update protocol
This commit is contained in:
Matt
@@ -5,18 +5,18 @@
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MAVPACKED(
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typedef struct __mavlink_airspeed_autocal_t {
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float vx; /*< [m/s] GPS velocity north m/s*/
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float vy; /*< [m/s] GPS velocity east m/s*/
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float vz; /*< [m/s] GPS velocity down m/s*/
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float diff_pressure; /*< [Pa] Differential pressure pascals*/
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float EAS2TAS; /*< Estimated to true airspeed ratio*/
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float ratio; /*< Airspeed ratio*/
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float state_x; /*< EKF state x*/
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float state_y; /*< EKF state y*/
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float state_z; /*< EKF state z*/
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float Pax; /*< EKF Pax*/
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float Pby; /*< EKF Pby*/
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float Pcz; /*< EKF Pcz*/
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float vx; /*< [m/s] GPS velocity north.*/
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float vy; /*< [m/s] GPS velocity east.*/
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float vz; /*< [m/s] GPS velocity down.*/
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float diff_pressure; /*< [Pa] Differential pressure.*/
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float EAS2TAS; /*< Estimated to true airspeed ratio.*/
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float ratio; /*< Airspeed ratio.*/
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float state_x; /*< EKF state x.*/
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float state_y; /*< EKF state y.*/
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float state_z; /*< EKF state z.*/
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float Pax; /*< EKF Pax.*/
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float Pby; /*< EKF Pby.*/
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float Pcz; /*< EKF Pcz.*/
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}) mavlink_airspeed_autocal_t;
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#define MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN 48
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@@ -74,18 +74,18 @@ typedef struct __mavlink_airspeed_autocal_t {
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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*
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* @param vx [m/s] GPS velocity north m/s
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* @param vy [m/s] GPS velocity east m/s
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* @param vz [m/s] GPS velocity down m/s
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* @param diff_pressure [Pa] Differential pressure pascals
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* @param EAS2TAS Estimated to true airspeed ratio
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* @param ratio Airspeed ratio
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* @param state_x EKF state x
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* @param state_y EKF state y
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* @param state_z EKF state z
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* @param Pax EKF Pax
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* @param Pby EKF Pby
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* @param Pcz EKF Pcz
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* @param vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_airspeed_autocal_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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@@ -135,18 +135,18 @@ static inline uint16_t mavlink_msg_airspeed_autocal_pack(uint8_t system_id, uint
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @param vx [m/s] GPS velocity north m/s
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* @param vy [m/s] GPS velocity east m/s
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* @param vz [m/s] GPS velocity down m/s
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* @param diff_pressure [Pa] Differential pressure pascals
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* @param EAS2TAS Estimated to true airspeed ratio
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* @param ratio Airspeed ratio
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* @param state_x EKF state x
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* @param state_y EKF state y
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* @param state_z EKF state z
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* @param Pax EKF Pax
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* @param Pby EKF Pby
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* @param Pcz EKF Pcz
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* @param vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_airspeed_autocal_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
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@@ -222,18 +222,18 @@ static inline uint16_t mavlink_msg_airspeed_autocal_encode_chan(uint8_t system_i
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* @brief Send a airspeed_autocal message
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* @param chan MAVLink channel to send the message
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*
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* @param vx [m/s] GPS velocity north m/s
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* @param vy [m/s] GPS velocity east m/s
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* @param vz [m/s] GPS velocity down m/s
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* @param diff_pressure [Pa] Differential pressure pascals
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* @param EAS2TAS Estimated to true airspeed ratio
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* @param ratio Airspeed ratio
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* @param state_x EKF state x
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* @param state_y EKF state y
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* @param state_z EKF state z
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* @param Pax EKF Pax
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* @param Pby EKF Pby
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* @param Pcz EKF Pcz
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* @param vx [m/s] GPS velocity north.
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* @param vy [m/s] GPS velocity east.
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* @param vz [m/s] GPS velocity down.
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* @param diff_pressure [Pa] Differential pressure.
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* @param EAS2TAS Estimated to true airspeed ratio.
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* @param ratio Airspeed ratio.
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* @param state_x EKF state x.
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* @param state_y EKF state y.
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* @param state_z EKF state z.
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* @param Pax EKF Pax.
