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-rw-r--r--mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h276
1 files changed, 276 insertions, 0 deletions
diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h
new file mode 100644
index 000000000..eceb61d51
--- /dev/null
+++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h
@@ -0,0 +1,276 @@
+// MESSAGE AIRSPEEDS PACKING
+
+#define MAVLINK_MSG_ID_AIRSPEEDS 182
+
+typedef struct __mavlink_airspeeds_t
+{
+ uint32_t time_boot_ms; ///< Timestamp (milliseconds since system boot)
+ int16_t airspeed_imu; ///< Airspeed estimate from IMU, cm/s
+ int16_t airspeed_pitot; ///< Pitot measured forward airpseed, cm/s
+ int16_t airspeed_hot_wire; ///< Hot wire anenometer measured airspeed, cm/s
+ int16_t airspeed_ultrasonic; ///< Ultrasonic measured airspeed, cm/s
+ int16_t aoa; ///< Angle of attack sensor, degrees * 10
+ int16_t aoy; ///< Yaw angle sensor, degrees * 10
+} mavlink_airspeeds_t;
+
+#define MAVLINK_MSG_ID_AIRSPEEDS_LEN 16
+#define MAVLINK_MSG_ID_182_LEN 16
+
+
+
+#define MAVLINK_MESSAGE_INFO_AIRSPEEDS { \
+ "AIRSPEEDS", \
+ 7, \
+ { { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_airspeeds_t, time_boot_ms) }, \
+ { "airspeed_imu", NULL, MAVLINK_TYPE_INT16_T, 0, 4, offsetof(mavlink_airspeeds_t, airspeed_imu) }, \
+ { "airspeed_pitot", NULL, MAVLINK_TYPE_INT16_T, 0, 6, offsetof(mavlink_airspeeds_t, airspeed_pitot) }, \
+ { "airspeed_hot_wire", NULL, MAVLINK_TYPE_INT16_T, 0, 8, offsetof(mavlink_airspeeds_t, airspeed_hot_wire) }, \
+ { "airspeed_ultrasonic", NULL, MAVLINK_TYPE_INT16_T, 0, 10, offsetof(mavlink_airspeeds_t, airspeed_ultrasonic) }, \
+ { "aoa", NULL, MAVLINK_TYPE_INT16_T, 0, 12, offsetof(mavlink_airspeeds_t, aoa) }, \
+ { "aoy", NULL, MAVLINK_TYPE_INT16_T, 0, 14, offsetof(mavlink_airspeeds_t, aoy) }, \
+ } \
+}
+
+
+/**
+ * @brief Pack a airspeeds message
+ * @param system_id ID of this system
+ * @param component_id ID of this component (e.g. 200 for IMU)
+ * @param msg The MAVLink message to compress the data into
+ *
+ * @param time_boot_ms Timestamp (milliseconds since system boot)
+ * @param airspeed_imu Airspeed estimate from IMU, cm/s
+ * @param airspeed_pitot Pitot measured forward airpseed, cm/s
+ * @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
+ * @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
+ * @param aoa Angle of attack sensor, degrees * 10
+ * @param aoy Yaw angle sensor, degrees * 10
+ * @return length of the message in bytes (excluding serial stream start sign)
+ */
+static inline uint16_t mavlink_msg_airspeeds_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
+ uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
+{
+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
+ char buf[16];
+ _mav_put_uint32_t(buf, 0, time_boot_ms);
+ _mav_put_int16_t(buf, 4, airspeed_imu);
+ _mav_put_int16_t(buf, 6, airspeed_pitot);
+ _mav_put_int16_t(buf, 8, airspeed_hot_wire);
+ _mav_put_int16_t(buf, 10, airspeed_ultrasonic);
+ _mav_put_int16_t(buf, 12, aoa);
+ _mav_put_int16_t(buf, 14, aoy);
+
+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, 16);
+#else
+ mavlink_airspeeds_t packet;
+ packet.time_boot_ms = time_boot_ms;
+ packet.airspeed_imu = airspeed_imu;
+ packet.airspeed_pitot = airspeed_pitot;
+ packet.airspeed_hot_wire = airspeed_hot_wire;
+ packet.airspeed_ultrasonic = airspeed_ultrasonic;
+ packet.aoa = aoa;
+ packet.aoy = aoy;
+
+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, 16);
+#endif
