RflySimSDK v3.08
RflySimSDK说明文档
载入中...
搜索中...
未找到
mavlink_msg_fw_soaring_data.h
1#pragma once
2// MESSAGE FW_SOARING_DATA PACKING
3
4#define MAVLINK_MSG_ID_FW_SOARING_DATA 210
5
6MAVPACKED(
7typedef struct __mavlink_fw_soaring_data_t {
8 uint64_t timestamp; /*< Timestamp [ms]*/
9 uint64_t timestampModeChanged; /*< Timestamp since last mode change[ms]*/
10 float xW; /*< Thermal core updraft strength [m/s]*/
11 float xR; /*< Thermal radius [m]*/
12 float xLat; /*< Thermal center latitude [deg]*/
13 float xLon; /*< Thermal center longitude [deg]*/
14 float VarW; /*< Variance W*/
15 float VarR; /*< Variance R*/
16 float VarLat; /*< Variance Lat*/
17 float VarLon; /*< Variance Lon */
18 float LoiterRadius; /*< Suggested loiter radius [m]*/
19 float LoiterDirection; /*< Suggested loiter direction*/
20 float DistToSoarPoint; /*< Distance to soar point [m]*/
21 float vSinkExp; /*< Expected sink rate at current airspeed, roll and throttle [m/s]*/
22 float z1_LocalUpdraftSpeed; /*< Measurement / updraft speed at current/local airplane position [m/s]*/
23 float z2_DeltaRoll; /*< Measurement / roll angle tracking error [deg]*/
24 float z1_exp; /*< Expected measurement 1*/
25 float z2_exp; /*< Expected measurement 2*/
26 float ThermalGSNorth; /*< Thermal drift (from estimator prediction step only) [m/s]*/
27 float ThermalGSEast; /*< Thermal drift (from estimator prediction step only) [m/s]*/
28 float TSE_dot; /*< Total specific energy change (filtered) [m/s]*/
29 float DebugVar1; /*< Debug variable 1*/
30 float DebugVar2; /*< Debug variable 2*/
31 uint8_t ControlMode; /*< Control Mode [-]*/
32 uint8_t valid; /*< Data valid [-]*/
33}) mavlink_fw_soaring_data_t;
34
35#define MAVLINK_MSG_ID_FW_SOARING_DATA_LEN 102
36#define MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN 102
37#define MAVLINK_MSG_ID_210_LEN 102
38#define MAVLINK_MSG_ID_210_MIN_LEN 102
39
40#define MAVLINK_MSG_ID_FW_SOARING_DATA_CRC 20
41#define MAVLINK_MSG_ID_210_CRC 20
42
43
44
45#if MAVLINK_COMMAND_24BIT
46#define MAVLINK_MESSAGE_INFO_FW_SOARING_DATA { \
47 210, \
48 "FW_SOARING_DATA", \
49 25, \
50 { { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_fw_soaring_data_t, timestamp) }, \
51 { "timestampModeChanged", NULL, MAVLINK_TYPE_UINT64_T, 0, 8, offsetof(mavlink_fw_soaring_data_t, timestampModeChanged) }, \
52 { "xW", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_fw_soaring_data_t, xW) }, \
53 { "xR", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_fw_soaring_data_t, xR) }, \
54 { "xLat", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_fw_soaring_data_t, xLat) }, \
55 { "xLon", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_fw_soaring_data_t, xLon) }, \
56 { "VarW", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_fw_soaring_data_t, VarW) }, \
57 { "VarR", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_fw_soaring_data_t, VarR) }, \
58 { "VarLat", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_fw_soaring_data_t, VarLat) }, \
59 { "VarLon", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_fw_soaring_data_t, VarLon) }, \
60 { "LoiterRadius", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_fw_soaring_data_t, LoiterRadius) }, \
61 { "LoiterDirection", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_fw_soaring_data_t, LoiterDirection) }, \
62 { "DistToSoarPoint", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_fw_soaring_data_t, DistToSoarPoint) }, \
63 { "vSinkExp", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_fw_soaring_data_t, vSinkExp) }, \
