case AO_TELEMETRY_SENSOR_TELEMETRUM:
case AO_TELEMETRY_SENSOR_TELEMINI:
case AO_TELEMETRY_SENSOR_TELENANO:
- case AO_TELEMETRY_SENSOR_MEGAMETRUM:
printf ("state %1d accel %5d pres %5d ",
telem.sensor.state, telem.sensor.accel, telem.sensor.pres);
printf ("accel %6.2f speed %6.2f height %5d ",
telem.satellite.sats[c].c_n_1);
}
printf ("\n");
+ break;
+ case AO_TELEMETRY_MEGA_SENSOR:
+ printf ("accel %5d pres %9d temp %5d accel_x %5d accel_y %5d accel_z %5d gyro_x %5d gyro_y %5d gyro_z %5d mag_x %5d mag_y %5d mag_z %5d\n",
+ telem.mega_sensor.accel,
+ telem.mega_sensor.pres,
+ telem.mega_sensor.temp,
+ telem.mega_sensor.accel_x,
+ telem.mega_sensor.accel_y,
+ telem.mega_sensor.accel_z,
+ telem.mega_sensor.gyro_x,
+ telem.mega_sensor.gyro_y,
+ telem.mega_sensor.gyro_z,
+ telem.mega_sensor.mag_x,
+ telem.mega_sensor.mag_y,
+ telem.mega_sensor.mag_z);
+ break;
+ case AO_TELEMETRY_MEGA_DATA:
+ printf ("state %1d v_batt %5d v_pyro %5d ",
+ telem.mega_data.state,
+ telem.mega_data.v_batt,
+ telem.mega_data.v_pyro);
+ for (c = 0; c < 6; c++)
+ printf ("s%1d %5d ", c,
+ telem.mega_data.sense[c] |
+ (telem.mega_data.sense[c] << 8));
+
+ printf ("ground_pres %5d ground_accel %5d accel_plus %5d accel_minus %5d ",
+ telem.mega_data.ground_pres,
+ telem.mega_data.ground_accel,
+ telem.mega_data.accel_plus_g,
+ telem.mega_data.accel_minus_g);
+
+ printf ("accel %6.2f speed %6.2f height %5d\n",
+ telem.mega_data.acceleration / 16.0,
+ telem.mega_data.speed / 16.0,
+ telem.mega_data.height);
+
break;
default:
printf("\n");
#define AO_TELEMETRY_SENSOR_TELEMETRUM 0x01
#define AO_TELEMETRY_SENSOR_TELEMINI 0x02
#define AO_TELEMETRY_SENSOR_TELENANO 0x03
-#define AO_TELEMETRY_SENSOR_MEGAMETRUM 0x08
struct ao_telemetry_sensor {
uint16_t serial; /* 0 */
/* 32 */
};
+#define AO_TELEMETRY_MEGA_SENSOR 0x08
+
+struct ao_telemetry_mega_sensor {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+
+ uint8_t pad5; /* 5 */
+ int16_t accel; /* 6 Z axis */
+
+ int32_t pres; /* 8 Pa * 10 */
+ int16_t temp; /* 12 °C * 100 */
+
+ int16_t accel_x; /* 14 */
+ int16_t accel_y; /* 16 */
+ int16_t accel_z; /* 18 */
+
+ int16_t gyro_x; /* 20 */
+ int16_t gyro_y; /* 22 */
+ int16_t gyro_z; /* 24 */
+
+ int16_t mag_x; /* 26 */
+ int16_t mag_y; /* 28 */
+ int16_t mag_z; /* 30 */
+ /* 32 */
+};
+
+#define AO_TELEMETRY_MEGA_DATA 0x09
+
+struct ao_telemetry_mega_data {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+
+ uint8_t state; /* 5 flight state */
+
+ int16_t v_batt; /* 6 battery voltage */
+ int16_t v_pyro; /* 8 pyro battery voltage */
+ int8_t sense[6]; /* 10 continuity sense */
+
+ int32_t ground_pres; /* 16 average pres on pad */
+ int16_t ground_accel; /* 20 average accel on pad */
+ int16_t accel_plus_g; /* 22 accel calibration at +1g */
+ int16_t accel_minus_g; /* 24 accel calibration at -1g */
+
+ int16_t acceleration; /* 26 m/s² * 16 */
+ int16_t speed; /* 28 m/s * 16 */
+ int16_t height; /* 30 m */
+ /* 32 */
+};
+
/* #define AO_SEND_ALL_BARO */
#define AO_TELEMETRY_BARO 0x80
struct ao_telemetry_location location;
struct ao_telemetry_satellite satellite;
struct ao_telemetry_companion companion;
+ struct ao_telemetry_mega_sensor mega_sensor;
+ struct ao_telemetry_mega_data mega_data;
struct ao_telemetry_baro baro;
};