if ((uart_fd = serialOpen("/dev/ttyAMA0", 9600)) >= 0) {
+    if ((uart_fd = serialOpen("/dev/ttyAMA0", 115200)) >= 0) {  // was 9600
       char c;
       int charss = (char) serialDataAvail(uart_fd);
       if (charss != 0)
@@ -398,12 +427,12 @@ int main(int argc, char * argv[]) {
   i2c_bus3 = (test_i2c_bus(3) != -1) ? ON : OFF;
 
   // check for camera	
-  char cmdbuffer1[1000];
+//  char cmdbuffer1[1000];
   FILE * file4 = popen("vcgencmd get_camera", "r");
-  fgets(cmdbuffer1, 1000, file4);
+  fgets(cmdbuffer, 1000, file4);
   char camera_present[] = "supported=1 detected=1";
   // printf("strstr: %s \n", strstr( & cmdbuffer1, camera_present));
-  camera = (strstr( (const char *)& cmdbuffer1, camera_present) != NULL) ? ON : OFF;
+  camera = (strstr( (const char *)& cmdbuffer, camera_present) != NULL) ? ON : OFF;
   //  printf("Camera result:%s camera: %d \n", & cmdbuffer1, camera);
   pclose(file4);
 
@@ -411,8 +440,7 @@ int main(int argc, char * argv[]) {
   printf("INFO: I2C bus status 0: %d 1: %d 3: %d camera: %d\n", i2c_bus0, i2c_bus1, i2c_bus3, camera);
   #endif
 
-  // if ((i2c_bus1 == OFF) && (i2c_bus3 == OFF)) {
-  if (i2c_bus3 == OFF) {  // i2c bus 13 can be turned off manually by editing /boot/config.txt
+  if (i2c_bus3 == OFF) {
 
     sim_mode = TRUE;
 
@@ -484,38 +512,14 @@ int main(int argc, char * argv[]) {
   for (int i = 0; i < 17; i++) {
     sensor_min[i] = 1000.0;
     sensor_max[i] = -1000.0;
-    printf("Sensor min and max initialized!");
+ //   printf("Sensor min and max initialized!");
   }
   for (int i = 0; i < 3; i++) {
     other_min[i] = 1000.0;
     other_max[i] = -1000.0;
   }
 
-  while (loop-- != 0) {
-    frames_sent++;
-
-    #ifdef DEBUG_LOGGING
-    fprintf(stderr, "INFO: Battery voltage: %f V  Battery Threshold %f V\n", batteryVoltage, batteryThreshold);
-    #endif
-    if ((batteryVoltage > 1.0) && (batteryVoltage < batteryThreshold)) // no battery INA219 will give 0V, no battery plugged into INA219 will read < 1V
-    {
-      fprintf(stderr, "Battery voltage too low: %f V - shutting down!\n", batteryVoltage);
-      digitalWrite(txLed, txLedOff);
-      digitalWrite(onLed, onLedOff);
-      sleep(1);
-      digitalWrite(onLed, onLedOn);
-      sleep(1);
-      digitalWrite(onLed, onLedOff);
-      sleep(1);
-      digitalWrite(onLed, onLedOn);
-      sleep(1);
-      digitalWrite(onLed, onLedOff);
-
-      popen("sudo shutdown -h now > /dev/null 2>&1", "r");
-      sleep(10);
-    }
-
-    if (mode == FSK) {
+   if (mode == FSK) {
       bitRate = 200;
       rsFrames = 1;
       payloads = 1;
@@ -556,12 +560,53 @@ int main(int argc, char * argv[]) {
 
       printf("\n BPSK Mode, bufLen: %d,  %d bits per frame, %d bits per second, %d seconds per frame %d ms sample period\n",
         bufLen, bufLen / (samples * frameCnt), bitRate, bufLen / (samples * frameCnt * bitRate), samplePeriod);
+	   
+      sin_samples = S_RATE/freq_Hz;	 		
+      printf("Sin map: ");	 		
+      for (int j = 0; j < sin_samples; j++) {	 		
+        sin_map[j] = (short int)(amplitude * sin((float)(2 * M_PI * j / sin_samples)));	 		
+	printf(" %d", sin_map[j]);	 		
+      }	 		
+      printf("\n");
+   }
+
+  long int loopTime;
+  loopTime = millis();	
+	
+  while (loop-- != 0) {
+    fflush(stdout);
+    fflush(stderr);
+//    frames_sent++;
+
+    printf("++++ Loop time: %d +++++\n", millis() - loopTime);
+    loopTime = millis();
+	  
+    #ifdef DEBUG_LOGGING
+    fprintf(stderr, "INFO: Battery voltage: %f V  Battery Threshold %f V\n", batteryVoltage, batteryThreshold);
+    #endif
+    if ((batteryVoltage > 1.0) && (batteryVoltage < batteryThreshold)) // no battery INA219 will give 0V, no battery plugged into INA219 will read < 1V
+    {
+      fprintf(stderr, "Battery voltage too low: %f V - shutting down!\n", batteryVoltage);
+      digitalWrite(txLed, txLedOff);
+      digitalWrite(onLed, onLedOff);
+      
+      sleep(1);
+      digitalWrite(onLed, onLedOn);
+      sleep(1);
+      digitalWrite(onLed, onLedOff);
+      sleep(1);
+      digitalWrite(onLed, onLedOn);
+      sleep(1);
+      digitalWrite(onLed, onLedOff);
+
+      popen("sudo shutdown -h now > /dev/null 2>&1", "r");
+      sleep(10);
     }
 
     //  sleep(1);  // Delay 1 second
     ctr = 0;
     #ifdef DEBUG_LOGGING
-    fprintf(stderr, "INFO: Getting TLM Data\n");
+//    fprintf(stderr, "INFO: Getting TLM Data\n");
     #endif
 
     if ((mode == AFSK) || (mode == CW)) {
@@ -572,7 +617,7 @@ int main(int argc, char * argv[]) {
     }
 
     #ifdef DEBUG_LOGGING
-    fprintf(stderr, "INFO: Getting ready to send\n");
+//    fprintf(stderr, "INFO: Getting ready to send\n");
     #endif
   }
 
@@ -641,6 +686,10 @@ void get_tlm(void) {
   FILE * txResult;
 
   for (int j = 0; j < frameCnt; j++) {
+	  
+    fflush(stdout);
+    fflush(stderr);
+	  
     digitalWrite(txLed, txLedOn);
     #ifdef DEBUG_LOGGING
     printf("Tx LED On\n");
@@ -652,12 +701,13 @@ void get_tlm(void) {
 
     int count1;
     char * token;
-    char cmdbuffer[1000];
+//    char cmdbuffer[1000];
 
-    FILE * file = popen(pythonStr, "r");
-    fgets(cmdbuffer, 1000, file);
-    //   printf("result: %s\n", cmdbuffer);
-    pclose(file);
+//    FILE * file = popen(pythonStr, "r");
+    fputc('\n', file1);
+    fgets(cmdbuffer, 1000, file1);
+    printf("Python result: %s\n", cmdbuffer);
+//    pclose(file);
 
     const char space[2] = " ";
     token = strtok(cmdbuffer, space);
@@ -696,7 +746,7 @@ void get_tlm(void) {
       cpuTemp /= 1000;
 
       #ifdef DEBUG_LOGGING
-      printf("CPU Temp Read: %6.1f\n", cpuTemp);
+//      printf("CPU Temp Read: %6.1f\n", cpuTemp);
       #endif
 
     }
@@ -819,7 +869,8 @@ void get_tlm(void) {
     char header_long[10];
     char header_str4[] = "hi hi ";
     char footer_str1[] = "\' > t.txt && echo \'";
-    char footer_str[] = ">CQ:010101/hi hi ' >> t.txt && gen_packets -o telem.wav t.txt -r 48000 > /dev/null 2>&1 && cat telem.wav | csdr convert_i16_f | csdr gain_ff 7000 | csdr convert_f_samplerf 20833 | sudo /home/pi/rpitx/rpitx -i- -m RF -f 434.9e3 > /dev/null 2>&1";
+//    char footer_str[] = ">CQ:010101/hi hi ' >> t.txt && gen_packets -o telem.wav t.txt -r 48000 > /dev/null 2>&1 && cat telem.wav | csdr convert_i16_f | csdr gain_ff 7000 | csdr convert_f_samplerf 20833 | sudo /home/pi/rpitx/rpitx -i- -m RF -f 434.9e3 > /dev/null 2>&1";
+    char footer_str[] = ">CQ:010101/hi hi ' >> t.txt && touch ready";  // transmit is done by rpitx.py
 
     if (ax5043) {
       strcpy(str, header_str);
@@ -885,7 +936,7 @@ void get_tlm(void) {
       int i = 0;
 
       serialPutchar(uart_fd, '?');
-      printf("Querying payload with ?\n");
+//      printf("Querying payload with ?\n");
       waitTime = millis() + 500;
       int end = FALSE;
       while ((millis() < waitTime) && !end) {
@@ -903,7 +954,7 @@ void get_tlm(void) {
       }
       //    sensor_payload[i++] = '\n';
       sensor_payload[i] = '\0';
-      printf("Payload string: %s", sensor_payload);
+      printf("Payload string: %s\n", sensor_payload);
 
       strcat(str, sensor_payload); // append to telemetry string for transmission
     }
@@ -954,6 +1005,7 @@ void get_tlm(void) {
       if (transmit) {
         FILE * file2 = popen(str, "r");
         pclose(file2);
+	sleep(2);
       } else {
         fprintf(stderr, "\nNo CubeSatSim Band Pass Filter detected.  No transmissions after the CW ID.\n");
         fprintf(stderr, " See http://cubesatsim.org/wiki for info about building a CubeSatSim\n\n");
@@ -982,7 +1034,7 @@ void get_tlm(void) {
 void get_tlm_fox() {
 