64 { "z1_LocalUpdraftSpeed", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_fw_soaring_data_t, z1_LocalUpdraftSpeed) }, \
65 { "z2_DeltaRoll", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_fw_soaring_data_t, z2_DeltaRoll) }, \
66 { "z1_exp", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_fw_soaring_data_t, z1_exp) }, \
67 { "z2_exp", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_fw_soaring_data_t, z2_exp) }, \
68 { "ThermalGSNorth", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_fw_soaring_data_t, ThermalGSNorth) }, \
69 { "ThermalGSEast", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_fw_soaring_data_t, ThermalGSEast) }, \
70 { "TSE_dot", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_fw_soaring_data_t, TSE_dot) }, \
71 { "DebugVar1", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_fw_soaring_data_t, DebugVar1) }, \
72 { "DebugVar2", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_fw_soaring_data_t, DebugVar2) }, \
73 { "ControlMode", NULL, MAVLINK_TYPE_UINT8_T, 0, 100, offsetof(mavlink_fw_soaring_data_t, ControlMode) }, \
74 { "valid", NULL, MAVLINK_TYPE_UINT8_T, 0, 101, offsetof(mavlink_fw_soaring_data_t, valid) }, \
75 } \
76}
77#else
78#define MAVLINK_MESSAGE_INFO_FW_SOARING_DATA { \
79 "FW_SOARING_DATA", \
80 25, \
81 { { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_fw_soaring_data_t, timestamp) }, \
82 { "timestampModeChanged", NULL, MAVLINK_TYPE_UINT64_T, 0, 8, offsetof(mavlink_fw_soaring_data_t, timestampModeChanged) }, \
83 { "xW", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_fw_soaring_data_t, xW) }, \
84 { "xR", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_fw_soaring_data_t, xR) }, \
85 { "xLat", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_fw_soaring_data_t, xLat) }, \
86 { "xLon", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_fw_soaring_data_t, xLon) }, \
87 { "VarW", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_fw_soaring_data_t, VarW) }, \
88 { "VarR", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_fw_soaring_data_t, VarR) }, \
89 { "VarLat", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_fw_soaring_data_t, VarLat) }, \
90 { "VarLon", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_fw_soaring_data_t, VarLon) }, \
91 { "LoiterRadius", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_fw_soaring_data_t, LoiterRadius) }, \
92 { "LoiterDirection", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_fw_soaring_data_t, LoiterDirection) }, \
93 { "DistToSoarPoint", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_fw_soaring_data_t, DistToSoarPoint) }, \
94 { "vSinkExp", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_fw_soaring_data_t, vSinkExp) }, \
95 { "z1_LocalUpdraftSpeed", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_fw_soaring_data_t, z1_LocalUpdraftSpeed) }, \
96 { "z2_DeltaRoll", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_fw_soaring_data_t, z2_DeltaRoll) }, \
97 { "z1_exp", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_fw_soaring_data_t, z1_exp) }, \
98 { "z2_exp", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_fw_soaring_data_t, z2_exp) }, \
99 { "ThermalGSNorth", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_fw_soaring_data_t, ThermalGSNorth) }, \
100 { "ThermalGSEast", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_fw_soaring_data_t, ThermalGSEast) }, \
101 { "TSE_dot", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_fw_soaring_data_t, TSE_dot) }, \
102 { "DebugVar1", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_fw_soaring_data_t, DebugVar1) }, \
