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sil/SIL/otherFiles/mavlink_msg_enginestate.h
T
Matthew 282e5684b1 init
2020-09-30 11:44:05 +08:00

464 lines
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#pragma once
// MESSAGE EngineState PACKING
#define MAVLINK_MSG_ID_EngineState 20201
typedef struct __mavlink_enginestate_t {
uint32_t time_boot_ms; /*< [ms] Timestamp (milliseconds since system boot)*/
uint16_t ChokeFlag; /*< ChokeFlag*/
uint16_t Ignition2Flag; /*< Ignition2Flag*/
uint16_t AmbientTemperatur; /*< AmbientTemperatur*/
uint16_t AirPressure; /*< AirPressure*/
uint16_t ActualFuelPressure; /*< ActualFuelPressure*/
uint16_t FuelPumpDutyCycle; /*< FuelPumpDutyCycle*/
uint16_t ActualJet1DutyCycle; /*< ActualJet1DutyCycle*/
uint16_t ActualRPM; /*< ActualRPM*/
uint16_t CHTemperature1; /*< CHTemperature1*/
uint16_t counts; /*< received number*/
} mavlink_enginestate_t;
#define MAVLINK_MSG_ID_EngineState_LEN 24
#define MAVLINK_MSG_ID_EngineState_MIN_LEN 24
#define MAVLINK_MSG_ID_20201_LEN 24
#define MAVLINK_MSG_ID_20201_MIN_LEN 24
#define MAVLINK_MSG_ID_EngineState_CRC 234
#define MAVLINK_MSG_ID_20201_CRC 234
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_EngineState { \
20201, \
"EngineState", \
11, \
{ { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_enginestate_t, time_boot_ms) }, \
{ "ChokeFlag", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_enginestate_t, ChokeFlag) }, \
{ "Ignition2Flag", NULL, MAVLINK_TYPE_UINT16_T, 0, 6, offsetof(mavlink_enginestate_t, Ignition2Flag) }, \
{ "AmbientTemperatur", NULL, MAVLINK_TYPE_UINT16_T, 0, 8, offsetof(mavlink_enginestate_t, AmbientTemperatur) }, \
{ "AirPressure", NULL, MAVLINK_TYPE_UINT16_T, 0, 10, offsetof(mavlink_enginestate_t, AirPressure) }, \
{ "ActualFuelPressure", NULL, MAVLINK_TYPE_UINT16_T, 0, 12, offsetof(mavlink_enginestate_t, ActualFuelPressure) }, \
{ "FuelPumpDutyCycle", NULL, MAVLINK_TYPE_UINT16_T, 0, 14, offsetof(mavlink_enginestate_t, FuelPumpDutyCycle) }, \
{ "ActualJet1DutyCycle", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_enginestate_t, ActualJet1DutyCycle) }, \
{ "ActualRPM", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_enginestate_t, ActualRPM) }, \
{ "CHTemperature1", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_enginestate_t, CHTemperature1) }, \
{ "counts", NULL, MAVLINK_TYPE_UINT16_T, 0, 22, offsetof(mavlink_enginestate_t, counts) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_EngineState { \
"EngineState", \
11, \
{ { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_enginestate_t, time_boot_ms) }, \
{ "ChokeFlag", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_enginestate_t, ChokeFlag) }, \
{ "Ignition2Flag", NULL, MAVLINK_TYPE_UINT16_T, 0, 6, offsetof(mavlink_enginestate_t, Ignition2Flag) }, \
{ "AmbientTemperatur", NULL, MAVLINK_TYPE_UINT16_T, 0, 8, offsetof(mavlink_enginestate_t, AmbientTemperatur) }, \
{ "AirPressure", NULL, MAVLINK_TYPE_UINT16_T, 0, 10, offsetof(mavlink_enginestate_t, AirPressure) }, \
{ "ActualFuelPressure", NULL, MAVLINK_TYPE_UINT16_T, 0, 12, offsetof(mavlink_enginestate_t, ActualFuelPressure) }, \
{ "FuelPumpDutyCycle", NULL, MAVLINK_TYPE_UINT16_T, 0, 14, offsetof(mavlink_enginestate_t, FuelPumpDutyCycle) }, \
{ "ActualJet1DutyCycle", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_enginestate_t, ActualJet1DutyCycle) }, \
{ "ActualRPM", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_enginestate_t, ActualRPM) }, \
{ "CHTemperature1", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_enginestate_t, CHTemperature1) }, \
{ "counts", NULL, MAVLINK_TYPE_UINT16_T, 0, 22, offsetof(mavlink_enginestate_t, counts) }, \