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* @param Pby EKF Pby.
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* @param Pcz EKF Pcz.
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*/
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#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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@@ -342,7 +342,7 @@ static inline void mavlink_msg_airspeed_autocal_send_buf(mavlink_message_t *msgb
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/**
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* @brief Get field vx from airspeed_autocal message
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*
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* @return [m/s] GPS velocity north m/s
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* @return [m/s] GPS velocity north.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_vx(const mavlink_message_t* msg)
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{
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@@ -352,7 +352,7 @@ static inline float mavlink_msg_airspeed_autocal_get_vx(const mavlink_message_t*
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/**
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* @brief Get field vy from airspeed_autocal message
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*
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* @return [m/s] GPS velocity east m/s
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* @return [m/s] GPS velocity east.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_vy(const mavlink_message_t* msg)
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{
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@@ -362,7 +362,7 @@ static inline float mavlink_msg_airspeed_autocal_get_vy(const mavlink_message_t*
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/**
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* @brief Get field vz from airspeed_autocal message
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*
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* @return [m/s] GPS velocity down m/s
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* @return [m/s] GPS velocity down.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_vz(const mavlink_message_t* msg)
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{
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@@ -372,7 +372,7 @@ static inline float mavlink_msg_airspeed_autocal_get_vz(const mavlink_message_t*
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/**
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* @brief Get field diff_pressure from airspeed_autocal message
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*
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* @return [Pa] Differential pressure pascals
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* @return [Pa] Differential pressure.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_diff_pressure(const mavlink_message_t* msg)
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{
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@@ -382,7 +382,7 @@ static inline float mavlink_msg_airspeed_autocal_get_diff_pressure(const mavlink
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/**
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* @brief Get field EAS2TAS from airspeed_autocal message
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*
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* @return Estimated to true airspeed ratio
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* @return Estimated to true airspeed ratio.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_EAS2TAS(const mavlink_message_t* msg)
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{
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@@ -392,7 +392,7 @@ static inline float mavlink_msg_airspeed_autocal_get_EAS2TAS(const mavlink_messa
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/**
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* @brief Get field ratio from airspeed_autocal message
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*
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* @return Airspeed ratio
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* @return Airspeed ratio.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_ratio(const mavlink_message_t* msg)
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{
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@@ -402,7 +402,7 @@ static inline float mavlink_msg_airspeed_autocal_get_ratio(const mavlink_message
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/**
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* @brief Get field state_x from airspeed_autocal message
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*
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* @return EKF state x
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* @return EKF state x.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_state_x(const mavlink_message_t* msg)
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{
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@@ -412,7 +412,7 @@ static inline float mavlink_msg_airspeed_autocal_get_state_x(const mavlink_messa
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/**
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* @brief Get field state_y from airspeed_autocal message
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*
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* @return EKF state y
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* @return EKF state y.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_state_y(const mavlink_message_t* msg)
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{
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@@ -422,7 +422,7 @@ static inline float mavlink_msg_airspeed_autocal_get_state_y(const mavlink_messa
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/**
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* @brief Get field state_z from airspeed_autocal message
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*
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* @return EKF state z
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* @return EKF state z.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_state_z(const mavlink_message_t* msg)
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{
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@@ -432,7 +432,7 @@ static inline float mavlink_msg_airspeed_autocal_get_state_z(const mavlink_messa
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/**
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* @brief Get field Pax from airspeed_autocal message
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*
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* @return EKF Pax
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* @return EKF Pax.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_Pax(const mavlink_message_t* msg)
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{
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@@ -442,7 +442,7 @@ static inline float mavlink_msg_airspeed_autocal_get_Pax(const mavlink_message_t
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/**
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* @brief Get field Pby from airspeed_autocal message
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*
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* @return EKF Pby
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* @return EKF Pby.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_Pby(const mavlink_message_t* msg)
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{
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@@ -452,7 +452,7 @@ static inline float mavlink_msg_airspeed_autocal_get_Pby(const mavlink_message_t
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/**
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* @brief Get field Pcz from airspeed_autocal message
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*
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* @return EKF Pcz
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* @return EKF Pcz.
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*/
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static inline float mavlink_msg_airspeed_autocal_get_Pcz(const mavlink_message_t* msg)
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{
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