103 { "DebugVar2", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_fw_soaring_data_t, DebugVar2) }, \
104 { "ControlMode", NULL, MAVLINK_TYPE_UINT8_T, 0, 100, offsetof(mavlink_fw_soaring_data_t, ControlMode) }, \
105 { "valid", NULL, MAVLINK_TYPE_UINT8_T, 0, 101, offsetof(mavlink_fw_soaring_data_t, valid) }, \
106 } \
107}
108#endif
109
110/**
111 * @brief Pack a fw_soaring_data message
112 * @param system_id ID of this system
113 * @param component_id ID of this component (e.g. 200 for IMU)
114 * @param msg The MAVLink message to compress the data into
115 *
116 * @param timestamp Timestamp [ms]
117 * @param timestampModeChanged Timestamp since last mode change[ms]
118 * @param xW Thermal core updraft strength [m/s]
119 * @param xR Thermal radius [m]
120 * @param xLat Thermal center latitude [deg]
121 * @param xLon Thermal center longitude [deg]
122 * @param VarW Variance W
123 * @param VarR Variance R
124 * @param VarLat Variance Lat
125 * @param VarLon Variance Lon
126 * @param LoiterRadius Suggested loiter radius [m]
127 * @param LoiterDirection Suggested loiter direction
128 * @param DistToSoarPoint Distance to soar point [m]
129 * @param vSinkExp Expected sink rate at current airspeed, roll and throttle [m/s]
130 * @param z1_LocalUpdraftSpeed Measurement / updraft speed at current/local airplane position [m/s]
131 * @param z2_DeltaRoll Measurement / roll angle tracking error [deg]
132 * @param z1_exp Expected measurement 1
133 * @param z2_exp Expected measurement 2
134 * @param ThermalGSNorth Thermal drift (from estimator prediction step only) [m/s]
135 * @param ThermalGSEast Thermal drift (from estimator prediction step only) [m/s]
136 * @param TSE_dot Total specific energy change (filtered) [m/s]
137 * @param DebugVar1 Debug variable 1
138 * @param DebugVar2 Debug variable 2
139 * @param ControlMode Control Mode [-]
140 * @param valid Data valid [-]
141 * @return length of the message in bytes (excluding serial stream start sign)
142 */
143static inline uint16_t mavlink_msg_fw_soaring_data_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
144 uint64_t timestamp, uint64_t timestampModeChanged, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, float LoiterDirection, float DistToSoarPoint, float vSinkExp, float z1_LocalUpdraftSpeed, float z2_DeltaRoll, float z1_exp, float z2_exp, float ThermalGSNorth, float ThermalGSEast, float TSE_dot, float DebugVar1, float DebugVar2, uint8_t ControlMode, uint8_t valid)
145{
146#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
147 char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN];
148 _mav_put_uint64_t(buf, 0, timestamp);
149 _mav_put_uint64_t(buf, 8, timestampModeChanged);
150 _mav_put_float(buf, 16, xW);
151 _mav_put_float(buf, 20, xR);
152 _mav_put_float(buf, 24, xLat);
153 _mav_put_float(buf, 28, xLon);
154 _mav_put_float(buf, 32, VarW);
155 _mav_put_float(buf, 36, VarR);
156 _mav_put_float(buf, 40, VarLat);
157 _mav_put_float(buf, 44, VarLon);
158 _mav_put_float(buf, 48, LoiterRadius);
159 _mav_put_float(buf, 52, LoiterDirection);
160 _mav_put_float(buf, 56, DistToSoarPoint);
161 _mav_put_float(buf, 60, vSinkExp);
162 _mav_put_float(buf, 64, z1_LocalUpdraftSpeed);
163 _mav_put_float(buf, 68, z2_DeltaRoll);
164 _mav_put_float(buf, 72, z1_exp);
165 _mav_put_float(buf, 76, z2_exp);
166 _mav_put_float(buf, 80, ThermalGSNorth);
167 _mav_put_float(buf, 84, ThermalGSEast);
168 _mav_put_float(buf, 88, TSE_dot);
169 _mav_put_float(buf, 92, DebugVar1);
170 _mav_put_float(buf, 96, DebugVar2);
171 _mav_put_uint8_t(buf, 100, ControlMode);
