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+#pragma once
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+// MESSAGE VK_FIXEDWING_CONTROL_VALUE PACKING
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+
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+#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE 53009
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+
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+
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+typedef struct __mavlink_vk_fixedwing_control_value_t {
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+ uint32_t timestamp; /*< [ms] Timestamp from system boot.*/
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+ float roll_value; /*< Roll control value,
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+ negative value means roll left.*/
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+ float pitch_value; /*< Pitch control value,
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+ negative value means pitch down.*/
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+ float throttle_value; /*< Throttle control
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+ value, negative value means throttle off*/
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+ float yaw_value; /*< Throttle control
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+ value, negative value means throttle off*/
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+} mavlink_vk_fixedwing_control_value_t;
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+
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+#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN 20
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+#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN 20
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+#define MAVLINK_MSG_ID_53009_LEN 20
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+#define MAVLINK_MSG_ID_53009_MIN_LEN 20
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+
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+#define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC 226
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+#define MAVLINK_MSG_ID_53009_CRC 226
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+
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+
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+
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+#if MAVLINK_COMMAND_24BIT
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+#define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \
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+ 53009, \
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+ "VK_FIXEDWING_CONTROL_VALUE", \
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+ 5, \
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+ { { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \
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+ { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \
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+ { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \
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+ { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \
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+ { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \
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+ } \
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+}
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+#else
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+#define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \
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+ "VK_FIXEDWING_CONTROL_VALUE", \
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+ 5, \
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+ { { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \
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+ { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \
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+ { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \
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+ { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \
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+ { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \
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+ } \
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+}
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+#endif
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+
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+/**
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+ * @brief Pack a vk_fixedwing_control_value message
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+ * @param system_id ID of this system
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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 timestamp [ms] Timestamp from system boot.
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+ * @param roll_value Roll control value,
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+ negative value means roll left.
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+ * @param pitch_value Pitch control value,
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+ negative value means pitch down.
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+ * @param throttle_value Throttle control
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+ value, negative value means throttle off
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+ * @param yaw_value Throttle control
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+ value, negative value means throttle off
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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_vk_fixedwing_control_value_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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+ uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
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+{
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+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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+ char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
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+ _mav_put_uint32_t(buf, 0, timestamp);
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+ _mav_put_float(buf, 4, roll_value);
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+ _mav_put_float(buf, 8, pitch_value);
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+ _mav_put_float(buf, 12, throttle_value);
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+ _mav_put_float(buf, 16, yaw_value);
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#else
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+ mavlink_vk_fixedwing_control_value_t packet;
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+ packet.timestamp = timestamp;
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+ packet.roll_value = roll_value;
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+ packet.pitch_value = pitch_value;
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+ packet.throttle_value = throttle_value;
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+ packet.yaw_value = yaw_value;
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#endif
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+
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+ msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
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+ return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+}
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+
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+/**
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+ * @brief Pack a vk_fixedwing_control_value message
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+ * @param system_id ID of this system
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+ * @param component_id ID of this component (e.g. 200 for IMU)
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+ * @param status MAVLink status structure
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+ * @param msg The MAVLink message to compress the data into
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+ *
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+ * @param timestamp [ms] Timestamp from system boot.
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+ * @param roll_value Roll control value,
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+ negative value means roll left.
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+ * @param pitch_value Pitch control value,
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+ negative value means pitch down.
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+ * @param throttle_value Throttle control
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+ value, negative value means throttle off
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+ * @param yaw_value Throttle control
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+ value, negative value means throttle off
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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_vk_fixedwing_control_value_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg,
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+ uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
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+{
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+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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+ char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
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+ _mav_put_uint32_t(buf, 0, timestamp);
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+ _mav_put_float(buf, 4, roll_value);
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+ _mav_put_float(buf, 8, pitch_value);
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+ _mav_put_float(buf, 12, throttle_value);
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+ _mav_put_float(buf, 16, yaw_value);
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#else
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+ mavlink_vk_fixedwing_control_value_t packet;
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+ packet.timestamp = timestamp;
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+ packet.roll_value = roll_value;
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+ packet.pitch_value = pitch_value;
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+ packet.throttle_value = throttle_value;
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+ packet.yaw_value = yaw_value;
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#endif
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+
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+ msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
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+#if MAVLINK_CRC_EXTRA
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+ return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+#else
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+ return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#endif
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+}
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+
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+/**
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+ * @brief Pack a vk_fixedwing_control_value message on a channel
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+ * @param system_id ID of this system
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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 timestamp [ms] Timestamp from system boot.
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+ * @param roll_value Roll control value,
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+ negative value means roll left.
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+ * @param pitch_value Pitch control value,
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+ negative value means pitch down.