   //  Reading I2C voltage and current sensors
-
+/*
   FILE * uptime_file = fopen("/proc/uptime", "r");
   fscanf(uptime_file, "%f", & uptime_sec);
   uptime = (int) uptime_sec;
@@ -990,7 +1042,7 @@ void get_tlm_fox() {
   printf("Reset Count: %d Uptime since Reset: %ld \n", reset_count, uptime);
   #endif
   fclose(uptime_file);
-
+*/
   int i;
   //	long int sync = SYNC_WORD;
   long int sync = syncWord;
@@ -999,8 +1051,13 @@ void get_tlm_fox() {
 
   //	short int b[DATA_LEN];
   short int b[dataLen];
+  short int b_max[dataLen];
+  short int b_min[dataLen];
+	
   memset(b, 0, sizeof(b));
-
+  memset(b_max, 0, sizeof(b_max));
+  memset(b_min, 0, sizeof(b_min));
+	
   //	short int h[HEADER_LEN];
   short int h[headerLen];
   memset(h, 0, sizeof(h));
@@ -1046,151 +1103,43 @@ void get_tlm_fox() {
       // delay for sample period
       digitalWrite(txLed, txLedOn);
       #ifdef DEBUG_LOGGING
-      printf("Tx LED On\n");
+//      printf("Tx LED On\n");
       #endif
-
+/*
       while ((millis() - sampleTime) < (unsigned int)samplePeriod)
         sleep((unsigned int)sleepTime);
-
+*/
+//      if (mode == FSK) 
+	sleep(2.3);  // No sleep at all!
+//      else	    
+//        sleep(1.3);
+	    
       digitalWrite(txLed, txLedOff);
       #ifdef DEBUG_LOGGING
-      printf("Tx LED Off\n");
+//      printf("Tx LED Off\n");
       #endif
 
-      printf("Sample period: %d\n", millis() - (unsigned int)sampleTime);
-      sampleTime = (int) millis();
+//      printf("Sample period: %d\n", millis() - (unsigned int)sampleTime);
+      sampleTime = (unsigned int) millis();
     } else
       printf("first time - no sleep\n");
-
-    int count1;
-    char * token;
-    char cmdbuffer[1000];
-
-    FILE * file = popen(pythonStr, "r");
-    fgets(cmdbuffer, 1000, file);
-    //  printf("result: %s\n", cmdbuffer);
-    pclose(file);
-
-    const char space[2] = " ";
-    token = strtok(cmdbuffer, space);
-
+	  
     float voltage[9], current[9], sensor[17], other[3];
+    char sensor_payload[500];
     memset(voltage, 0, sizeof(voltage));
     memset(current, 0, sizeof(current));
     memset(sensor, 0, sizeof(sensor));
-    memset(other, 0, sizeof(other));
-
-    for (count1 = 0; count1 < 8; count1++) {
-      if (token != NULL) {
-        voltage[count1] = (float) atof(token);
-        #ifdef DEBUG_LOGGING
-        //		printf("voltage: %f ", voltage[count1]);
-        #endif
-        token = strtok(NULL, space);
-        if (token != NULL) {
-          current[count1] = (float) atof(token);
-          if ((current[count1] < 0) && (current[count1] > -0.5))
-            current[count1] *= (-1.0f);
-          #ifdef DEBUG_LOGGING
-          //		 printf("current: %f\n", current[count1]);
-          #endif
-          token = strtok(NULL, space);
-        }
-      }
-    }
-
-    //	 printf("\n"); 	  
-
-    batteryVoltage = voltage[map[BAT]];
-    if (batteryVoltage < 3.5) {
-      NormalModeFailure = 1;
-      printf("Safe Mode!\n");
-    } else
-      NormalModeFailure = 0;
-
-    FILE * cpuTempSensor = fopen("/sys/class/thermal/thermal_zone0/temp", "r");
-    if (cpuTempSensor) {
-      double cpuTemp;
-      fscanf(cpuTempSensor, "%lf", & cpuTemp);
-      cpuTemp /= 1000;
-
-      #ifdef DEBUG_LOGGING
-      printf("CPU Temp Read: %6.1f\n", cpuTemp);
-      #endif
-
-      other[IHU_TEMP] = (double)cpuTemp;
-
-      //    IHUcpuTemp = (int)((cpuTemp * 10.0) + 0.5);
-    }
-    fclose(cpuTempSensor);
-
-    char sensor_payload[500];
-
-    if (payload == ON) {
-      STEMBoardFailure = 0;
-
-      char c;
-      int charss = (char) serialDataAvail(uart_fd);
-      if (charss != 0)
-        printf("Clearing buffer of %d chars \n", charss);
-      while ((charss--> 0))
-        c = (char) serialGetchar(uart_fd); // clear buffer
-
-      unsigned int waitTime;
-      int i = 0;
-      serialPutchar(uart_fd, '?');
-      printf("Querying payload with ?\n");
-      waitTime = millis() + 500;
-      int end = FALSE;
-      //     int retry = FALSE;
-      while ((millis() < waitTime) && !end) {
-        int chars = (char) serialDataAvail(uart_fd);
-        while ((chars--> 0) && !end) {
-          c = (char) serialGetchar(uart_fd);
-          //	  printf ("%c", c);
-          //	  fflush(stdout);
-          if (c != '\n') {
-            sensor_payload[i++] = c;
-          } else {
-            end = TRUE;
-          }
-        }
-      }
-      sensor_payload[i++] = ' ';
-      //    sensor_payload[i++] = '\n';
-      sensor_payload[i] = '\0';
-      printf("Payload string: %s \n", sensor_payload);
-
-      if ((sensor_payload[0] == 'O') && (sensor_payload[1] == 'K')) // only process if valid payload response
-      {
-        int count1;
-        char * token;
-        //   char cmdbuffer[1000];
-
-        //	FILE *file = popen("python3 /home/pi/CubeSatSim/python/voltcurrent.py 1 11", "r");	
-        //    	fgets(cmdbuffer, 1000, file);
-        //	printf("result: %s\n", cmdbuffer);
-        //    	pclose(file);
-
-        const char space[2] = " ";
-        token = strtok(sensor_payload, space);
-        for (count1 = 0; count1 < 17; count1++) {
-          if (token != NULL) {
-            sensor[count1] = (float) atof(token);
-            #ifdef DEBUG_LOGGING
-            printf("sensor: %f ", sensor[count1]);
-            #endif
-            token = strtok(NULL, space);
-          }
-        }
-        printf("\n");
-
-      }
-
-    }
-
-    if (sim_mode) {
-      // simulated telemetry 
+    memset(other, 0, sizeof(other));	
+	  
+    FILE * uptime_file = fopen("/proc/uptime", "r");
+    fscanf(uptime_file, "%f", & uptime_sec);
+    uptime = (int) uptime_sec;
+//    #ifdef DEBUG_LOGGING
+//    printf("INFO: Reset Count: %d Uptime since Reset: %ld \n", reset_count, uptime);
+//    #endif
+    fclose(uptime_file);	
+	  
+    if (sim_mode) { // simulated telemetry 
 
       double time = ((long int)millis() - time_start) / 1000.0;
 
@@ -1200,11 +1149,6 @@ void get_tlm_fox() {
         printf("\n\nSwitching eclipse mode! \n\n");
       }
 
-      /*
-        double Xi = eclipse * amps_max[0] * sin(2.0 * 3.14 * time / (46.0 * speed)) * fabs(sin(2.0 * 3.14 * time / (46.0 * speed))) + rnd_float(-2, 2);	  
-        double Yi = eclipse * amps_max[1] * sin((2.0 * 3.14 * time / (46.0 * speed)) + (3.14/2.0)) * fabs(sin((2.0 * 3.14 * time / (46.0 * speed)) + (3.14/2.0))) + rnd_float(-2, 2);	  
-        double Zi = eclipse * amps_max[2] * sin((2.0 * 3.14 * time / (46.0 * speed)) + 3.14 + angle[2])  * fabs(sin((2.0 * 3.14 * time / (46.0 * speed)) + 3.14 + angle[2])) + rnd_float(-2, 2);
-      */
       double Xi = eclipse * amps_max[0] * (float) sin(2.0 * 3.14 * time / (46.0 * speed)) + rnd_float(-2, 2);
       double Yi = eclipse * amps_max[1] * (float) sin((2.0 * 3.14 * time / (46.0 * speed)) + (3.14 / 2.0)) + rnd_float(-2, 2);
       double Zi = eclipse * amps_max[2] * (float) sin((2.0 * 3.14 * time / (46.0 * speed)) + 3.14 + angle[2]) + rnd_float(-2, 2);
@@ -1261,79 +1205,214 @@ void get_tlm_fox() {
 