172 _mav_put_uint8_t(buf, 101, valid);
173
174 memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN);
175#else
176 mavlink_fw_soaring_data_t packet;
177 packet.timestamp = timestamp;
178 packet.timestampModeChanged = timestampModeChanged;
179 packet.xW = xW;
180 packet.xR = xR;
181 packet.xLat = xLat;
182 packet.xLon = xLon;
183 packet.VarW = VarW;
184 packet.VarR = VarR;
185 packet.VarLat = VarLat;
186 packet.VarLon = VarLon;
187 packet.LoiterRadius = LoiterRadius;
188 packet.LoiterDirection = LoiterDirection;
189 packet.DistToSoarPoint = DistToSoarPoint;
190 packet.vSinkExp = vSinkExp;
191 packet.z1_LocalUpdraftSpeed = z1_LocalUpdraftSpeed;
192 packet.z2_DeltaRoll = z2_DeltaRoll;
193 packet.z1_exp = z1_exp;
194 packet.z2_exp = z2_exp;
195 packet.ThermalGSNorth = ThermalGSNorth;
196 packet.ThermalGSEast = ThermalGSEast;
197 packet.TSE_dot = TSE_dot;
198 packet.DebugVar1 = DebugVar1;
199 packet.DebugVar2 = DebugVar2;
200 packet.ControlMode = ControlMode;
201 packet.valid = valid;
202
203 memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN);
204#endif
205
206 msg->msgid = MAVLINK_MSG_ID_FW_SOARING_DATA;
207 return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
208}
209
210/**
211 * @brief Pack a fw_soaring_data message on a channel
212 * @param system_id ID of this system
213 * @param component_id ID of this component (e.g. 200 for IMU)
214 * @param chan The MAVLink channel this message will be sent over
215 * @param msg The MAVLink message to compress the data into
216 * @param timestamp Timestamp [ms]
217 * @param timestampModeChanged Timestamp since last mode change[ms]
218 * @param xW Thermal core updraft strength [m/s]
219 * @param xR Thermal radius [m]
220 * @param xLat Thermal center latitude [deg]
221 * @param xLon Thermal center longitude [deg]
222 * @param VarW Variance W
223 * @param VarR Variance R
224 * @param VarLat Variance Lat
225 * @param VarLon Variance Lon
226 * @param LoiterRadius Suggested loiter radius [m]
227 * @param LoiterDirection Suggested loiter direction
228 * @param DistToSoarPoint Distance to soar point [m]
229 * @param vSinkExp Expected sink rate at current airspeed, roll and throttle [m/s]
230 * @param z1_LocalUpdraftSpeed Measurement / updraft speed at current/local airplane position [m/s]
231 * @param z2_DeltaRoll Measurement / roll angle tracking error [deg]
232 * @param z1_exp Expected measurement 1
233 * @param z2_exp Expected measurement 2
234 * @param ThermalGSNorth Thermal drift (from estimator prediction step only) [m/s]
235 * @param ThermalGSEast Thermal drift (from estimator prediction step only) [m/s]
236 * @param TSE_dot Total specific energy change (filtered) [m/s]
237 * @param DebugVar1 Debug variable 1
238 * @param DebugVar2 Debug variable 2
239 * @param ControlMode Control Mode [-]
240 * @param valid Data valid [-]
241 * @return length of the message in bytes (excluding serial stream start sign)
242 */
243static inline uint16_t mavlink_msg_fw_soaring_data_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
244 mavlink_message_t* msg,
245 uint64_t timestamp,uint64_t timestampModeChanged,float xW,float xR,float xLat,float xLon,float VarW,float VarR,float VarLat,float VarLon,float LoiterRadius,float LoiterDirection,float DistToSoarPoint,float vSinkExp,float z1_LocalUpdraftSpeed,float z2_DeltaRoll,float z1_exp,float z2_exp,float ThermalGSNorth,float ThermalGSEast,float TSE_dot,float DebugVar1,float DebugVar2,uint8_t ControlMode,uint8_t valid)
246{
247#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
248 char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN];