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+ * @param throttle_value Throttle control
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+ value, negative value means throttle off
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+ * @param yaw_value Throttle control
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+ value, negative value means throttle off
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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_vk_fixedwing_control_value_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
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+ mavlink_message_t* msg,
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+ uint32_t timestamp,float roll_value,float pitch_value,float throttle_value,float yaw_value)
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+{
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+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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+ char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
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+ _mav_put_uint32_t(buf, 0, timestamp);
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+ _mav_put_float(buf, 4, roll_value);
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+ _mav_put_float(buf, 8, pitch_value);
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+ _mav_put_float(buf, 12, throttle_value);
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+ _mav_put_float(buf, 16, yaw_value);
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#else
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+ mavlink_vk_fixedwing_control_value_t packet;
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+ packet.timestamp = timestamp;
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+ packet.roll_value = roll_value;
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+ packet.pitch_value = pitch_value;
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+ packet.throttle_value = throttle_value;
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+ packet.yaw_value = yaw_value;
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+
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+ memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
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+#endif
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+
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+ msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE;
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+ return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+}
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+
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+/**
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+ * @brief Encode a vk_fixedwing_control_value struct
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+ *
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+ * @param system_id ID of this system
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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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+ * @param vk_fixedwing_control_value C-struct to read the message contents from
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+ */
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+static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
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+{
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+ return mavlink_msg_vk_fixedwing_control_value_pack(system_id, component_id, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
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+}
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+
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+/**
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+ * @brief Encode a vk_fixedwing_control_value struct on a channel
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+ *
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+ * @param system_id ID of this system
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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 vk_fixedwing_control_value C-struct to read the message contents from
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+ */
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+static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
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+{
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+ return mavlink_msg_vk_fixedwing_control_value_pack_chan(system_id, component_id, chan, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
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+}
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+
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+/**
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+ * @brief Encode a vk_fixedwing_control_value struct with provided status structure
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+ *
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+ * @param system_id ID of this system
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+ * @param component_id ID of this component (e.g. 200 for IMU)
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+ * @param status MAVLink status structure
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+ * @param msg The MAVLink message to compress the data into
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+ * @param vk_fixedwing_control_value C-struct to read the message contents from
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+ */
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+static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
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+{
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+ return mavlink_msg_vk_fixedwing_control_value_pack_status(system_id, component_id, _status, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
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+}
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+
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+/**
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+ * @brief Send a vk_fixedwing_control_value message
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+ * @param chan MAVLink channel to send the message
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+ *
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+ * @param timestamp [ms] Timestamp from system boot.
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+ * @param roll_value Roll control value,
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+ negative value means roll left.
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+ * @param pitch_value Pitch control value,
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+ negative value means pitch down.
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+ * @param throttle_value Throttle control
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+ value, negative value means throttle off
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+ * @param yaw_value Throttle control
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+ value, negative value means throttle off
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+ */
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+#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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+
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+static inline void mavlink_msg_vk_fixedwing_control_value_send(mavlink_channel_t chan, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
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+{
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+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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+ char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN];
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+ _mav_put_uint32_t(buf, 0, timestamp);
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+ _mav_put_float(buf, 4, roll_value);
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+ _mav_put_float(buf, 8, pitch_value);
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+ _mav_put_float(buf, 12, throttle_value);
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+ _mav_put_float(buf, 16, yaw_value);
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+
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+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+#else
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+ mavlink_vk_fixedwing_control_value_t packet;
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+ packet.timestamp = timestamp;
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+ packet.roll_value = roll_value;
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+ packet.pitch_value = pitch_value;
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+ packet.throttle_value = throttle_value;
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+ packet.yaw_value = yaw_value;
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+
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+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)&packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+#endif
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+}
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+
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+/**
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+ * @brief Send a vk_fixedwing_control_value message
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+ * @param chan MAVLink channel to send the message
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+ * @param struct The MAVLink struct to serialize
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+ */
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+static inline void mavlink_msg_vk_fixedwing_control_value_send_struct(mavlink_channel_t chan, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
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+{
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+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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+ mavlink_msg_vk_fixedwing_control_value_send(chan, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value);
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+#else
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+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)vk_fixedwing_control_value, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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+#endif
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+}
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+
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+#if MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN <= MAVLINK_MAX_PAYLOAD_LEN
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+/*
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+ This variant of _send() can be used to save stack space by re-using
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|
+ memory from the receive buffer. The caller provides a
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|
+ mavlink_message_t which is the size of a full mavlink message. This
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+ is usually the receive buffer for the channel, and allows a reply to an
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|
+ incoming message with minimum stack space usage.