       // end of simulated telemetry
     }
+    else {
+      int count1;
+      char * token;
+//    char cmdbuffer[1000];
+/**/
+//    FILE * file = popen(pythonStr, "r");
+      fputc('\n', file1);
+      fgets(cmdbuffer, 1000, file1);
+      fprintf(stderr, "Python read Result: %s\n", cmdbuffer);
+//    pclose(file);
+/**/
+      const char space[2] = " ";
+      token = strtok(cmdbuffer, space);
+
+      for (count1 = 0; count1 < 8; count1++) {
+        if (token != NULL) {
+          voltage[count1] = (float) atof(token);
+          #ifdef DEBUG_LOGGING
+          //  printf("voltage: %f ", voltage[count1]);
+          #endif
+          token = strtok(NULL, space);
+          if (token != NULL) {
+            current[count1] = (float) atof(token);
+            if ((current[count1] < 0) && (current[count1] > -0.5))
+              current[count1] *= (-1.0f);
+            #ifdef DEBUG_LOGGING
+            //  printf("current: %f\n", current[count1]);
+            #endif
+            token = strtok(NULL, space);
+          }
+        }
+      }
+    //	 printf("\n"); 	  
+	
+//   sleep(0.5);
+//    printf("Sleep over\n");	
+	
+      batteryVoltage = voltage[map[BAT]];
+      if (batteryVoltage < 3.5) {
+        NormalModeFailure = 1;
+        printf("Safe Mode!\n");
+      } else
+        NormalModeFailure = 0;
 
-    for (count1 = 0; count1 < 8; count1++) {
-      if (voltage[count1] < voltage_min[count1])
-        voltage_min[count1] = voltage[count1];
-      if (current[count1] < current_min[count1])
-        current_min[count1] = current[count1];
-
-      if (voltage[count1] > voltage_max[count1])
-        voltage_max[count1] = voltage[count1];
-      if (current[count1] > current_max[count1])
-        current_max[count1] = current[count1];
+      FILE * cpuTempSensor = fopen("/sys/class/thermal/thermal_zone0/temp", "r");
+      if (cpuTempSensor) {
+        double cpuTemp;
+        fscanf(cpuTempSensor, "%lf", & cpuTemp);
+        cpuTemp /= 1000;
 
-      printf("Vmin %f Vmax %f Imin %f Imax %f \n", voltage_min[count1], voltage_max[count1], current_min[count1], current_max[count1]);
-    }
+        #ifdef DEBUG_LOGGING
+//        printf("CPU Temp Read: %6.1f\n", cpuTemp);
+        #endif
 
-    if ((sensor_payload[0] == 'O') && (sensor_payload[1] == 'K')) {
-      for (count1 = 0; count1 < 17; count1++) {
-        if (sensor[count1] < sensor_min[count1])
-          sensor_min[count1] = sensor[count1];
-        if (sensor[count1] > sensor_max[count1])
-          sensor_max[count1] = sensor[count1];
+        other[IHU_TEMP] = (double)cpuTemp;
 
-        printf("Smin %f Smax %f \n", sensor_min[count1], sensor_max[count1]);
+      //  IHUcpuTemp = (int)((cpuTemp * 10.0) + 0.5);
       }
-    }
+      fclose(cpuTempSensor);
 
-    for (count1 = 0; count1 < 3; count1++) {
-      if (other[count1] < other_min[count1])
-        other_min[count1] = other[count1];
-      if (other[count1] > other_max[count1])
-        other_max[count1] = other[count1];
+      if (payload == ON) {  // -55
+        STEMBoardFailure = 0;
 
-      printf("Other min %f max %f \n", other_min[count1], other_max[count1]);
-    }
+        char c;
+        int charss = (char) serialDataAvail(uart_fd);
+        if (charss != 0)
+        printf("Clearing buffer of %d chars \n", charss);
+        while ((charss--> 0))
+          c = (char) serialGetchar(uart_fd); // clear buffer
+/*	      
+        charss = (char) serialDataAvail(uart_fd);
+        if (charss != 0)
+        printf("Clearing buffer of %d chars \n", charss);
+        while ((charss--> 0))
+          c = (char) serialGetchar(uart_fd); // clear buffer
+*/	      
+
+        unsigned int waitTime;
+        int i = 0;
+        serialPutchar(uart_fd, '?');
+//        printf("Querying payload with ?\n");
+        waitTime = millis() + 500;
+        int end = FALSE;
+        //  int retry = FALSE;
+        while ((millis() < waitTime) && !end) {
+          int chars = (char) serialDataAvail(uart_fd);
+          while ((chars--> 0) && !end) {
+            c = (char) serialGetchar(uart_fd);
+            //	printf ("%c", c);
+            //	fflush(stdout);
+            if (c != '\n') {
+              sensor_payload[i++] = c;
+            } else {
+              end = TRUE;
+            }
+          }
+        }
+        sensor_payload[i++] = ' ';
+        //  sensor_payload[i++] = '\n';
+        sensor_payload[i] = '\0';
+        printf("Payload string: %s", sensor_payload);
 
-   if (mode == FSK) {	  
-    if (loop % 8 == 0) {
-      printf("Sending MIN frame \n");
-      frm_type = 0x03;
-      for (count1 = 0; count1 < 17; count1++) {
-        if (count1 < 3)
-          other[count1] = other_min[count1];
-        if (count1 < 8) {
-          voltage[count1] = voltage_min[count1];
-          current[count1] = current_min[count1];
+        if ((sensor_payload[0] == 'O') && (sensor_payload[1] == 'K')) // only process if valid payload response
+        {
+          int count1;
+          char * token;
+          //  char cmdbuffer[1000];
+
+        //	FILE *file = popen("python3 /home/pi/CubeSatSim/python/voltcurrent.py 1 11", "r");	
+        //    	fgets(cmdbuffer, 1000, file);
+        //	printf("result: %s\n", cmdbuffer);
+        //    	pclose(file);
+
+          const char space[2] = " ";
+          token = strtok(sensor_payload, space);
+          for (count1 = 0; count1 < 17; count1++) {
+            if (token != NULL) {
+              sensor[count1] = (float) atof(token);
+              #ifdef DEBUG_LOGGING
+              //  printf("sensor: %f ", sensor[count1]);
+              #endif
+              token = strtok(NULL, space);
+            }
+          }
+          printf("\n");
         }
-        if (sensor_min[count1] != 1000.0) // make sure values are valid
-          sensor[count1] = sensor_min[count1];
       }
-    }
-    if ((loop + 4) % 8 == 0) {
-      printf("Sending MAX frame \n");
-      frm_type = 0x02;
-      for (count1 = 0; count1 < 17; count1++) {
-        if (count1 < 3)
-          other[count1] = other_max[count1];
-        if (count1 < 8) {
-          voltage[count1] = voltage_max[count1];
-          current[count1] = current_max[count1];
-        }
-        if (sensor_max[count1] != -1000.0) // make sure values are valid
-          sensor[count1] = sensor_max[count1];
+      if ((sensor_payload[0] == 'O') && (sensor_payload[1] == 'K')) {
+        for (count1 = 0; count1 < 17; count1++) {
+          if (sensor[count1] < sensor_min[count1])
+            sensor_min[count1] = sensor[count1];
+          if (sensor[count1] > sensor_max[count1])
+            sensor_max[count1] = sensor[count1];
+            //  printf("Smin %f Smax %f \n", sensor_min[count1], sensor_max[count1]);
+        }   	    
       }
     }
-   }
+//    if (mode == FSK) 
+    {  // just moved
+      for (int count1 = 0; count1 < 8; count1++) {
+        if (voltage[count1] < voltage_min[count1])
+          voltage_min[count1] = voltage[count1];
+        if (current[count1] < current_min[count1])
+          current_min[count1] = current[count1];
+	      
+        if (voltage[count1] > voltage_max[count1])
+          voltage_max[count1] = voltage[count1];
+        if (current[count1] > current_max[count1])
+          current_max[count1] = current[count1];
+
+//         printf("Vmin %4.2f Vmax %4.2f Imin %4.2f Imax %4.2f \n", voltage_min[count1], voltage_max[count1], current_min[count1], current_max[count1]);
+      }
+       for (int count1 = 0; count1 < 3; count1++) {
+        if (other[count1] < other_min[count1])
+          other_min[count1] = other[count1];
+        if (other[count1] > other_max[count1])
+          other_max[count1] = other[count1];
+
+        //  printf("Other min %f max %f \n", other_min[count1], other_max[count1]);
+      }
+      	  if (mode == FSK)
+	  {
+	      if (loop % 8 == 0) {
+		printf("Sending MIN frame \n");
+		frm_type = 0x03;
+		for (int count1 = 0; count1 < 17; count1++) {
+		  if (count1 < 3)
+		    other[count1] = other_min[count1];
+		  if (count1 < 8) {
+		    voltage[count1] = voltage_min[count1];
+		    current[count1] = current_min[count1];
+		  }
+		  if (sensor_min[count1] != 1000.0) // make sure values are valid
+		    sensor[count1] = sensor_min[count1];
+		}
+	      }
+	      if ((loop + 4) % 8 == 0) {
+		printf("Sending MAX frame \n");
+		frm_type = 0x02;
+		for (int count1 = 0; count1 < 17; count1++) {
+		  if (count1 < 3)
+		    other[count1] = other_max[count1];
+		  if (count1 < 8) {
+		    voltage[count1] = voltage_max[count1];
+		    current[count1] = current_max[count1];
+		  }
+		  if (sensor_max[count1] != -1000.0) // make sure values are valid
+		    sensor[count1] = sensor_max[count1];
+		}
+	      }
+	  }
+	  else
+	  	frm_type = 0x02;  // BPSK always send MAX MIN frame
+    }  
+	  
+//   if (mode == FSK) {	// remove this 
+//   }
     memset(rs_frame, 0, sizeof(rs_frame));
     memset(parities, 0, sizeof(parities));
-
+/*
     FILE * uptime_file = fopen("/proc/uptime", "r");
     fscanf(uptime_file, "%f", & uptime_sec);
     uptime = (int) uptime_sec;
     fclose(uptime_file);
     printf("Reset Count: %d Uptime since Reset: %ld \n", reset_count, uptime);
+*/	  
+    //sleep(1);
+    //printf("Sleep over\n");
 