249 _mav_put_uint64_t(buf, 0, timestamp);
250 _mav_put_uint64_t(buf, 8, timestampModeChanged);
251 _mav_put_float(buf, 16, xW);
252 _mav_put_float(buf, 20, xR);
253 _mav_put_float(buf, 24, xLat);
254 _mav_put_float(buf, 28, xLon);
255 _mav_put_float(buf, 32, VarW);
256 _mav_put_float(buf, 36, VarR);
257 _mav_put_float(buf, 40, VarLat);
258 _mav_put_float(buf, 44, VarLon);
259 _mav_put_float(buf, 48, LoiterRadius);
260 _mav_put_float(buf, 52, LoiterDirection);
261 _mav_put_float(buf, 56, DistToSoarPoint);
262 _mav_put_float(buf, 60, vSinkExp);
263 _mav_put_float(buf, 64, z1_LocalUpdraftSpeed);
264 _mav_put_float(buf, 68, z2_DeltaRoll);
265 _mav_put_float(buf, 72, z1_exp);
266 _mav_put_float(buf, 76, z2_exp);
267 _mav_put_float(buf, 80, ThermalGSNorth);
268 _mav_put_float(buf, 84, ThermalGSEast);
269 _mav_put_float(buf, 88, TSE_dot);
270 _mav_put_float(buf, 92, DebugVar1);
271 _mav_put_float(buf, 96, DebugVar2);
272 _mav_put_uint8_t(buf, 100, ControlMode);
273 _mav_put_uint8_t(buf, 101, valid);
274
275 memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN);
276#else
277 mavlink_fw_soaring_data_t packet;
278 packet.timestamp = timestamp;
279 packet.timestampModeChanged = timestampModeChanged;
280 packet.xW = xW;
281 packet.xR = xR;
282 packet.xLat = xLat;
283 packet.xLon = xLon;
284 packet.VarW = VarW;
285 packet.VarR = VarR;
286 packet.VarLat = VarLat;
287 packet.VarLon = VarLon;
288 packet.LoiterRadius = LoiterRadius;
289 packet.LoiterDirection = LoiterDirection;
290 packet.DistToSoarPoint = DistToSoarPoint;
291 packet.vSinkExp = vSinkExp;
292 packet.z1_LocalUpdraftSpeed = z1_LocalUpdraftSpeed;
293 packet.z2_DeltaRoll = z2_DeltaRoll;
294 packet.z1_exp = z1_exp;
295 packet.z2_exp = z2_exp;
296 packet.ThermalGSNorth = ThermalGSNorth;
297 packet.ThermalGSEast = ThermalGSEast;
298 packet.TSE_dot = TSE_dot;
299 packet.DebugVar1 = DebugVar1;
300 packet.DebugVar2 = DebugVar2;
301 packet.ControlMode = ControlMode;
302 packet.valid = valid;
303
304 memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN);
305#endif
306
307 msg->msgid = MAVLINK_MSG_ID_FW_SOARING_DATA;
308 return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
309}
310
311/**
312 * @brief Encode a fw_soaring_data struct
313 *
314 * @param system_id ID of this system
315 * @param component_id ID of this component (e.g. 200 for IMU)
316 * @param msg The MAVLink message to compress the data into
317 * @param fw_soaring_data C-struct to read the message contents from
318 */
319static inline uint16_t mavlink_msg_fw_soaring_data_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_fw_soaring_data_t* fw_soaring_data)
320{
321 return mavlink_msg_fw_soaring_data_pack(system_id, component_id, msg, fw_soaring_data->timestamp, fw_soaring_data->timestampModeChanged, fw_soaring_data->xW, fw_soaring_data->xR, fw_soaring_data->xLat, fw_soaring_data->xLon, fw_soaring_data->VarW, fw_soaring_data->VarR, fw_soaring_data->VarLat, fw_soaring_data->VarLon, fw_soaring_data->LoiterRadius, fw_soaring_data->LoiterDirection, fw_soaring_data->DistToSoarPoint, fw_soaring_data->vSinkExp, fw_soaring_data->z1_LocalUpdraftSpeed, fw_soaring_data->z2_DeltaRoll, fw_soaring_data->z1_exp, fw_soaring_data->z2_exp, fw_soaring_data->ThermalGSNorth, fw_soaring_data->ThermalGSEast, fw_soaring_data->TSE_dot, fw_soaring_data->DebugVar1, fw_soaring_data->DebugVar2, fw_soaring_data->ControlMode, fw_soaring_data->valid);
322}
323
324/**
325 * @brief Encode a fw_soaring_data struct on a channel
326 *
327 * @param system_id ID of this system
