/* 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;
};