} \
}
#endif
/**
* @brief Pack a enginestate 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 [ms] Timestamp (milliseconds since system boot)
* @param ChokeFlag ChokeFlag
* @param Ignition2Flag Ignition2Flag
* @param AmbientTemperatur AmbientTemperatur
* @param AirPressure AirPressure
* @param ActualFuelPressure ActualFuelPressure
* @param FuelPumpDutyCycle FuelPumpDutyCycle
* @param ActualJet1DutyCycle ActualJet1DutyCycle
* @param ActualRPM ActualRPM
* @param CHTemperature1 CHTemperature1
* @param counts received number
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_enginestate_pack(uint16_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint32_t time_boot_ms, uint16_t ChokeFlag, uint16_t Ignition2Flag, uint16_t AmbientTemperatur, uint16_t AirPressure, uint16_t ActualFuelPressure, uint16_t FuelPumpDutyCycle, uint16_t ActualJet1DutyCycle, uint16_t ActualRPM, uint16_t CHTemperature1, uint16_t counts)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_EngineState_LEN];
_mav_put_uint32_t(buf, 0, time_boot_ms);
_mav_put_uint16_t(buf, 4, ChokeFlag);
_mav_put_uint16_t(buf, 6, Ignition2Flag);
_mav_put_uint16_t(buf, 8, AmbientTemperatur);
_mav_put_uint16_t(buf, 10, AirPressure);
_mav_put_uint16_t(buf, 12, ActualFuelPressure);
_mav_put_uint16_t(buf, 14, FuelPumpDutyCycle);
_mav_put_uint16_t(buf, 16, ActualJet1DutyCycle);
_mav_put_uint16_t(buf, 18, ActualRPM);
_mav_put_uint16_t(buf, 20, CHTemperature1);
_mav_put_uint16_t(buf, 22, counts);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_EngineState_LEN);
#else
mavlink_enginestate_t packet;
packet.time_boot_ms = time_boot_ms;
packet.ChokeFlag = ChokeFlag;
packet.Ignition2Flag = Ignition2Flag;
packet.AmbientTemperatur = AmbientTemperatur;
packet.AirPressure = AirPressure;
packet.ActualFuelPressure = ActualFuelPressure;
packet.FuelPumpDutyCycle = FuelPumpDutyCycle;
packet.ActualJet1DutyCycle = ActualJet1DutyCycle;
packet.ActualRPM = ActualRPM;
packet.CHTemperature1 = CHTemperature1;
packet.counts = counts;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_EngineState_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_EngineState;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
}
/**
* @brief Pack a enginestate 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 time_boot_ms [ms] Timestamp (milliseconds since system boot)
* @param ChokeFlag ChokeFlag
* @param Ignition2Flag Ignition2Flag
* @param AmbientTemperatur AmbientTemperatur
* @param AirPressure AirPressure
* @param ActualFuelPressure ActualFuelPressure
* @param FuelPumpDutyCycle FuelPumpDutyCycle
* @param ActualJet1DutyCycle ActualJet1DutyCycle
* @param ActualRPM ActualRPM
* @param CHTemperature1 CHTemperature1
* @param counts received number
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_enginestate_pack_chan(uint16_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint32_t time_boot_ms,uint16_t ChokeFlag,uint16_t Ignition2Flag,uint16_t AmbientTemperatur,uint16_t AirPressure,uint16_t ActualFuelPressure,uint16_t FuelPumpDutyCycle,uint16_t ActualJet1DutyCycle,uint16_t ActualRPM,uint16_t CHTemperature1,uint16_t counts)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_EngineState_LEN];
_mav_put_uint32_t(buf, 0, time_boot_ms);
_mav_put_uint16_t(buf, 4, ChokeFlag);
_mav_put_uint16_t(buf, 6, Ignition2Flag);
_mav_put_uint16_t(buf, 8, AmbientTemperatur);
_mav_put_uint16_t(buf, 10, AirPressure);
_mav_put_uint16_t(buf, 12, ActualFuelPressure);
_mav_put_uint16_t(buf, 14, FuelPumpDutyCycle);
_mav_put_uint16_t(buf, 16, ActualJet1DutyCycle);
_mav_put_uint16_t(buf, 18, ActualRPM);
_mav_put_uint16_t(buf, 20, CHTemperature1);