328 * @param component_id ID of this component (e.g. 200 for IMU)
329 * @param chan The MAVLink channel this message will be sent over
330 * @param msg The MAVLink message to compress the data into
331 * @param fw_soaring_data C-struct to read the message contents from
332 */
333static inline uint16_t mavlink_msg_fw_soaring_data_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_fw_soaring_data_t* fw_soaring_data)
334{
335 return mavlink_msg_fw_soaring_data_pack_chan(system_id, component_id, chan, msg, fw_soaring_data->timestamp, fw_soaring_data->timestampModeChanged, fw_soaring_data->xW, fw_soaring_data->xR, fw_soaring_data->xLat, fw_soaring_data->xLon, fw_soaring_data->VarW, fw_soaring_data->VarR, fw_soaring_data->VarLat, fw_soaring_data->VarLon, fw_soaring_data->LoiterRadius, fw_soaring_data->LoiterDirection, fw_soaring_data->DistToSoarPoint, fw_soaring_data->vSinkExp, fw_soaring_data->z1_LocalUpdraftSpeed, fw_soaring_data->z2_DeltaRoll, fw_soaring_data->z1_exp, fw_soaring_data->z2_exp, fw_soaring_data->ThermalGSNorth, fw_soaring_data->ThermalGSEast, fw_soaring_data->TSE_dot, fw_soaring_data->DebugVar1, fw_soaring_data->DebugVar2, fw_soaring_data->ControlMode, fw_soaring_data->valid);
336}
337
338/**
339 * @brief Send a fw_soaring_data message
340 * @param chan MAVLink channel to send the message
341 *
342 * @param timestamp Timestamp [ms]
343 * @param timestampModeChanged Timestamp since last mode change[ms]
344 * @param xW Thermal core updraft strength [m/s]
345 * @param xR Thermal radius [m]
346 * @param xLat Thermal center latitude [deg]
347 * @param xLon Thermal center longitude [deg]
348 * @param VarW Variance W
349 * @param VarR Variance R
350 * @param VarLat Variance Lat
351 * @param VarLon Variance Lon
352 * @param LoiterRadius Suggested loiter radius [m]
353 * @param LoiterDirection Suggested loiter direction
354 * @param DistToSoarPoint Distance to soar point [m]
355 * @param vSinkExp Expected sink rate at current airspeed, roll and throttle [m/s]
356 * @param z1_LocalUpdraftSpeed Measurement / updraft speed at current/local airplane position [m/s]
357 * @param z2_DeltaRoll Measurement / roll angle tracking error [deg]
358 * @param z1_exp Expected measurement 1
359 * @param z2_exp Expected measurement 2
360 * @param ThermalGSNorth Thermal drift (from estimator prediction step only) [m/s]
361 * @param ThermalGSEast Thermal drift (from estimator prediction step only) [m/s]
362 * @param TSE_dot Total specific energy change (filtered) [m/s]
363 * @param DebugVar1 Debug variable 1
364 * @param DebugVar2 Debug variable 2
365 * @param ControlMode Control Mode [-]
366 * @param valid Data valid [-]
367 */
368#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
369
370static inline void mavlink_msg_fw_soaring_data_send(mavlink_channel_t chan, uint64_t timestamp, uint64_t timestampModeChanged, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, float LoiterDirection, float DistToSoarPoint, float vSinkExp, float z1_LocalUpdraftSpeed, float z2_DeltaRoll, float z1_exp, float z2_exp, float ThermalGSNorth, float ThermalGSEast, float TSE_dot, float DebugVar1, float DebugVar2, uint8_t ControlMode, uint8_t valid)
371{
372#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
373 char buf[MAVLINK_MSG_ID_FW_SOARING_DATA_LEN];
374 _mav_put_uint64_t(buf, 0, timestamp);
375 _mav_put_uint64_t(buf, 8, timestampModeChanged);
376 _mav_put_float(buf, 16, xW);
377 _mav_put_float(buf, 20, xR);
378 _mav_put_float(buf, 24, xLat);
379 _mav_put_float(buf, 28, xLon);
380 _mav_put_float(buf, 32, VarW);
381 _mav_put_float(buf, 36, VarR);