     h[0] = (short int) ((h[0] & 0xf8) | (id & 0x07)); // 3 bits
     //    printf("h[0] %x\n", h[0]);
@@ -1368,7 +1447,6 @@ void get_tlm_fox() {
     negZv = (int)(voltage[map[MINUS_Z]] * 100);
 
     batt_c_v = (int)(voltage[map[BAT]] * 100);
-
     battCurr = (int)(current[map[BAT]] + 0.5) + 2048;
     PSUVoltage = (int)(voltage[map[BUS]] * 100);
     PSUCurrent = (int)(current[map[BUS]] + 0.5) + 2048;
@@ -1376,9 +1454,6 @@ void get_tlm_fox() {
     if (payload == ON)
       STEMBoardFailure = 0;
 
-    //  if (payload == ON)
-    //	  STEMBoardFailure = 0;
-
     // read payload sensor if available
 
     encodeA(b, 0 + head_offset, batt_a_v);
@@ -1427,8 +1502,122 @@ void get_tlm_fox() {
       encodeB(b, 25 + head_offset, negXi);
       encodeA(b, 27 + head_offset, negYi);
       encodeB(b, 28 + head_offset, negZi);
-    }
-
+	    
+      encodeA(b_max, 12 + head_offset, (int)(voltage_max[map[PLUS_X]] * 100));
+      encodeB(b_max, 13 + head_offset, (int)(voltage_max[map[PLUS_Y]] * 100));
+      encodeA(b_max, 15 + head_offset, (int)(voltage_max[map[PLUS_Z]] * 100));
+      encodeB(b_max, 16 + head_offset, (int)(voltage_max[map[MINUS_X]] * 100));
+      encodeA(b_max, 18 + head_offset, (int)(voltage_max[map[MINUS_Y]] * 100));
+      encodeB(b_max, 19 + head_offset, (int)(voltage_max[map[MINUS_Z]] * 100));
+
+      encodeA(b_max, 21 + head_offset, (int)(current_max[map[PLUS_X]] + 0.5) + 2048);
+      encodeB(b_max, 22 + head_offset, (int)(current_max[map[PLUS_Y]] + 0.5) + 2048);
+      encodeA(b_max, 24 + head_offset, (int)(current_max[map[PLUS_Z]] + 0.5) + 2048);
+      encodeB(b_max, 25 + head_offset, (int)(current_max[map[MINUS_X]] + 0.5) + 2048);
+      encodeA(b_max, 27 + head_offset, (int)(current_max[map[MINUS_Y]] + 0.5) + 2048);
+      encodeB(b_max, 28 + head_offset, (int)(current_max[map[MINUS_Z]] + 0.5) + 2048);	    
+
+      encodeA(b_max, 9 + head_offset, (int)(current_max[map[BAT]] + 0.5) + 2048);
+      encodeA(b_max, 3 + head_offset, (int)(voltage_max[map[BAT]] * 100));
+      encodeA(b_max, 30 + head_offset, (int)(voltage_max[map[BUS]] * 100));
+      encodeB(b_max, 46 + head_offset, (int)(current_max[map[BUS]] + 0.5) + 2048);
+	    
+      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
+      {	        	    
+	      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
+	      encodeB(b_max, 7 + head_offset, (int)(sensor_max[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel	    
+
+	      encodeA(b_max, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure
+	      encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] * 10.0 + 0.5)); // Altitude
+	      encodeB(b_max, 40 + head_offset, (int)(sensor_max[GYRO_X] + 0.5) + 2048);
+	      encodeA(b_max, 42 + head_offset, (int)(sensor_max[GYRO_Y] + 0.5) + 2048);
+	      encodeB(b_max, 43 + head_offset, (int)(sensor_max[GYRO_Z] + 0.5) + 2048);
+
+	      encodeA(b_max, 48 + head_offset, (int)(sensor_max[XS2]) + 2048);
+	      encodeB(b_max, 49 + head_offset, (int)(sensor_max[XS3] * 100 + 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));
+      }	  
+      else
+      {	        	    
+	      encodeB(b_max, 4 + head_offset, 2048); // 0
+	      encodeA(b_max, 6 + head_offset, 2048); // 0
+	      encodeB(b_max, 7 + head_offset, 2048); // 0	    
+
+//	      encodeA(b_max, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure
+//	      encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] * 10.0 + 0.5)); // Altitude
+	      encodeB(b_max, 40 + head_offset, 2048);
+	      encodeA(b_max, 42 + head_offset, 2048);
+	      encodeB(b_max, 43 + head_offset, 2048);
+
+	      encodeA(b_max, 48 + head_offset, 2048);
+	      encodeB(b_max, 49 + head_offset, 2048);
+//	      encodeB(b_max, 10 + head_offset, (int)(sensor_max[TEMP] * 10 + 0.5)); 	
+//	      encodeA(b_max, 45 + head_offset, (int)(sensor_max[HUMI] + 0.5));
+      }	  	      
+      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));
+      encodeA(b_min, 15 + head_offset, (int)(voltage_min[map[PLUS_Z]] * 100));
+      encodeB(b_min, 16 + head_offset, (int)(voltage_min[map[MINUS_X]] * 100));
+      encodeA(b_min, 18 + head_offset, (int)(voltage_min[map[MINUS_Y]] * 100));
+      encodeB(b_min, 19 + head_offset, (int)(voltage_min[map[MINUS_Z]] * 100));
+
+      encodeA(b_min, 21 + head_offset, (int)(current_min[map[PLUS_X]] + 0.5) + 2048);
+      encodeB(b_min, 22 + head_offset, (int)(current_min[map[PLUS_Y]] + 0.5) + 2048);
+      encodeA(b_min, 24 + head_offset, (int)(current_min[map[PLUS_Z]] + 0.5) + 2048);
+      encodeB(b_min, 25 + head_offset, (int)(current_min[map[MINUS_X]] + 0.5) + 2048);
+      encodeA(b_min, 27 + head_offset, (int)(current_min[map[MINUS_Y]] + 0.5) + 2048);
+      encodeB(b_min, 28 + head_offset, (int)(current_min[map[MINUS_Z]] + 0.5) + 2048);	
+	    
+      encodeA(b_min, 9 + head_offset, (int)(current_min[map[BAT]] + 0.5) + 2048);
+      encodeA(b_min, 3 + head_offset, (int)(voltage_min[map[BAT]] * 100));
+      encodeA(b_min, 30 + head_offset, (int)(voltage_min[map[BUS]] * 100));
+      encodeB(b_min, 46 + head_offset, (int)(current_min[map[BUS]] + 0.5) + 2048);
+	    
+      encodeB(b_min, 31 + head_offset, ((int)(other_min[SPIN] * 10)) + 2048);
+      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
+      {	        
+	      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
+	      encodeB(b_min, 7 + head_offset, (int)(sensor_min[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel	
+
+	      encodeA(b_min, 33 + head_offset, (int)(sensor_min[PRES] + 0.5)); // Pressure
+	      encodeB(b_min, 34 + head_offset, (int)(sensor_min[ALT] * 10.0 + 0.5)); // Altitude
+	      encodeB(b_min, 40 + head_offset, (int)(sensor_min[GYRO_X] + 0.5) + 2048);
+	      encodeA(b_min, 42 + head_offset, (int)(sensor_min[GYRO_Y] + 0.5) + 2048);
+	      encodeB(b_min, 43 + head_offset, (int)(sensor_min[GYRO_Z] + 0.5) + 2048);
+
+	      encodeA(b_min, 48 + head_offset, (int)(sensor_min[XS2]) + 2048);
+	      encodeB(b_min, 49 + head_offset, (int)(sensor_min[XS3] * 100 + 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));
+    }      
+      else
+      {	        	    
+	      encodeB(b_min, 4 + head_offset, 2048); // 0
+	      encodeA(b_min, 6 + head_offset, 2048); // 0
+	      encodeB(b_min, 7 + head_offset, 2048); // 0	    
+
+//	      encodeA(b_min, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure
+//	      encodeB(b_min, 34 + head_offset, (int)(sensor_max[ALT] * 10.0 + 0.5)); // Altitude
+	      encodeB(b_min, 40 + head_offset, 2048);
+	      encodeA(b_min, 42 + head_offset, 2048);
+	      encodeB(b_min, 43 + head_offset, 2048);
+
+	      encodeA(b_min, 48 + head_offset, 2048);
+	      encodeB(b_min, 49 + head_offset, 2048);
+//	      encodeB(b_min, 10 + head_offset, (int)(sensor_max[TEMP] * 10 + 0.5)); 	
+//	      encodeA(b_min, 45 + head_offset, (int)(sensor_max[HUMI] + 0.5));
+      }	 
+    }    
     encodeA(b, 30 + head_offset, PSUVoltage);
     //  encodeB(b, 31 + head_offset,(spin * 10) + 2048);	  
     encodeB(b, 31 + head_offset, ((int)(other[SPIN] * 10)) + 2048);
@@ -1478,10 +1667,14 @@ void get_tlm_fox() {
       printf("TX Antenna Deployed!\n");
     }
     