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+ */
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|
+static inline void mavlink_msg_vk_fixedwing_control_value_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value)
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|
|
+{
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|
+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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|
+ char *buf = (char *)msgbuf;
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|
+ _mav_put_uint32_t(buf, 0, timestamp);
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+ _mav_put_float(buf, 4, roll_value);
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+ _mav_put_float(buf, 8, pitch_value);
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+ _mav_put_float(buf, 12, throttle_value);
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+ _mav_put_float(buf, 16, yaw_value);
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+
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+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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|
|
+#else
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+ mavlink_vk_fixedwing_control_value_t *packet = (mavlink_vk_fixedwing_control_value_t *)msgbuf;
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|
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+ packet->timestamp = timestamp;
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+ packet->roll_value = roll_value;
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+ packet->pitch_value = pitch_value;
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+ packet->throttle_value = throttle_value;
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+ packet->yaw_value = yaw_value;
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+
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|
+ _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC);
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|
|
+#endif
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|
|
+}
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|
|
+#endif
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|
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+
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|
|
+#endif
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|
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+
|
|
|
+// MESSAGE VK_FIXEDWING_CONTROL_VALUE UNPACKING
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+
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+
|
|
|
+/**
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|
|
+ * @brief Get field timestamp from vk_fixedwing_control_value message
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|
|
+ *
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|
+ * @return [ms] Timestamp from system boot.
|
|
|
+ */
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|
|
+static inline uint32_t mavlink_msg_vk_fixedwing_control_value_get_timestamp(const mavlink_message_t* msg)
|
|
|
+{
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|
|
+ return _MAV_RETURN_uint32_t(msg, 0);
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|
|
+}
|
|
|
+
|
|
|
+/**
|
|
|
+ * @brief Get field roll_value from vk_fixedwing_control_value message
|
|
|
+ *
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|
|
+ * @return Roll control value,
|
|
|
+ negative value means roll left.
|
|
|
+ */
|
|
|
+static inline float mavlink_msg_vk_fixedwing_control_value_get_roll_value(const mavlink_message_t* msg)
|
|
|
+{
|
|
|
+ return _MAV_RETURN_float(msg, 4);
|
|
|
+}
|
|
|
+
|
|
|
+/**
|
|
|
+ * @brief Get field pitch_value from vk_fixedwing_control_value message
|
|
|
+ *
|
|
|
+ * @return Pitch control value,
|
|
|
+ negative value means pitch down.
|
|
|
+ */
|
|
|
+static inline float mavlink_msg_vk_fixedwing_control_value_get_pitch_value(const mavlink_message_t* msg)
|
|
|
+{
|
|
|
+ return _MAV_RETURN_float(msg, 8);
|
|
|
+}
|
|
|
+
|
|
|
+/**
|
|
|
+ * @brief Get field throttle_value from vk_fixedwing_control_value message
|
|
|
+ *
|
|
|
+ * @return Throttle control
|
|
|
+ value, negative value means throttle off
|
|
|
+ */
|
|
|
+static inline float mavlink_msg_vk_fixedwing_control_value_get_throttle_value(const mavlink_message_t* msg)
|
|
|
+{
|
|
|
+ return _MAV_RETURN_float(msg, 12);
|
|
|
+}
|
|
|
+
|
|
|
+/**
|
|
|
+ * @brief Get field yaw_value from vk_fixedwing_control_value message
|
|
|
+ *
|
|
|
+ * @return Throttle control
|
|
|
+ value, negative value means throttle off
|
|
|
+ */
|
|
|
+static inline float mavlink_msg_vk_fixedwing_control_value_get_yaw_value(const mavlink_message_t* msg)
|
|
|
+{
|
|
|
+ return _MAV_RETURN_float(msg, 16);
|
|
|
+}
|
|
|
+
|
|
|
+/**
|
|
|
+ * @brief Decode a vk_fixedwing_control_value message into a struct
|
|
|
+ *
|
|
|
+ * @param msg The message to decode
|
|
|
+ * @param vk_fixedwing_control_value C-struct to decode the message contents into
|
|
|
+ */
|
|
|
+static inline void mavlink_msg_vk_fixedwing_control_value_decode(const mavlink_message_t* msg, mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value)
|
|
|
+{
|
|
|
+#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
|
+ vk_fixedwing_control_value->timestamp = mavlink_msg_vk_fixedwing_control_value_get_timestamp(msg);
|
|
|
+ vk_fixedwing_control_value->roll_value = mavlink_msg_vk_fixedwing_control_value_get_roll_value(msg);
|
|
|
+ vk_fixedwing_control_value->pitch_value = mavlink_msg_vk_fixedwing_control_value_get_pitch_value(msg);
|
|
|
+ vk_fixedwing_control_value->throttle_value = mavlink_msg_vk_fixedwing_control_value_get_throttle_value(msg);
|
|
|
+ vk_fixedwing_control_value->yaw_value = mavlink_msg_vk_fixedwing_control_value_get_yaw_value(msg);
|
|
|
+#else
|
|
|
+ uint8_t len = msg->len < MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN? msg->len : MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN;
|
|
|
+ memset(vk_fixedwing_control_value, 0, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN);
|
|
|
+ memcpy(vk_fixedwing_control_value, _MAV_PAYLOAD(msg), len);
|
|
|
+#endif
|
|
|
+}
|