_mav_put_uint16_t(buf, 22, counts);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_EngineState_LEN);
#else
mavlink_enginestate_t packet;
packet.time_boot_ms = time_boot_ms;
packet.ChokeFlag = ChokeFlag;
packet.Ignition2Flag = Ignition2Flag;
packet.AmbientTemperatur = AmbientTemperatur;
packet.AirPressure = AirPressure;
packet.ActualFuelPressure = ActualFuelPressure;
packet.FuelPumpDutyCycle = FuelPumpDutyCycle;
packet.ActualJet1DutyCycle = ActualJet1DutyCycle;
packet.ActualRPM = ActualRPM;
packet.CHTemperature1 = CHTemperature1;
packet.counts = counts;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_EngineState_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_EngineState;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
}
/**
* @brief Encode a enginestate 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 enginestate C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_enginestate_encode(uint16_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_enginestate_t* enginestate)
{
return mavlink_msg_enginestate_pack(system_id, component_id, msg, enginestate->time_boot_ms, enginestate->ChokeFlag, enginestate->Ignition2Flag, enginestate->AmbientTemperatur, enginestate->AirPressure, enginestate->ActualFuelPressure, enginestate->FuelPumpDutyCycle, enginestate->ActualJet1DutyCycle, enginestate->ActualRPM, enginestate->CHTemperature1, enginestate->counts);
}
/**
* @brief Encode a enginestate 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 enginestate C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_enginestate_encode_chan(uint16_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_enginestate_t* enginestate)
{
return mavlink_msg_enginestate_pack_chan(system_id, component_id, chan, msg, enginestate->time_boot_ms, enginestate->ChokeFlag, enginestate->Ignition2Flag, enginestate->AmbientTemperatur, enginestate->AirPressure, enginestate->ActualFuelPressure, enginestate->FuelPumpDutyCycle, enginestate->ActualJet1DutyCycle, enginestate->ActualRPM, enginestate->CHTemperature1, enginestate->counts);
}
/**
* @brief Send a enginestate message
* @param chan MAVLink channel to send the message
*
* @param time_boot_ms [ms] Timestamp (milliseconds since system boot)
* @param ChokeFlag ChokeFlag
* @param Ignition2Flag Ignition2Flag
* @param AmbientTemperatur AmbientTemperatur
* @param AirPressure AirPressure
* @param ActualFuelPressure ActualFuelPressure
* @param FuelPumpDutyCycle FuelPumpDutyCycle
* @param ActualJet1DutyCycle ActualJet1DutyCycle
* @param ActualRPM ActualRPM
* @param CHTemperature1 CHTemperature1
* @param counts received number
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_enginestate_send(mavlink_channel_t chan, uint32_t time_boot_ms, uint16_t ChokeFlag, uint16_t Ignition2Flag, uint16_t AmbientTemperatur, uint16_t AirPressure, uint16_t ActualFuelPressure, uint16_t FuelPumpDutyCycle, uint16_t ActualJet1DutyCycle, uint16_t ActualRPM, uint16_t CHTemperature1, uint16_t counts)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_EngineState_LEN];
_mav_put_uint32_t(buf, 0, time_boot_ms);
_mav_put_uint16_t(buf, 4, ChokeFlag);
_mav_put_uint16_t(buf, 6, Ignition2Flag);
_mav_put_uint16_t(buf, 8, AmbientTemperatur);
_mav_put_uint16_t(buf, 10, AirPressure);
_mav_put_uint16_t(buf, 12, ActualFuelPressure);
_mav_put_uint16_t(buf, 14, FuelPumpDutyCycle);
_mav_put_uint16_t(buf, 16, ActualJet1DutyCycle);
_mav_put_uint16_t(buf, 18, ActualRPM);
_mav_put_uint16_t(buf, 20, CHTemperature1);
_mav_put_uint16_t(buf, 22, counts);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_EngineState, buf, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