-    if (mode == BPSK) {  // WOD field experiments
-      encodeA(b, 63 + head_offset, 0xff);  
-      encodeB(b, 74 + head_offset, 0xff);	
-    }
+    if (mode == BPSK) {  // wod field experiments
+      unsigned long val = 0xffff;
+      encodeA(b, 64 + head_offset, 0xff & val); 
+      encodeA(b, 65 + head_offset, val >> 8); 	    
+      encodeA(b, 63 + head_offset, 0x00); 
+      encodeA(b, 62 + head_offset, 0x01);
+      encodeB(b, 74 + head_offset, 0xfff); 
+    }	  
     short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)];
     short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)];
 
@@ -1498,8 +1691,29 @@ void get_tlm_fox() {
             data8[ctr1++] = rs_frame[j][i];
             //				printf ("data8[%d] = %x \n", ctr1 - 1, rs_frame[j][i]);
           } else {
-            rs_frame[j][i] = b[ctr3 % dataLen];
-            update_rs(parities[j], b[ctr3 % dataLen]);
+	     if (mode == FSK)
+	     {
+            	rs_frame[j][i] = b[ctr3 % dataLen];
+            	update_rs(parities[j], b[ctr3 % dataLen]);
+	     }  else // BPSK
+		if ((int)(ctr3/dataLen) == 3)  
+		{
+            		rs_frame[j][i] = b_max[ctr3 % dataLen];
+            		update_rs(parities[j], b_max[ctr3 % dataLen]);
+		}
+		else if ((int)(ctr3/dataLen) == 4)  
+		{
+            		rs_frame[j][i] = b_min[ctr3 % dataLen];
+            		update_rs(parities[j], b_min[ctr3 % dataLen]);
+		}		
+		else
+		{
+            		rs_frame[j][i] = b[ctr3 % dataLen];
+            		update_rs(parities[j], b[ctr3 % dataLen]);
+		}
+	     {
+	    }
+		  
             //  				printf("%d rs_frame[%d][%d] = %x %d \n", 
             //  					ctr1, j, i, b[ctr3 % DATA_LEN], ctr3 % DATA_LEN);
             data8[ctr1++] = rs_frame[j][i];
@@ -1520,6 +1734,9 @@ void get_tlm_fox() {
     		printf("\n");
     */
     #endif
+	   
+    //sleep(1);
+    //printf("Sleep over\n");
 
     int ctr2 = 0;
     memset(data10, 0, sizeof(data10));
@@ -1659,15 +1876,30 @@ void get_tlm_fox() {
 
   if (!error && transmit) {
     //	digitalWrite (0, LOW);
-    printf("Sending %d buffer bytes over socket after %d ms!\n", ctr, (long unsigned int)millis() - start);
+ //   printf("Sending %d buffer bytes over socket after %d ms!\n", ctr, (long unsigned int)millis() - start);
     start = millis();
     int sock_ret = send(sock, buffer, (unsigned int)(ctr * 2 + 2), 0);
-    printf("Millis5: %d Result of socket send: %d \n", (unsigned int)millis() - start, sock_ret);
-
+    printf("Millis6: %d Result of socket send: %d \n\n", (unsigned int)millis() - start, sock_ret);
+    
     if (sock_ret < (ctr * 2 + 2)) {
-      printf("Not resending\n");
-      //	 	sock_ret = send(sock, buffer[sock_ret], ctr * 2 + 2 - sock_ret, 0);
-      //       		printf("Millis10: %d Result of socket send: %d \n", millis() - start, sock_ret);
+  //    printf("Not resending\n");
+      sleep(0.5);
+      sock_ret = send(sock, &buffer[sock_ret], (unsigned int)(ctr * 2 + 2 - sock_ret), 0);
+      printf("Millis7: %d Result of socket send: %d \n\n", millis() - start, sock_ret);
+    }
+    
+    if (mode == BPSK)
+    {	  
+      start = millis();  // send frame a second time
+      sock_ret = send(sock, buffer, (unsigned int)(ctr * 2 + 2), 0);
+      printf("Millis8: %d Result of socket send: %d \n\n", (unsigned int)millis() - start, sock_ret);
+    
+      if (sock_ret < (ctr * 2 + 2)) {
+  //    printf("Not resending\n");
+        sleep(0.5);
+        sock_ret = send(sock, &buffer[sock_ret], (unsigned int)(ctr * 2 + 2 - sock_ret), 0);
+        printf("Millis9: %d Result of socket send: %d \n\n", millis() - start, sock_ret);
+      }
     }
 
     if (sock_ret == -1) {
@@ -1682,13 +1914,42 @@ void get_tlm_fox() {
   }
   //    digitalWrite (0, HIGH);
 
-  if (mode == FSK)
-    firstTime = 0;
-  else if (frames_sent > 0) //5)
+//  if (mode == FSK)
     firstTime = 0;
+//  else if (frames_sent > 0) //5)
+//    firstTime = 0;
 
   return;
 }
+
+// code by https://stackoverflow.com/questions/25161377/open-a-cmd-program-with-full-functionality-i-o/25177958#25177958
+
+    FILE *sopen(const char *program)
+    {
+        int fds[2];
+        pid_t pid;
+
+        if (socketpair(AF_UNIX, SOCK_STREAM, 0, fds) < 0)
+            return NULL;
+
+        switch(pid=vfork()) {
+        case -1:    /* Error */
+            close(fds[0]);
+            close(fds[1]);
+            return NULL;
+        case 0:     /* child */
+            close(fds[0]);
+            dup2(fds[1], 0);
+            dup2(fds[1], 1);
+            close(fds[1]);
+            execl("/bin/sh", "sh", "-c", program, NULL);
+            _exit(127);
+        }
+        /* parent */
+        close(fds[1]);
+        return fdopen(fds[0], "r+");
+    }
+
  /*
  * TelemEncoding.h
  *
@@ -1889,10 +2150,11 @@ void write_wave(int i, short int *buffer)
 		else
 		{
 			if ((ctr - flip_ctr) < smaller)
-  		 		buffer[ctr++] = (short int)(amplitude * 0.4 * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE))); 					
- 			else
- 		 		buffer[ctr++] = (short int)(amplitude * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE)));
- 		 } 			
+//  		 		buffer[ctr++] = (short int)(amplitude * 0.4 * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE)));	 	  		 		buffer[ctr++] = (short int)(amplitude * 0.4 * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE)));	
+  		 		buffer[ctr++] = (short int)(phase * sin_map[ctr % sin_samples] / 2);
+		else
+//  		 		buffer[ctr++] = (short int)(amplitude * 0.4 * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE)));	 	 		 		buffer[ctr++] = (short int)(amplitude * phase * sin((float)(2*M_PI*i*freq_Hz/S_RATE)));	
+  		 		buffer[ctr++] = (short int)(phase * sin_map[ctr % sin_samples]); 		 } 			
 //		printf("%d %d \n", i, buffer[ctr - 1]);
 
 }
@@ -1955,7 +2217,7 @@ int test_i2c_bus(int bus)
 //      	 	printf("%s error: %d \n", &command, error);
     	 	if (error != 0) 
     	 	{	
-    	 		printf("ERROR: %sd bus has a problem \n  Check I2C wiring and pullup resistors \n", busDev);
+    	 		printf("ERROR: %s bus has a problem \n  Check I2C wiring and pullup resistors \n", busDev);
 			output = -1;
     		}													
 	} else
diff --git a/arduino/Payload_BME280_MPU6050_XS.ino b/arduino/Payload_BME280_MPU6050_XS.ino
index b7280828..9173fa97 100644
--- a/arduino/Payload_BME280_MPU6050_XS.ino
+++ b/arduino/Payload_BME280_MPU6050_XS.ino
@@ -81,6 +81,8 @@ void setup() {
     Serial.println(((float)eeprom_word_read(2)) / 100.0, DEC);
     Serial.println(((float)eeprom_word_read(3)) / 100.0, DEC);
   }
+  pinMode(greenLED, OUTPUT);
+  pinMode(blueLED, OUTPUT);
 }
 
 void loop() {
@@ -271,7 +273,7 @@ void blink(int length)
 
