Update main.c fix payload failure

master-latency
Alan Johnston 4 months ago committed by GitHub
parent c16a1191ba
commit 0880257c30
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GPG Key ID: B5690EEEBB952194

@ -1468,16 +1468,17 @@ void get_tlm_fox() {
encodeA(b, 3 + head_offset, batt_c_v);
if ((failureMode != FAIL_MPU) && (failureMode != FAIL_PAYLOAD)) {
encodeB(b, 4 + head_offset, (int)(sensor[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b, 6 + head_offset, (int)(sensor[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b, 7 + head_offset, (int)(sensor[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
}
else
if ((failureMode == FAIL_MPU) || (failureMode == FAIL_PAYLOAD))
{
encodeB(b, 4 + head_offset, 2048); // 0
encodeA(b, 6 + head_offset, 2048); // 0
encodeB(b, 7 + head_offset, 2048); // 0
encodeB(b, 7 + head_offset, 2048); // 0
}
else
{
encodeB(b, 4 + head_offset, (int)(sensor[ACCEL_X] * 100 + 0.5) + 2048); // Xaccel
encodeA(b, 6 + head_offset, (int)(sensor[ACCEL_Y] * 100 + 0.5) + 2048); // Yaccel
encodeB(b, 7 + head_offset, (int)(sensor[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel
}
encodeA(b, 9 + head_offset, battCurr);
@ -1669,36 +1670,51 @@ void get_tlm_fox() {
encodeA(b, 30 + head_offset, BAT2Voltage);
encodeB(b, 31 + head_offset, ((int)(other[SPIN] * 10)) + 2048);
if (failureMode != FAIL_BME) {
encodeA(b, 33 + head_offset, (int)(sensor[PRES] + 0.5)); // Pressure
encodeB(b, 34 + head_offset, (int)(sensor[ALT] * 10.0 + 0.5)); // Altitude
encodeA(b, 45 + head_offset, (int)(sensor[HUMI] * 10 + 0.5)); // in place of sensor1
encodeA(b, 39 + head_offset, (int)(other[IHU_TEMP] * 10 + 0.5));
}
encodeA(b, 36 + head_offset, Resets);
encodeB(b, 37 + head_offset, (int)(other[RSSI] + 0.5) + 2048);
if (failureMode != FAIL_MPU) {
encodeB(b, 40 + head_offset, (int)(sensor[GYRO_X] + 0.5) + 2048);
encodeA(b, 42 + head_offset, (int)(sensor[GYRO_Y] + 0.5) + 2048);
encodeB(b, 43 + head_offset, (int)(sensor[GYRO_Z] + 0.5) + 2048);
}
if (failureMode != FAIL_PAYLOAD) {
if (failureMode != FAIL_BME) {
encodeA(b, 33 + head_offset, (int)(sensor[PRES] + 0.5)); // Pressure
encodeB(b, 34 + head_offset, (int)(sensor[ALT] * 10.0 + 0.5)); // Altitude
encodeA(b, 45 + head_offset, (int)(sensor[HUMI] * 10 + 0.5)); // in place of sensor1
encodeA(b, 39 + head_offset, (int)(other[IHU_TEMP] * 10 + 0.5));
}
encodeA(b, 36 + head_offset, Resets);
encodeB(b, 37 + head_offset, (int)(other[RSSI] + 0.5) + 2048);
if (failureMode != FAIL_MPU) {
encodeB(b, 40 + head_offset, (int)(sensor[GYRO_X] + 0.5) + 2048);
encodeA(b, 42 + head_offset, (int)(sensor[GYRO_Y] + 0.5) + 2048);
encodeB(b, 43 + head_offset, (int)(sensor[GYRO_Z] + 0.5) + 2048);
}
else
{
encodeB(b, 40 + head_offset, 2048);
encodeA(b, 42 + head_offset, 2048);
encodeB(b, 43 + head_offset, 2048);
}
encodeA(b, 48 + head_offset, (int)(sensor[DTEMP] * 10 + 0.5) + 2048);
encodeB(b, 49 + head_offset, (int)(sensor[XS1]));
encodeA(b, 0 + head_offset, (int)(sensor[XS2]));
encodeB(b, 1 + head_offset, (int)(sensor[XS3]));
}
else
{
encodeB(b, 40 + head_offset, 2048);
encodeA(b, 42 + head_offset, 2048);
encodeB(b, 43 + head_offset, 2048);
}
{
encodeB(b_min, 4 + head_offset, 2048); // 0
encodeA(b_min, 6 + head_offset, 2048); // 0
encodeB(b_min, 7 + head_offset, 2048); // 0
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, 46 + head_offset, BAT2Current);
encodeA(b, 48 + head_offset, (int)(sensor[DTEMP] * 10 + 0.5) + 2048);
// encodeB(b, 49 + head_offset, (int)(sensor[XS1] * 10 + 0.5) + 2048);
encodeB(b, 49 + head_offset, (int)(sensor[XS1]));
encodeA(b, 0 + head_offset, (int)(sensor[XS2]));
encodeB(b, 1 + head_offset, (int)(sensor[XS3]));
FILE * command_count_file = fopen("/home/pi/CubeSatSim/command_count.txt", "r");
if (command_count_file != NULL) {
char count_string[10];

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