Ardupilot2/libraries/GCS_MAVLink/include/slugs/mavlink_msg_pwm_commands.h
james.goppert 125b971173 Updated mavlink added eeprom class.
git-svn-id: https://arducopter.googlecode.com/svn/trunk@1239 f9c3cf11-9bcb-44bc-f272-b75c42450872
2010-12-23 23:02:51 +00:00

236 lines
9.9 KiB
C

// MESSAGE PWM_COMMANDS PACKING
#define MAVLINK_MSG_ID_PWM_COMMANDS 175
typedef struct __mavlink_pwm_commands_t
{
uint16_t dt_c; ///< AutoPilot's throttle command
uint16_t dla_c; ///< AutoPilot's left aileron command
uint16_t dra_c; ///< AutoPilot's right aileron command
uint16_t dr_c; ///< AutoPilot's rudder command
uint16_t dle_c; ///< AutoPilot's left elevator command
uint16_t dre_c; ///< AutoPilot's right elevator command
uint16_t dlf_c; ///< AutoPilot's left flap command
uint16_t drf_c; ///< AutoPilot's right flap command
uint16_t aux1; ///< AutoPilot's aux1 command
uint16_t aux2; ///< AutoPilot's aux2 command
} mavlink_pwm_commands_t;
/**
* @brief Send a pwm_commands message
*
* @param dt_c AutoPilot's throttle command
* @param dla_c AutoPilot's left aileron command
* @param dra_c AutoPilot's right aileron command
* @param dr_c AutoPilot's rudder command
* @param dle_c AutoPilot's left elevator command
* @param dre_c AutoPilot's right elevator command
* @param dlf_c AutoPilot's left flap command
* @param drf_c AutoPilot's right flap command
* @param aux1 AutoPilot's aux1 command
* @param aux2 AutoPilot's aux2 command
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_pwm_commands_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, uint16_t dt_c, uint16_t dla_c, uint16_t dra_c, uint16_t dr_c, uint16_t dle_c, uint16_t dre_c, uint16_t dlf_c, uint16_t drf_c, uint16_t aux1, uint16_t aux2)
{
uint16_t i = 0;
msg->msgid = MAVLINK_MSG_ID_PWM_COMMANDS;
i += put_uint16_t_by_index(dt_c, i, msg->payload); //AutoPilot's throttle command
i += put_uint16_t_by_index(dla_c, i, msg->payload); //AutoPilot's left aileron command
i += put_uint16_t_by_index(dra_c, i, msg->payload); //AutoPilot's right aileron command
i += put_uint16_t_by_index(dr_c, i, msg->payload); //AutoPilot's rudder command
i += put_uint16_t_by_index(dle_c, i, msg->payload); //AutoPilot's left elevator command
i += put_uint16_t_by_index(dre_c, i, msg->payload); //AutoPilot's right elevator command
i += put_uint16_t_by_index(dlf_c, i, msg->payload); //AutoPilot's left flap command
i += put_uint16_t_by_index(drf_c, i, msg->payload); //AutoPilot's right flap command
i += put_uint16_t_by_index(aux1, i, msg->payload); //AutoPilot's aux1 command
i += put_uint16_t_by_index(aux2, i, msg->payload); //AutoPilot's aux2 command
return mavlink_finalize_message(msg, system_id, component_id, i);
}
static inline uint16_t mavlink_msg_pwm_commands_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, uint8_t target, uint16_t dt_c, uint16_t dla_c, uint16_t dra_c, uint16_t dr_c, uint16_t dle_c, uint16_t dre_c, uint16_t dlf_c, uint16_t drf_c, uint16_t aux1, uint16_t aux2)
{
uint16_t i = 0;
msg->msgid = MAVLINK_MSG_ID_PWM_COMMANDS;
i += put_uint8_t_by_index(target, i, msg->payload); //The system reporting the diagnostic
i += put_uint16_t_by_index(dt_c, i, msg->payload); //AutoPilot's throttle command
i += put_uint16_t_by_index(dla_c, i, msg->payload); //AutoPilot's left aileron command
i += put_uint16_t_by_index(dra_c, i, msg->payload); //AutoPilot's right aileron command
i += put_uint16_t_by_index(dr_c, i, msg->payload); //AutoPilot's rudder command
i += put_uint16_t_by_index(dle_c, i, msg->payload); //AutoPilot's left elevator command
i += put_uint16_t_by_index(dre_c, i, msg->payload); //AutoPilot's right elevator command
i += put_uint16_t_by_index(dlf_c, i, msg->payload); //AutoPilot's left flap command
i += put_uint16_t_by_index(drf_c, i, msg->payload); //AutoPilot's right flap command
i += put_uint16_t_by_index(aux1, i, msg->payload); //AutoPilot's aux1 command
i += put_uint16_t_by_index(aux2, i, msg->payload); //AutoPilot's aux2 command