 #if defined __AVR_ATmega32U4__
   digitalWrite(RXLED, HIGH);    // set the RX LED OFF
-  TXLED0; //TX LED is not tied to a normally controlled pin so a macro is needed, turn LED OFF
+  TXLED0; //TX LED macro to turn LED ON
 #endif  
 }
 
diff --git a/config b/config
new file mode 100755
index 00000000..d881c326
--- /dev/null
+++ b/config
@@ -0,0 +1,209 @@
+#!/bin/bash
+
+# echo $1
+
+if [ "$1" = "" ]; then
+	echo "Include a configuration option:"
+	echo
+	set -- "-h"
+fi	
+
+if [ "$1" = "-i" ]; then
+	echo "Restarting CubeSatSim"
+	sudo systemctl restart cubesatsim
+	exit 
+elif [ "$1" = "-a" ]; then
+	echo "changing CubeSatSim to AFSK mode"
+	sudo echo "ARG1=a" > .mode	
+	sudo systemctl restart cubesatsim
+	exit 
+elif [ "$1" = "-f" ]; then
+	echo "changing CubeSatSim to FSK mode"
+	sudo echo "ARG1=f" > .mode	
+	sudo systemctl restart cubesatsim
+	exit 
+elif [ "$1" = "-b" ]; then
+	echo "changing CubeSatSim to BPSK mode"
+	sudo echo "ARG1=b" > .mode	
+	sudo systemctl restart cubesatsim
+	exit 
+elif [ "$1" = "-s" ]; then
+	echo "changing CubeSatSim to SSTV mode"
+	sudo echo "ARG1=s" > .mode	
+	sudo systemctl restart cubesatsim
+	exit 
+elif [ "$1" = "-h" ]; then
+	echo "config OPTION"
+	echo
+	echo "Changes CubeSatSim mode, resets, or modifies configuration file"
+	echo 
+	echo "   -h     This help info"
+	echo "   -a     Change to AFSK/APRS mode"
+	echo "   -f     Change to FSK/DUV mode"
+	echo "   -b     Change to BPSK mode"
+	echo "   -s     Change to SSTV mode"
+	echo "   -i     Restarts CubeSatsim software"
+	echo "   -c     Change the CALLSIGN in the configuration file sim.cfg"
+	echo "   -r     Change the Resets Count in the configuration file sim.cfg"
+	echo "   -l     Change the Latitude and Longitude in the configuration file sim.cfg"
+	echo "          Only used for APRS telemetry"
+	echo
+	exit
+
+elif [ "$1" = "-c" ]; then
+
+	echo	
+	echo "Editing the CALLSIGN in the"
+	echo  "configuration file for CubeSatSim"	
+	echo
+	echo "Return keeps current value."
+#	echo -e "Current sim.cfg configuration file:"	
+#	echo
+	
+	value=`cat /home/pi/CubeSatSim/sim.cfg`
+	echo "$value" > /dev/null
+	set -- $value
+
+	echo "Current value of CALLSIGN is"	
+	echo $1
+	echo
+	
+#	echo $1 $2 $3 $4
+
+	echo "Enter callsign in all capitals: "
+	read callsign
+
+	if [ -z $callsign ] ; then
+
+		callsign="$1"
+		echo "Keeping value of" $callsign
+	fi
+	
+	echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
+
+	echo $callsign $2 $3 $4
+	echo $callsign $2 $3 $4 > /home/pi/CubeSatSim/sim.cfg
+	echo
+	echo "Restarting CubeSatSim with new configuraation file"
+	echo
+
+	sudo systemctl restart cubesatsim
+	
+elif [ "$1" = "-r" ]; then
+
+	echo	
+	echo "Editing the Reset Count in the"
+	echo  "configuration file for CubeSatSim"	
+	echo
+	echo "Return keeps current value."
+#	echo -e "Current sim.cfg configuration file:"	
+#	echo
+	
+	value=`cat /home/pi/CubeSatSim/sim.cfg`
+	echo "$value" > /dev/null
+	set -- $value
+	
+	echo
+	echo "Current value of Reset Count is"	
+	echo $2
+	echo
+	
+#	echo $1 $2 $3 $4
+
+	echo -e "Enter Reset Count (integer): "
+
+	read resets
+
+	if [ -z $resets ] ; then
+		resets="$2"
+		echo "Keeping value of" $resets
+	fi
+
+	if ! [[ $resets =~ ^[0-9]+$ ]] ; then
+		echo "Error: not an integer!"
+		resets="$2"
+		echo "Keeping value of" $resets
+	fi 
+
+	echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
+
+	echo $1 $resets $3 $4
+	echo $1 $resets $3 $4 > /home/pi/CubeSatSim/sim.cfg
+	echo
+	echo "Restarting CubeSatSim with new configuraation file"
+	echo
+	
+	sudo systemctl restart cubesatsim
+	
+elif [ "$1" = "-l" ]; then
+
+	echo	
+	echo "Editing latitude and longitude in the"
+	echo "configuration file for CubeSatSim"
+	echo "(Only used for APRS telemetry)"
+	echo
+	echo "Return keeps current value."
+#	echo -e "Current sim.cfg configuration file:"	
+#	echo
+	
+	value=`cat /home/pi/CubeSatSim/sim.cfg`
+	echo "$value" > /dev/null
+	set -- $value
+
+	echo
+	echo "Current value of latitude is"	
+	echo $3
+	echo
+	
+#	echo $1 $2 $3 $4
+
+	echo -e "Enter latitude  (decimal degrees, positive is north): "
+
+	read lat 
+
+	if [ -z $lat ] ; then
+
+		lat="$3"
+		echo "Keeping value of" $lat
+	fi
+
+	if ! [[ $lat =~ ^[+-]?[0-9]+([.][0-9]+)?$ ]] ; then
+
+		echo "Error: not a number!"
+		lat="$3"
+		echo "Keeping value of" $lat
+	fi 
+	
+	echo
+	echo "Current value of longitude is"	
+	echo $4
+	echo
+
+	echo -e "Enter longitude (decimal degrees, positive is east): "
+
+	read long 
+
+	if [ -z $long ] ; then
+
+		long="$4"
+		echo "Keeping value of" $long
+	fi
+
+	if ! [[ $long =~ ^[+-]?[0-9]+([.][0-9]+)?$ ]] ; then
+
+		echo "Error: not a number!"
+		long="$4"
+		echo "Keeping value of" $long
+	fi 
+
+	echo -e "\nCubeSatSim configuraation sim.cfg file updated to: \n"
+	echo $1 $2 $lat $long
+	echo $1 $2 $lat $long > /home/pi/CubeSatSim/sim.cfg
+	echo
+	echo "Restarting CubeSatSim with new configuraation file"
+	echo
+	
+	sudo systemctl restart cubesatsim
+fi
+
+# sudo systemctl restart cubesatsim
diff --git a/demo.sh b/demo.sh
index de318527..84b71b50 100755
--- a/demo.sh
+++ b/demo.sh
@@ -15,8 +15,9 @@ if [[ ("$1" = "a" ) || (("$1" = "c") && ("$(($y %4))" = 3)) ]]; then
    	echo "Mode is continuous AFSK"
     	/home/pi/CubeSatSim/radioafsk afsk
 elif [[ ("$1" = "b" ) || (("$1" = "c") && ("$(($y %4))" = 1)) ]]; then
-   	echo "Mode is continuous BPSK"  
-    	/home/pi/CubeSatSim/radioafsk bpsk
+   	echo "Mode is continuous BPSK" 
+    sudo cpulimit -l 2.5 -b -P radioafsk
+    /home/pi/CubeSatSim/radioafsk bpsk
 elif [[ ("$1" = "s" ) || (("$1" = "c") && ("$(($y %4))" = 2)) ]]; then
    	echo "Mode is continuous SSTV"  
     	while true; do sleep 5; done
diff --git a/log b/log
new file mode 100755
index 00000000..f551c284
--- /dev/null
+++ b/log
@@ -0,0 +1,9 @@
+#!/bin/bash
+
+echo -e "\nLog file script for CubeSatSim\n"
+
+sudo journalctl -u cubesatsim > log.txt 
+cat log.txt
+
+echo -e "\nLog file also saved as /home/pi/CubeSatSim/log.txt"
+
diff --git a/python/voltcurrent.py b/python/voltcurrent.py
index f34e9e52..c5d0fce6 100644
--- a/python/voltcurrent.py
+++ b/python/voltcurrent.py
@@ -1,20 +1,22 @@
 """Sample code and test for adafruit_in219"""
 # Reads all voltage and current sensors for two I2C buses
-
+import time
 import sys
 #import board
 import busio
 from adafruit_extended_bus import ExtendedI2C as I2C
 from adafruit_ina219 import INA219
+from adafruit_ina219 import ADCResolution, BusVoltageRange
 
