diff options
Diffstat (limited to 'mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h')
| -rw-r--r-- | mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h | 419 |
1 files changed, 419 insertions, 0 deletions
diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h new file mode 100644 index 000000000..d046f2ad0 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h @@ -0,0 +1,419 @@ +// MESSAGE AIRSPEED_AUTOCAL PACKING + +#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL 174 + +typedef struct __mavlink_airspeed_autocal_t +{ + float vx; ///< GPS velocity north m/s + float vy; ///< GPS velocity east m/s + float vz; ///< GPS velocity down m/s + float diff_pressure; ///< Differential pressure pascals + float EAS2TAS; ///< Estimated to true airspeed ratio + float ratio; ///< Airspeed ratio + float state_x; ///< EKF state x + float state_y; ///< EKF state y + float state_z; ///< EKF state z + float Pax; ///< EKF Pax + float Pby; ///< EKF Pby + float Pcz; ///< EKF Pcz +} mavlink_airspeed_autocal_t; + +#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN 48 +#define MAVLINK_MSG_ID_174_LEN 48 + +#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC 167 +#define MAVLINK_MSG_ID_174_CRC 167 + + + +#define MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL { \ + "AIRSPEED_AUTOCAL", \ + 12, \ + { { "vx", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_airspeed_autocal_t, vx) }, \ + { "vy", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_airspeed_autocal_t, vy) }, \ + { "vz", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_airspeed_autocal_t, vz) }, \ + { "diff_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_airspeed_autocal_t, diff_pressure) }, \ + { "EAS2TAS", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_airspeed_autocal_t, EAS2TAS) }, \ + { "ratio", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_airspeed_autocal_t, ratio) }, \ + { "state_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_airspeed_autocal_t, state_x) }, \ + { "state_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_airspeed_autocal_t, state_y) }, \ + { "state_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_airspeed_autocal_t, state_z) }, \ + { "Pax", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_airspeed_autocal_t, Pax) }, \ + { "Pby", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_airspeed_autocal_t, Pby) }, \ + { "Pcz", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_airspeed_autocal_t, Pcz) }, \ + } \ +} + + +/** + * @brief Pack a airspeed_autocal 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 vx GPS velocity north m/s + * @param vy GPS velocity east m/s + * @param vz GPS velocity down m/s + * @param diff_pressure Differential pressure pascals + * @param EAS2TAS Estimated to true airspeed ratio + * @param ratio Airspeed ratio + * @param state_x EKF state x + * @param state_y EKF state y + * @param state_z EKF state z + * @param Pax EKF Pax + * @param Pby EKF Pby + * @param Pcz EKF Pcz + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_airspeed_autocal_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; + _mav_put_float(buf, 0, vx); + _mav_put_float(buf, 4, vy); + _mav_put_float(buf, 8, vz); + _mav_put_float(buf, 12, diff_pressure); + _mav_put_float(buf, 16, EAS2TAS); + _mav_put_float(buf, 20, ratio); + _mav_put_float(buf, 24, state_x); + _mav_put_float(buf, 28, state_y); + _mav_put_float(buf, 32, state_z); + _mav_put_float(buf, 36, Pax); + _mav_put_float(buf, 40, Pby); + _mav_put_float(buf, 44, Pcz); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#else + mavlink_airspeed_autocal_t packet; + packet.vx = vx; + packet.vy = vy; + packet.vz = vz; + packet.diff_pressure = diff_pressure; + packet.EAS2TAS = EAS2TAS; + packet.ratio = ratio; + packet.state_x = state_x; + packet.state_y = state_y; + packet.state_z = state_z; + packet.Pax = Pax; + packet.Pby = Pby; + packet.Pcz = Pcz; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +} + +/** + * @brief Pack a airspeed_autocal 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 will be sent over + * @param msg The MAVLink message to compress the data into + * @param vx GPS velocity north m/s + * @param vy