zrzk
/
zr-v4
1
0
Fork 0
Code Issues Pull Requests Projects Releases Wiki Activity
Browse Source

GCS_MAVLink: added missing header

master
Andrew Tridgell 12 years ago
parent
d08d7f4929
commit
67401294f4
1 changed files with 419 additions and 0 deletions
Whitespace
Show all changes Ignore whitespace when comparing lines Ignore changes in amount of whitespace Ignore changes in whitespace at EOL
Split View
Diff Options
Show Stats Download Patch File Download Diff File
  1. 419
      libraries/GCS_MAVLink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h

419
libraries/GCS_MAVLink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h
Unescape View File

@ -0,0 +1,419 @@ @@ -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
}
Write Preview
Loading…
Cancel
Save