 if __name__ == "__main__":
 #	    print 'Length: ', len(sys.argv)
   
   buses = [1, 3] # default I2C buses
   config = False
+  one = two = three = four = five = six = seven = eight = 0
   
   if (len(sys.argv)) > 1:
-#   print("There are arguments!")
+#   print("There are arguments!", file=sys.stderr)
 #   if (('a' == sys.argv[1]) or ('afsk' in sys.argv[1])):
     buses[0] = int(sys.argv[1], base=10)
     if (len(sys.argv)) > 2:
@@ -22,45 +24,325 @@ if __name__ == "__main__":
       if (len(sys.argv)) > 3:
         if sys.argv[3] == "c":
           config = True
-          from adafruit_ina219 import ADCResolution, BusVoltageRange
+          
+#  print(buses[0])
+#  print(buses[1])
 
   addresses = [0x40, 0x41, 0x44, 0x45] #INA219 addresses on the bus
-#  print("buses: ", buses, " addr: ", addresses)
-  for x in buses:
-    try:
-      i2c_bus = I2C(x) # Device is /dev/i2c-x
-      for y in addresses:
- #     print(x,y)
-        try:
+#  print("buses: ", buses, " addr: ", addresses, file=sys.stderr)
+
+# config
+
+#  for x in buses:
+#    try:
+#      i2c_bus = I2C(x) # Device is /dev/i2c-x
+#      for y in addresses:
+#        print(x,y)
+#        try:
   # Create library object using  Extended Bus I2C port
-#         print("bus: ", x, " addr: ", y)
-          if x == 0 and y == 0x45:
+#          print("bus: ", x, " addr: ", y)
+#          if x == 0 and y == 0x45:
 #           print("Reading INA219 in MoPower Board")
-            i2c_bus = I2C(1)
-            ina219 = INA219(i2c_bus, 0x4a)
-          else:
-            ina219 = INA219(i2c_bus, y)
-   
-#       print("ina219 test")
-          if config:
-#           print("Configuring")
+#            i2c_bus = I2C(1)
+#            ina219 = INA219(i2c_bus, 0x4a)
+#          else:
+#            ina219 = INA219(i2c_bus, y)
+#          print("ina219 test")
+  
+#          print("Configuring")
 # optional : change configuration to use 32 samples averaging for both bus voltage and shunt voltage
-            ina219.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
-            ina219.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+#          ina219.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+#          ina219.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
 # optional : change voltage range to 16V
-            ina219.bus_voltage_range = BusVoltageRange.RANGE_16V
+#          ina219.bus_voltage_range = BusVoltageRange.RANGE_16V
+#        except:
+#          print("Python Error 2", file=sys.stderr, flush=True)
+#    except:
+#      print("Python Error 1", file=sys.stderr, flush=True)
+# No try checking yet
+  
+#  if buses[0] == 0 and addresses[0] == 0x45:
+#    print("Reading INA219 in MoPower Board")
+#    ina219_one = INA219(I2C(1), 0x4a) 
+#  else:
+  if (buses[0] != -1):
+    try:
+      i2c_one = I2C(buses[0])
+      try:
+        ina219_one = INA219(i2c_one, addresses[0])
+        ina219_one.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_one.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_one.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        one = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        one = 0
+      try:  
+        ina219_two = INA219(i2c_one, addresses[1])
+        ina219_two.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_two.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_two.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        two = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+         two = 0
+  
+      try:  
+        ina219_three = INA219(i2c_one, addresses[2])
+        ina219_three.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_three.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_three.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        three = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        three = 0
+  
+      try:  
+        ina219_four= INA219(i2c_one, addresses[3])
+        ina219_four.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_four.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_four.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        four = 1
+      except:
+        four = 0  
+#        print("Python Error 3", file=sys.stderr, flush=True)
+    except:
+      print("Python Error 5",  file=sys.stderr, flush=True)
+      
+  if (buses[1] != -1):
+    try:
+      i2c_two = I2C(buses[1])
+#      print(i2c_two)
+      try:  
+        ina219_five = INA219(i2c_two, addresses[0])  
+        ina219_five.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_five.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_five.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        five = 1  
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        five = 0
+      try:  
+        ina219_six = INA219(i2c_two, addresses[1]) 
+        ina219_six.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_six.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_six.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        six = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        six = 0
+      try:  
+        ina219_seven = INA219(i2c_two, addresses[2]) 
+        ina219_seven.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_seven.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_seven.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        seven = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        seven = 0
+      try:  
+        ina219_eight = INA219(i2c_two, addresses[3]) 
+        ina219_eight.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_eight.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_eight.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        eight = 1
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        eight = 0
+    except:
+      print("Python Error 5",  file=sys.stderr, flush=True)
+
+  while (True):
+    error = 0
+    try:
+      time.sleep(0.01)
+      print("{:6.3f} ".format(ina219_one.bus_voltage), "{:6.3f} ".format(ina219_one.current) , end = '')
+    except:
+      
+      try:
+        ina219_one = INA219(i2c_one, addresses[0])
+        ina219_one.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_one.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_one.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_one.bus_voltage), "{:6.3f} ".format(ina219_one.current) , end = '')
+        error = 1    
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '') 
+ 
+      
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_two.bus_voltage), "{:6.3f} ".format(ina219_two.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_two = INA219(i2c_one, addresses[1])
+        ina219_two.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_two.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_two.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_two.bus_voltage), "{:6.3f} ".format(ina219_two.current) , end = '') 
+        error = 1   
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '') 
 