#else
mavlink_enginestate_t packet;
packet.time_boot_ms = time_boot_ms;
packet.ChokeFlag = ChokeFlag;
packet.Ignition2Flag = Ignition2Flag;
packet.AmbientTemperatur = AmbientTemperatur;
packet.AirPressure = AirPressure;
packet.ActualFuelPressure = ActualFuelPressure;
packet.FuelPumpDutyCycle = FuelPumpDutyCycle;
packet.ActualJet1DutyCycle = ActualJet1DutyCycle;
packet.ActualRPM = ActualRPM;
packet.CHTemperature1 = CHTemperature1;
packet.counts = counts;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_EngineState, (const char *)&packet, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
#endif
}
/**
* @brief Send a enginestate message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_enginestate_send_struct(mavlink_channel_t chan, const mavlink_enginestate_t* enginestate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_enginestate_send(chan, enginestate->time_boot_ms, enginestate->ChokeFlag, enginestate->Ignition2Flag, enginestate->AmbientTemperatur, enginestate->AirPressure, enginestate->ActualFuelPressure, enginestate->FuelPumpDutyCycle, enginestate->ActualJet1DutyCycle, enginestate->ActualRPM, enginestate->CHTemperature1, enginestate->counts);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_EngineState, (const char *)enginestate, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
#endif
}
#if MAVLINK_MSG_ID_EngineState_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
This varient of _send() can be used to save stack space by re-using
memory from the receive buffer. The caller provides a
mavlink_message_t which is the size of a full mavlink message. This
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_enginestate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint16_t ChokeFlag, uint16_t Ignition2Flag, uint16_t AmbientTemperatur, uint16_t AirPressure, uint16_t ActualFuelPressure, uint16_t FuelPumpDutyCycle, uint16_t ActualJet1DutyCycle, uint16_t ActualRPM, uint16_t CHTemperature1, uint16_t counts)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint32_t(buf, 0, time_boot_ms);
_mav_put_uint16_t(buf, 4, ChokeFlag);
_mav_put_uint16_t(buf, 6, Ignition2Flag);
_mav_put_uint16_t(buf, 8, AmbientTemperatur);
_mav_put_uint16_t(buf, 10, AirPressure);
_mav_put_uint16_t(buf, 12, ActualFuelPressure);
_mav_put_uint16_t(buf, 14, FuelPumpDutyCycle);
_mav_put_uint16_t(buf, 16, ActualJet1DutyCycle);
_mav_put_uint16_t(buf, 18, ActualRPM);
_mav_put_uint16_t(buf, 20, CHTemperature1);
_mav_put_uint16_t(buf, 22, counts);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_EngineState, buf, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
#else
mavlink_enginestate_t *packet = (mavlink_enginestate_t *)msgbuf;
packet->time_boot_ms = time_boot_ms;
packet->ChokeFlag = ChokeFlag;
packet->Ignition2Flag = Ignition2Flag;
packet->AmbientTemperatur = AmbientTemperatur;
packet->AirPressure = AirPressure;
packet->ActualFuelPressure = ActualFuelPressure;
packet->FuelPumpDutyCycle = FuelPumpDutyCycle;
packet->ActualJet1DutyCycle = ActualJet1DutyCycle;
packet->ActualRPM = ActualRPM;
packet->CHTemperature1 = CHTemperature1;
packet->counts = counts;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_EngineState, (const char *)packet, MAVLINK_MSG_ID_EngineState_MIN_LEN, MAVLINK_MSG_ID_EngineState_LEN, MAVLINK_MSG_ID_EngineState_CRC);
#endif
}
#endif
#endif
// MESSAGE EngineState UNPACKING
/**
* @brief Get field time_boot_ms from enginestate message
*
* @return [ms] Timestamp (milliseconds since system boot)
*/
static inline uint32_t mavlink_msg_enginestate_get_time_boot_ms(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint32_t(msg, 0);
}