+
+ msg->msgid = MAVLINK_MSG_ID_AIRSPEEDS;
+ return mavlink_finalize_message(msg, system_id, component_id, 16, 154);
+}
+
+/**
+ * @brief Pack a airspeeds message on a channel
+ * @param system_id ID of this system
+ * @param component_id ID of this component (e.g. 200 for IMU)
+ * @param chan The MAVLink channel this message was sent over
+ * @param msg The MAVLink message to compress the data into
+ * @param time_boot_ms Timestamp (milliseconds since system boot)
+ * @param airspeed_imu Airspeed estimate from IMU, cm/s
+ * @param airspeed_pitot Pitot measured forward airpseed, cm/s
+ * @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
+ * @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
+ * @param aoa Angle of attack sensor, degrees * 10
+ * @param aoy Yaw angle sensor, degrees * 10
+ * @return length of the message in bytes (excluding serial stream start sign)
+ */
+static inline uint16_t mavlink_msg_airspeeds_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
+ mavlink_message_t* msg,
+ uint32_t time_boot_ms,int16_t airspeed_imu,int16_t airspeed_pitot,int16_t airspeed_hot_wire,int16_t airspeed_ultrasonic,int16_t aoa,int16_t aoy)
+{
+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
+ char buf[16];
+ _mav_put_uint32_t(buf, 0, time_boot_ms);
+ _mav_put_int16_t(buf, 4, airspeed_imu);
+ _mav_put_int16_t(buf, 6, airspeed_pitot);
+ _mav_put_int16_t(buf, 8, airspeed_hot_wire);
+ _mav_put_int16_t(buf, 10, airspeed_ultrasonic);
+ _mav_put_int16_t(buf, 12, aoa);
+ _mav_put_int16_t(buf, 14, aoy);
+
+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, 16);
+#else
+ mavlink_airspeeds_t packet;
+ packet.time_boot_ms = time_boot_ms;
+ packet.airspeed_imu = airspeed_imu;
+ packet.airspeed_pitot = airspeed_pitot;
+ packet.airspeed_hot_wire = airspeed_hot_wire;
+ packet.airspeed_ultrasonic = airspeed_ultrasonic;
+ packet.aoa = aoa;
+ packet.aoy = aoy;
+
+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, 16);
+#endif
+
+ msg->msgid = MAVLINK_MSG_ID_AIRSPEEDS;
+ return mavlink_finalize_message_chan(msg, system_id, component_id, chan, 16, 154);
+}
+
+/**
+ * @brief Encode a airspeeds struct into a message
+ *
+ * @param system_id ID of this system
+ * @param component_id ID of this component (e.g. 200 for IMU)
+ * @param msg The MAVLink message to compress the data into
+ * @param airspeeds C-struct to read the message contents from
+ */
+static inline uint16_t mavlink_msg_airspeeds_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeeds_t* airspeeds)
+{
+ return mavlink_msg_airspeeds_pack(system_id, component_id, msg, airspeeds->time_boot_ms, airspeeds->airspeed_imu, airspeeds->airspeed_pitot, airspeeds->airspeed_hot_wire, airspeeds->airspeed_ultrasonic, airspeeds->aoa, airspeeds->aoy);
+}
+
+/**
+ * @brief Send a airspeeds message
+ * @param chan MAVLink channel to send the message
+ *
+ * @param time_boot_ms Timestamp (milliseconds since system boot)
+ * @param airspeed_imu Airspeed estimate from IMU, cm/s
+ * @param airspeed_pitot Pitot measured forward airpseed, cm/s
+ * @param airspeed_hot_wire Hot wire anenometer measured airspeed, cm/s
+ * @param airspeed_ultrasonic Ultrasonic measured airspeed, cm/s
+ * @param aoa Angle of attack sensor, degrees * 10
+ * @param aoy Yaw angle sensor, degrees * 10
+ */
+#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
+
+static inline void mavlink_msg_airspeeds_send(mavlink_channel_t chan, uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy)
+{