-          bus_voltage = ina219.bus_voltage  # voltage on V- (load side)
-#         shunt_voltage = ina219.shunt_voltage  # voltage between V+ and V- across the shunt
-          current = ina219.current  # current in mA
-          if x == 0 and y == 0x45:
-            current = current * 10
-# INA219 measure bus voltage on the load side. So PSU voltage = bus_voltage + shunt_voltage
-#         print("{:6.3f}".format(bus_voltage + shunt_voltage))
-          print("{:6.3f} ".format(bus_voltage), "{:6.3f} ".format(current) , end = '')    
-        except:
-          print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '')
+      
+    try:
+      time.sleep(0.01) 
+      print("{:6.3f} ".format(ina219_three.bus_voltage), "{:6.3f} ".format(ina219_three.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_three = INA219(i2c_one, addresses[2])
+        ina219_three.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_three.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_three.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_three.bus_voltage), "{:6.3f} ".format(ina219_three.current) , end = '') 
+        error = 1    
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '')  
+      
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_four.bus_voltage), "{:6.3f} ".format(ina219_four.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_four= INA219(i2c_one, addresses[3])
+        ina219_four.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_four.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_four.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_four.bus_voltage), "{:6.3f} ".format(ina219_four.current) , end = '') 
+        error = 1    
+        
+      except:
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '')    
+      
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_five.bus_voltage), "{:6.3f} ".format(ina219_five.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_five = INA219(i2c_two, addresses[0])  
+        ina219_five.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_five.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_five.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_five.bus_voltage), "{:6.3f} ".format(ina219_five.current) , end = '') 
+        error = 1    
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '') 
+       
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_six.bus_voltage), "{:6.3f} ".format(ina219_six.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_six = INA219(i2c_two, addresses[1]) 
+        ina219_six.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_six.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_six.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_six.bus_voltage), "{:6.3f} ".format(ina219_six.current) , end = '') 
+        error = 1 
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '') 
+          
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_seven.bus_voltage), "{:6.3f} ".format(ina219_seven.current) , end = '') 
+    except:
+      
+      try:  
+        ina219_seven = INA219(i2c_two, addresses[2]) 
+        ina219_seven.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_seven.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_seven.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_seven.bus_voltage), "{:6.3f} ".format(ina219_seven.current) , end = '') 
+        error = 1
+        
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '') 
+      
+    try:
+      time.sleep(0.01)  
+      print("{:6.3f} ".format(ina219_eight.bus_voltage), "{:6.3f} ".format(ina219_eight.current), end = '')  
     except:
-      print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), "{:6.3f} ".format(0),  "{:6.3f} ".format(0), "{:6.3f} ".format(0),  "{:6.3f} ".format(0), "{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '')   
-#        pass
-  print(" ")
+      
+      try:  
+        ina219_eight = INA219(i2c_two, addresses[3]) 
+        ina219_eight.bus_adc_resolution = ADCResolution.ADCRES_12BIT_32S   # 1S
+        time.sleep(0.001)
+        ina219_eight.shunt_adc_resolution = ADCResolution.ADCRES_12BIT_32S     # 1S
+        time.sleep(0.001)
+        ina219_eight.bus_voltage_range = BusVoltageRange.RANGE_16V
+        time.sleep(0.01)
+        print("{:6.3f} ".format(ina219_eight.bus_voltage), "{:6.3f} ".format(ina219_eight.current), end = '')  
+        error = 1
+       
+      except:
+#        print("Python Error 3", file=sys.stderr, flush=True)
+        print("{:6.3f} ".format(0),  "{:6.3f} ".format(0), end = '')  
+      
+    if (error == 0):
+      print(" ")
+    else:
+      print("Python Error Recovered!")
+      
+    inp = input()
+#   print(inp)
diff --git a/rpitx.py b/rpitx.py
index 7bfc90d9..bbb87c06 100644
--- a/rpitx.py
+++ b/rpitx.py
@@ -109,6 +109,7 @@ if __name__ == "__main__":
 		else:
 			print("FSK") 
 			system("sudo nc -l 8080 | csdr convert_i16_f | csdr gain_ff 7000 | csdr convert_f_samplerf 20833 | sudo /home/pi/rpitx/rpitx -i- -m RF -f 434.9e3")
+
 	else:
 		print("No Band Pass Filter so no telemetry transmit.  See http://cubesatsim.org/wiki for instructions on how to build the BPF.")
 		while 1:
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_maxtelemetry.csv
new file mode 100644
index 00000000..c55ada57
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_maxtelemetry.csv
@@ -0,0 +1,61 @@
+60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
+0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale)
+1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
+2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
+4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
+5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
+6,MAX,battCurr,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
+7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature
+8,MAX,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage
+9,MAX,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage
+10,MAX,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage
+11,MAX,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage
+12,MAX,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage
+13,MAX,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage
+14,MAX,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X solar Panel current
+15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y solar Panel current
+16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z solar Panel current
+17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X solar Panel current
+18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y solar Panel current
+19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z solar Panel current
+20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply Voltage
+21,MAX,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,MAX,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
+23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
+24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,MAX,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
+26,MAX,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
+27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
+28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
+29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
+30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,Humidity
+31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
+32,MAX,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
+33,MAX,Sensor2,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
+35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
+36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
+37,MAX,rf6,12,-,0,NONE,0,0,0,None,None
+38,MAX,rf7,12,-,0,NONE,0,0,0,None,None
+39,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
+40,MAX,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
+41,MAX,pad,4,-,34,NONE,0,0,0,None,Unused
+42,MAX,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
+43,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
+44,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+45,MAX,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator
+46,MAX,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator
+47,MAX,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator
+48,MAX,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator
+49,MAX,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator
+50,MAX,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
+51,MAX,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status
+52,MAX,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status
+53,MAX,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator
+54,MAX,pad1,1,-,0,NONE,0,0,0,NONE,Filler
+55,MAX,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping.  In hundreds
+56,MAX,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
+57,MAX,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
+58,MAX,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
+59,MAX,pad2,28,-,0,NONE,0,0,0,NONE,Filler
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_mintelemetry.csv
new file mode 100644
index 00000000..690b9da2
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_mintelemetry.csv
@@ -0,0 +1,61 @@
+60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
+0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale)
+1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
+2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
+4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
+5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
+6,MIN,battCurr,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
+7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature
+8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage
+9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage
+10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage
+11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage
+12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage
+13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage
+14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X solar Panel current
+15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y solar Panel current
+16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z solar Panel current
+17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X solar Panel current
+18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y solar Panel current
+19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z solar Panel current
+20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply Voltage
+21,MIN,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,MIN,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
+23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
+24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,MIN,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
+26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
+27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
+28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
+29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
+30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,Humidity
+31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
+32,MIN,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
+33,MIN,Sensor2,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
+35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
+36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
+37,MIN,rf6,12,-,0,NONE,0,0,0,None,None
+38,MIN,rf7,12,-,0,NONE,0,0,0,None,None
+39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
+40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
+41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused
+42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
+43,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
+44,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator
+46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator
+47,MIN,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator
+48,MIN,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator
+49,MIN,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator
+50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
+51,MIN,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status
+52,MIN,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status
+53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator
+54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler
+55,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping.  In hundreds
+56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
+57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
+58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
+59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_rttelemetry.csv
new file mode 100644
index 00000000..ec06db4f
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_PSK_rttelemetry.csv
@@ -0,0 +1,61 @@
+60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
+0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
+1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
+2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
+4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
+5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
+6,realTime,battCurr,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current
+7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload sensor temperature
+8,realTime,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar panel voltage
+9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar panel voltage
+10,realTime,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar panel voltage
+11,realTime,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar panel voltage
+12,realTime,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar panel voltage
+13,realTime,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar panel voltage
+14,realTime,posXi,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X solar panel current
+15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y solar panel current
+16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z solar panel current
+17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X solar panel current
+18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y solar panel current
+19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z solar panel current
+20,realTime,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply voltage
+21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,realTime,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload sensor pressure
+23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload sensor altitude
+24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,realTime,rssi,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication
+26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal temperature of IHU from Pi
+27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular veolcity around X Axis
+28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular veolcity around Y Axis
+29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular veolcity around Z Axis
+30,realTime,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
+31,realTime,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
+32,realTime,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload extra Sensor 1
+33,realTime,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload extra Sensor 2
+34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload, STEM Payload STEM Payload board failure indicator
+35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+36,realTime,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
+37,realTime,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
+38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
+39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
+40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
+41,realTime,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
+42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
+43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
+44,realTime,TxAntenna,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
+45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
+46,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
+47,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
+48,realTime,rf6,12,-,0,NONE,0,0,0,None,None
+49,realTime,rf7,12,-,0,NONE,0,0,0,None,None
+50,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
+51,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
+52,realTime,pad,4,-,34,NONE,0,0,0,None,Unused
+53,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
+54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler
+55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping.  In hundreds
+56,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
+57,realTime,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
+58,realTime,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
+59,realTime,pad2,28,-,0,NONE,0,0,0,NONE,Filler
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_conversion_curves.csv b/spacecraft/FoxTelem_11a/CubeSatSim_conversion_curves.csv
new file mode 100644
index 00000000..30f05985
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_conversion_curves.csv
@@ -0,0 +1,13 @@
+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
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_maxtelemetry.csv
new file mode 100644
index 00000000..57fe1706
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_maxtelemetry.csv
@@ -0,0 +1,47 @@
+46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMAX_NAME,DESCRIPTION
+0,MAX,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
+1,MAX,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
+2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
+4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
+5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
+6,MAX,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
+7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
+8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
+9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
+10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel
+11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel
+12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel
+13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel
+14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel
+15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel
+16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel
+17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
+18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
+19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
+20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage
+21,MAX,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,MAX,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
+23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
+24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,MAX,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
+26,MAX,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
+27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
+28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
+29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
+30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Sensor 1,STEM Payload Sensor Humidity 
+31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
+32,MAX,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
+33,MAX,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
+35,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+36,MAX,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
+37,MAX,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
+38,MAX,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
+39,MAX,I2CBus1Failure,1,-,17,NONE,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
+40,MAX,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
+41,MAX,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator
+42,MAX,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
+43,MAX,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
+44,MAX,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
+45,MAX,Pad,58,-,0,NONE,0,0,0,NONE,NONE
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv
new file mode 100644
index 00000000..006ab3ef
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv
@@ -0,0 +1,47 @@
+46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION
+0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
+1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
+2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
+4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
+5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
+6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
+7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
+8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
+9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
+10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel
+11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel
+12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel
+13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel
+14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel
+15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel
+16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel
+17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
+18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
+19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
+20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage
+21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
+23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
+24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,MIN,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication
+26,MIN,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU
+27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
+28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
+29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
+30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,STEM Payload Sensor Humidity
+31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
+32,MIN,Sensor1,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
+33,MIN,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
+35,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
+37,MIN,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
+38,MIN,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
+39,MIN,I2CBus1Failure,1,-,17,NONE,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
+40,MIN,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
+41,MIN,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator
+42,MIN,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received
+43,MIN,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status
+44,MIN,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status
+45,MIN,Pad,58,-,0,NONE,0,0,0,NONE,NONE
diff --git a/spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
new file mode 100644
index 00000000..4d466a3a
--- /dev/null
+++ b/spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
@@ -0,0 +1,47 @@
+46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
+0,RT,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
+1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
+2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
+4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
+5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
+6,RT,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current
+7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
+8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel
+9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel
+10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel
+11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel
+12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel
+13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel
+14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel
+15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel
+16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel
+17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel
+18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel
+19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel
+20,RT,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage
+21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
+22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
+23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude
+24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
+25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication
+26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU
+27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
+28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
+29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
+30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,STEM Payload Sensor Humidity
+31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
+32,RT,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
+33,RT,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload,STEM Payload Board Status
+35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
+36,RT,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
+37,RT,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
+38,RT,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
+39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
+40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
+41,RT,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
+42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
+43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
+44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
+45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE
diff --git a/systemd/cubesatsim.service b/systemd/cubesatsim.service
index 633f689d..e704d5b8 100644
--- a/systemd/cubesatsim.service
+++ b/systemd/cubesatsim.service
@@ -10,6 +10,8 @@ StandardOutput=inherit
 StandardError=inherit
 Restart=always
 User=root
+CPUAccounting=true
+CPUQuota=5%
 
 [Install]
 WantedBy=default.target