/**
* @brief Get field ChokeFlag from enginestate message
*
* @return ChokeFlag
*/
static inline uint16_t mavlink_msg_enginestate_get_ChokeFlag(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 4);
}
/**
* @brief Get field Ignition2Flag from enginestate message
*
* @return Ignition2Flag
*/
static inline uint16_t mavlink_msg_enginestate_get_Ignition2Flag(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 6);
}
/**
* @brief Get field AmbientTemperatur from enginestate message
*
* @return AmbientTemperatur
*/
static inline uint16_t mavlink_msg_enginestate_get_AmbientTemperatur(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 8);
}
/**
* @brief Get field AirPressure from enginestate message
*
* @return AirPressure
*/
static inline uint16_t mavlink_msg_enginestate_get_AirPressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 10);
}
/**
* @brief Get field ActualFuelPressure from enginestate message
*
* @return ActualFuelPressure
*/
static inline uint16_t mavlink_msg_enginestate_get_ActualFuelPressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 12);
}
/**
* @brief Get field FuelPumpDutyCycle from enginestate message
*
* @return FuelPumpDutyCycle
*/
static inline uint16_t mavlink_msg_enginestate_get_FuelPumpDutyCycle(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 14);
}
/**
* @brief Get field ActualJet1DutyCycle from enginestate message
*
* @return ActualJet1DutyCycle
*/
static inline uint16_t mavlink_msg_enginestate_get_ActualJet1DutyCycle(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 16);
}
/**
* @brief Get field ActualRPM from enginestate message
*
* @return ActualRPM
*/
static inline uint16_t mavlink_msg_enginestate_get_ActualRPM(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 18);
}
/**
* @brief Get field CHTemperature1 from enginestate message
*
* @return CHTemperature1
*/
static inline uint16_t mavlink_msg_enginestate_get_CHTemperature1(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 20);
}
/**
* @brief Get field counts from enginestate message
*
* @return received number
*/
static inline uint16_t mavlink_msg_enginestate_get_counts(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 22);
}
/**
* @brief Decode a enginestate message into a struct
*
* @param msg The message to decode
* @param enginestate C-struct to decode the message contents into
*/
static inline void mavlink_msg_enginestate_decode(const mavlink_message_t* msg, mavlink_enginestate_t* enginestate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
enginestate->time_boot_ms = mavlink_msg_enginestate_get_time_boot_ms(msg);
enginestate->ChokeFlag = mavlink_msg_enginestate_get_ChokeFlag(msg);
enginestate->Ignition2Flag = mavlink_msg_enginestate_get_Ignition2Flag(msg);
enginestate->AmbientTemperatur = mavlink_msg_enginestate_get_AmbientTemperatur(msg);
enginestate->AirPressure = mavlink_msg_enginestate_get_AirPressure(msg);
enginestate->ActualFuelPressure = mavlink_msg_enginestate_get_ActualFuelPressure(msg);
enginestate->FuelPumpDutyCycle = mavlink_msg_enginestate_get_FuelPumpDutyCycle(msg);
enginestate->ActualJet1DutyCycle = mavlink_msg_enginestate_get_ActualJet1DutyCycle(msg);
enginestate->ActualRPM = mavlink_msg_enginestate_get_ActualRPM(msg);
enginestate->CHTemperature1 = mavlink_msg_enginestate_get_CHTemperature1(msg);
enginestate->counts = mavlink_msg_enginestate_get_counts(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_EngineState_LEN? msg->len : MAVLINK_MSG_ID_EngineState_LEN;
memset(enginestate, 0, MAVLINK_MSG_ID_EngineState_LEN);
memcpy(enginestate, _MAV_PAYLOAD(msg), len);
#endif
}
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