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, i);
}
static inline uint16_t mavlink_msg_pwm_commands_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_pwm_commands_t* pwm_commands)
{
return mavlink_msg_pwm_commands_pack(system_id, component_id, msg, pwm_commands->dt_c, pwm_commands->dla_c, pwm_commands->dra_c, pwm_commands->dr_c, pwm_commands->dle_c, pwm_commands->dre_c, pwm_commands->dlf_c, pwm_commands->drf_c, pwm_commands->aux1, pwm_commands->aux2);
}
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_pwm_commands_send(mavlink_channel_t chan, uint16_t dt_c, uint16_t dla_c, uint16_t dra_c, uint16_t dr_c, uint16_t dle_c, uint16_t dre_c, uint16_t dlf_c, uint16_t drf_c, uint16_t aux1, uint16_t aux2)
{
mavlink_message_t msg;
mavlink_msg_pwm_commands_pack_chan(mavlink_system.sysid, mavlink_system.compid, chan, &msg, target, dt_c, dla_c, dra_c, dr_c, dle_c, dre_c, dlf_c, drf_c, aux1, aux2);
mavlink_send_uart(chan, &msg);
}
#endif
// MESSAGE PWM_COMMANDS UNPACKING
/**
* @brief Get field dt_c from pwm_commands message
*
* @return AutoPilot's throttle command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dt_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload)[0];
r.b[0] = (msg->payload)[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dla_c from pwm_commands message
*
* @return AutoPilot's left aileron command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dla_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dra_c from pwm_commands message
*
* @return AutoPilot's right aileron command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dra_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dr_c from pwm_commands message
*
* @return AutoPilot's rudder command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dr_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dle_c from pwm_commands message
*
* @return AutoPilot's left elevator command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dle_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dre_c from pwm_commands message
*
* @return AutoPilot's right elevator command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dre_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field dlf_c from pwm_commands message
*
* @return AutoPilot's left flap command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_dlf_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field drf_c from pwm_commands message
*
* @return AutoPilot's right flap command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_drf_c(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field aux1 from pwm_commands message
*
* @return AutoPilot's aux1 command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_aux1(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
/**
* @brief Get field aux2 from pwm_commands message
*
* @return AutoPilot's aux2 command
*/
static inline uint16_t mavlink_msg_pwm_commands_get_aux2(const mavlink_message_t* msg)
{
generic_16bit r;
r.b[1] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[0];
r.b[0] = (msg->payload+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t)+sizeof(uint16_t))[1];
return (uint16_t)r.s;
}
static inline void mavlink_msg_pwm_commands_decode(const mavlink_message_t* msg, mavlink_pwm_commands_t* pwm_commands)
{
pwm_commands->dt_c = mavlink_msg_pwm_commands_get_dt_c(msg);
pwm_commands->dla_c = mavlink_msg_pwm_commands_get_dla_c(msg);
pwm_commands->dra_c = mavlink_msg_pwm_commands_get_dra_c(msg);
pwm_commands->dr_c = mavlink_msg_pwm_commands_get_dr_c(msg);
pwm_commands->dle_c = mavlink_msg_pwm_commands_get_dle_c(msg);
pwm_commands->dre_c = mavlink_msg_pwm_commands_get_dre_c(msg);
pwm_commands->dlf_c = mavlink_msg_pwm_commands_get_dlf_c(msg);
pwm_commands->drf_c = mavlink_msg_pwm_commands_get_drf_c(msg);
pwm_commands->aux1 = mavlink_msg_pwm_commands_get_aux1(msg);
pwm_commands->aux2 = mavlink_msg_pwm_commands_get_aux2(msg);
}