GPS velocity east m/s + * @param vz GPS velocity down m/s + * @param diff_pressure Differential pressure pascals + * @param EAS2TAS Estimated to true airspeed ratio + * @param ratio Airspeed ratio + * @param state_x EKF state x + * @param state_y EKF state y + * @param state_z EKF state z + * @param Pax EKF Pax + * @param Pby EKF Pby + * @param Pcz EKF Pcz + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_airspeed_autocal_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + float vx,float vy,float vz,float diff_pressure,float EAS2TAS,float ratio,float state_x,float state_y,float state_z,float Pax,float Pby,float Pcz) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; + _mav_put_float(buf, 0, vx); + _mav_put_float(buf, 4, vy); + _mav_put_float(buf, 8, vz); + _mav_put_float(buf, 12, diff_pressure); + _mav_put_float(buf, 16, EAS2TAS); + _mav_put_float(buf, 20, ratio); + _mav_put_float(buf, 24, state_x); + _mav_put_float(buf, 28, state_y); + _mav_put_float(buf, 32, state_z); + _mav_put_float(buf, 36, Pax); + _mav_put_float(buf, 40, Pby); + _mav_put_float(buf, 44, Pcz); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#else + mavlink_airspeed_autocal_t packet; + packet.vx = vx; + packet.vy = vy; + packet.vz = vz; + packet.diff_pressure = diff_pressure; + packet.EAS2TAS = EAS2TAS; + packet.ratio = ratio; + packet.state_x = state_x; + packet.state_y = state_y; + packet.state_z = state_z; + packet.Pax = Pax; + packet.Pby = Pby; + packet.Pcz = Pcz; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_AIRSPEED_AUTOCAL; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +} + +/** + * @brief Encode a airspeed_autocal struct + * + * @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 airspeed_autocal C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_airspeed_autocal_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal) +{ + return mavlink_msg_airspeed_autocal_pack(system_id, component_id, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz); +} + +/** + * @brief Encode a airspeed_autocal struct 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 will be sent over + * @param msg The MAVLink message to compress the data into + * @param airspeed_autocal C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_airspeed_autocal_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_airspeed_autocal_t* airspeed_autocal) +{ + return mavlink_msg_airspeed_autocal_pack_chan(system_id, component_id, chan, msg, airspeed_autocal->vx, airspeed_autocal->vy, airspeed_autocal->vz, airspeed_autocal->diff_pressure, airspeed_autocal->EAS2TAS, airspeed_autocal->ratio, airspeed_autocal->state_x, airspeed_autocal->state_y, airspeed_autocal->state_z, airspeed_autocal->Pax, airspeed_autocal->Pby, airspeed_autocal->Pcz); +} + +/** + * @brief Send a airspeed_autocal message + * @param chan MAVLink channel to send the message + * + * @param vx GPS velocity north m/s + * @param vy GPS velocity east m/s + * @param vz GPS velocity down m/s + * @param diff_pressure Differential pressure pascals + * @param EAS2TAS Estimated to true airspeed ratio + * @param ratio Airspeed ratio + * @param state_x EKF state x + * @param state_y EKF state y + * @param state_z EKF state z + * @param Pax EKF Pax + * @param Pby EKF Pby + * @param Pcz EKF Pcz + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_airspeed_autocal_send(mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN]; + _mav_put_float(buf, 0, vx); + _mav_put_float(buf, 4, vy); + _mav_put_float(buf, 8, vz); + _mav_put_float(buf, 12, diff_pressure); + _mav_put_float(buf, 16, EAS2TAS); + _mav_put_float(buf, 20, ratio); + _mav_put_float(buf, 24, state_x); + _mav_put_float(buf, 28, state_y); + _mav_put_float(buf, 32, state_z); + _mav_put_float(buf, 36, Pax); + _mav_put_float(buf, 40, Pby); + _mav_put_float(buf, 44, Pcz); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +#else + mavlink_airspeed_autocal_t packet; + packet.vx = vx; + packet.vy = vy; + packet.vz = vz; + packet.diff_pressure = diff_pressure; + packet.EAS2TAS = EAS2TAS; + packet.ratio = ratio; + packet.state_x = state_x; + packet.state_y = state_y; + packet.state_z = state_z; + packet.Pax = Pax; + packet.Pby = Pby; + packet.Pcz = Pcz; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)&packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +#endif +} + +#endif + +// MESSAGE AIRSPEED_AUTOCAL UNPACKING + + +/** + * @brief Get field vx from airspeed_autocal message + * + * @return GPS velocity north m/s + */ +static inline float mavlink_msg_airspeed_autocal_get_vx(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 0); +} + +/** + * @brief Get field vy from airspeed_autocal message + * + * @return GPS velocity east m/s + */ +static inline float mavlink_msg_airspeed_autocal_get_vy(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 4); +} + +/** + * @brief Get field vz from airspeed_autocal message + * + * @return GPS velocity down m/s + */ +static inline float mavlink_msg_airspeed_autocal_get_vz(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 8); +} + +/** + * @brief Get field diff_pressure from airspeed_autocal message + * + * @return Differential pressure pascals + */ +static inline float mavlink_msg_airspeed_autocal_get_diff_pressure(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 12); +} + +/** + * @brief Get field EAS2TAS from airspeed_autocal message + * + * @return Estimated to true airspeed ratio + */ +static inline float mavlink_msg_airspeed_autocal_get_EAS2TAS(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 16); +} + +/** + * @brief Get field ratio from airspeed_autocal message + * + * @return Airspeed ratio + */ +static inline float mavlink_msg_airspeed_autocal_get_ratio(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 20); +} + +/** + * @brief Get field state_x from airspeed_autocal message + * + * @return EKF state x + */ +static inline float mavlink_msg_airspeed_autocal_get_state_x(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 24); +} + +/** + * @brief Get field state_y from airspeed_autocal message + * + * @return EKF state y + */ +static inline float mavlink_msg_airspeed_autocal_get_state_y(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 28); +} + +/** + * @brief Get field state_z from airspeed_autocal message + * + * @return EKF state z + */ +static inline float mavlink_msg_airspeed_autocal_get_state_z(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 32); +} + +/** + * @brief Get field Pax from airspeed_autocal message + * + * @return EKF Pax + */ +static inline float mavlink_msg_airspeed_autocal_get_Pax(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 36); +} + +/** + * @brief Get field Pby from airspeed_autocal message + * + * @return EKF Pby + */ +static inline float mavlink_msg_airspeed_autocal_get_Pby(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 40); +} + +/** + * @brief Get field Pcz from airspeed_autocal message + * + * @return EKF Pcz + */ +static inline float mavlink_msg_airspeed_autocal_get_Pcz(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 44); +} + +/** + * @brief Decode a airspeed_autocal message into a struct + * + * @param msg The message to decode + * @param airspeed_autocal C-struct to decode the message contents into + */ +static inline void mavlink_msg_airspeed_autocal_decode(const mavlink_message_t* msg, mavlink_airspeed_autocal_t* airspeed_autocal) +{ +#if MAVLINK_NEED_BYTE_SWAP + airspeed_autocal->vx = mavlink_msg_airspeed_autocal_get_vx(msg); + airspeed_autocal->vy = mavlink_msg_airspeed_autocal_get_vy(msg); + airspeed_autocal->vz = mavlink_msg_airspeed_autocal_get_vz(msg); + airspeed_autocal->diff_pressure = mavlink_msg_airspeed_autocal_get_diff_pressure(msg); + airspeed_autocal->EAS2TAS = mavlink_msg_airspeed_autocal_get_EAS2TAS(msg); + airspeed_autocal->ratio = mavlink_msg_airspeed_autocal_get_ratio(msg); + airspeed_autocal->state_x = mavlink_msg_airspeed_autocal_get_state_x(msg); + airspeed_autocal->state_y = mavlink_msg_airspeed_autocal_get_state_y(msg); + airspeed_autocal->state_z = mavlink_msg_airspeed_autocal_get_state_z(msg); + airspeed_autocal->Pax = mavlink_msg_airspeed_autocal_get_Pax(msg); + airspeed_autocal->Pby = mavlink_msg_airspeed_autocal_get_Pby(msg); + airspeed_autocal->Pcz = mavlink_msg_airspeed_autocal_get_Pcz(msg); +#else + memcpy(airspeed_autocal, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +} |