+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
+ char buf[16];
+ _mav_put_uint32_t(buf, 0, time_boot_ms);
+ _mav_put_int16_t(buf, 4, airspeed_imu);
+ _mav_put_int16_t(buf, 6, airspeed_pitot);
+ _mav_put_int16_t(buf, 8, airspeed_hot_wire);
+ _mav_put_int16_t(buf, 10, airspeed_ultrasonic);
+ _mav_put_int16_t(buf, 12, aoa);
+ _mav_put_int16_t(buf, 14, aoy);
+
+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, buf, 16, 154);
+#else
+ mavlink_airspeeds_t packet;
+ packet.time_boot_ms = time_boot_ms;
+ packet.airspeed_imu = airspeed_imu;
+ packet.airspeed_pitot = airspeed_pitot;
+ packet.airspeed_hot_wire = airspeed_hot_wire;
+ packet.airspeed_ultrasonic = airspeed_ultrasonic;
+ packet.aoa = aoa;
+ packet.aoy = aoy;
+
+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)&packet, 16, 154);
+#endif
+}
+
+#endif
+
+// MESSAGE AIRSPEEDS UNPACKING
+
+
+/**
+ * @brief Get field time_boot_ms from airspeeds message
+ *
+ * @return Timestamp (milliseconds since system boot)
+ */
+static inline uint32_t mavlink_msg_airspeeds_get_time_boot_ms(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_uint32_t(msg, 0);
+}
+
+/**
+ * @brief Get field airspeed_imu from airspeeds message
+ *
+ * @return Airspeed estimate from IMU, cm/s
+ */
+static inline int16_t mavlink_msg_airspeeds_get_airspeed_imu(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 4);
+}
+
+/**
+ * @brief Get field airspeed_pitot from airspeeds message
+ *
+ * @return Pitot measured forward airpseed, cm/s
+ */
+static inline int16_t mavlink_msg_airspeeds_get_airspeed_pitot(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 6);
+}
+
+/**
+ * @brief Get field airspeed_hot_wire from airspeeds message
+ *
+ * @return Hot wire anenometer measured airspeed, cm/s
+ */
+static inline int16_t mavlink_msg_airspeeds_get_airspeed_hot_wire(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 8);
+}
+
+/**
+ * @brief Get field airspeed_ultrasonic from airspeeds message
+ *
+ * @return Ultrasonic measured airspeed, cm/s
+ */
+static inline int16_t mavlink_msg_airspeeds_get_airspeed_ultrasonic(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 10);
+}
+
+/**
+ * @brief Get field aoa from airspeeds message
+ *
+ * @return Angle of attack sensor, degrees * 10
+ */
+static inline int16_t mavlink_msg_airspeeds_get_aoa(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 12);
+}
+
+/**
+ * @brief Get field aoy from airspeeds message
+ *
+ * @return Yaw angle sensor, degrees * 10
+ */
+static inline int16_t mavlink_msg_airspeeds_get_aoy(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_int16_t(msg, 14);
+}
+
+/**
+ * @brief Decode a airspeeds message into a struct
+ *
+ * @param msg The message to decode
+ * @param airspeeds C-struct to decode the message contents into
+ */
+static inline void mavlink_msg_airspeeds_decode(const mavlink_message_t* msg, mavlink_airspeeds_t* airspeeds)
+{
+#if MAVLINK_NEED_BYTE_SWAP
+ airspeeds->time_boot_ms = mavlink_msg_airspeeds_get_time_boot_ms(msg);
+ airspeeds->airspeed_imu = mavlink_msg_airspeeds_get_airspeed_imu(msg);
+ airspeeds->airspeed_pitot = mavlink_msg_airspeeds_get_airspeed_pitot(msg);
+ airspeeds->airspeed_hot_wire = mavlink_msg_airspeeds_get_airspeed_hot_wire(msg);
+ airspeeds->airspeed_ultrasonic = mavlink_msg_airspeeds_get_airspeed_ultrasonic(msg);
+ airspeeds->aoa = mavlink_msg_airspeeds_get_aoa(msg);
+ airspeeds->aoy = mavlink_msg_airspeeds_get_aoy(msg);
+#else
+ memcpy(airspeeds, _MAV_PAYLOAD(msg), 16);
+#endif
+}