382 _mav_put_float(buf, 40, VarLat);
383 _mav_put_float(buf, 44, VarLon);
384 _mav_put_float(buf, 48, LoiterRadius);
385 _mav_put_float(buf, 52, LoiterDirection);
386 _mav_put_float(buf, 56, DistToSoarPoint);
387 _mav_put_float(buf, 60, vSinkExp);
388 _mav_put_float(buf, 64, z1_LocalUpdraftSpeed);
389 _mav_put_float(buf, 68, z2_DeltaRoll);
390 _mav_put_float(buf, 72, z1_exp);
391 _mav_put_float(buf, 76, z2_exp);
392 _mav_put_float(buf, 80, ThermalGSNorth);
393 _mav_put_float(buf, 84, ThermalGSEast);
394 _mav_put_float(buf, 88, TSE_dot);
395 _mav_put_float(buf, 92, DebugVar1);
396 _mav_put_float(buf, 96, DebugVar2);
397 _mav_put_uint8_t(buf, 100, ControlMode);
398 _mav_put_uint8_t(buf, 101, valid);
399
400 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
401#else
402 mavlink_fw_soaring_data_t packet;
403 packet.timestamp = timestamp;
404 packet.timestampModeChanged = timestampModeChanged;
405 packet.xW = xW;
406 packet.xR = xR;
407 packet.xLat = xLat;
408 packet.xLon = xLon;
409 packet.VarW = VarW;
410 packet.VarR = VarR;
411 packet.VarLat = VarLat;
412 packet.VarLon = VarLon;
413 packet.LoiterRadius = LoiterRadius;
414 packet.LoiterDirection = LoiterDirection;
415 packet.DistToSoarPoint = DistToSoarPoint;
416 packet.vSinkExp = vSinkExp;
417 packet.z1_LocalUpdraftSpeed = z1_LocalUpdraftSpeed;
418 packet.z2_DeltaRoll = z2_DeltaRoll;
419 packet.z1_exp = z1_exp;
420 packet.z2_exp = z2_exp;
421 packet.ThermalGSNorth = ThermalGSNorth;
422 packet.ThermalGSEast = ThermalGSEast;
423 packet.TSE_dot = TSE_dot;
424 packet.DebugVar1 = DebugVar1;
425 packet.DebugVar2 = DebugVar2;
426 packet.ControlMode = ControlMode;
427 packet.valid = valid;
428
429 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)&packet, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
430#endif
431}
432
433/**
434 * @brief Send a fw_soaring_data message
435 * @param chan MAVLink channel to send the message
436 * @param struct The MAVLink struct to serialize
437 */
438static inline void mavlink_msg_fw_soaring_data_send_struct(mavlink_channel_t chan, const mavlink_fw_soaring_data_t* fw_soaring_data)
439{
440#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
441 mavlink_msg_fw_soaring_data_send(chan, fw_soaring_data->timestamp, fw_soaring_data->timestampModeChanged, fw_soaring_data->xW, fw_soaring_data->xR, fw_soaring_data->xLat, fw_soaring_data->xLon, fw_soaring_data->VarW, fw_soaring_data->VarR, fw_soaring_data->VarLat, fw_soaring_data->VarLon, fw_soaring_data->LoiterRadius, fw_soaring_data->LoiterDirection, fw_soaring_data->DistToSoarPoint, fw_soaring_data->vSinkExp, fw_soaring_data->z1_LocalUpdraftSpeed, fw_soaring_data->z2_DeltaRoll, fw_soaring_data->z1_exp, fw_soaring_data->z2_exp, fw_soaring_data->ThermalGSNorth, fw_soaring_data->ThermalGSEast, fw_soaring_data->TSE_dot, fw_soaring_data->DebugVar1, fw_soaring_data->DebugVar2, fw_soaring_data->ControlMode, fw_soaring_data->valid);
442#else
443 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)fw_soaring_data, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
444#endif
445}
446
447#if MAVLINK_MSG_ID_FW_SOARING_DATA_LEN <= MAVLINK_MAX_PAYLOAD_LEN
448/*
449 This varient of _send() can be used to save stack space by re-using
450 memory from the receive buffer. The caller provides a
451 mavlink_message_t which is the size of a full mavlink message. This
452 is usually the receive buffer for the channel, and allows a reply to an
453 incoming message with minimum stack space usage.
454 */
455static inline void mavlink_msg_fw_soaring_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint64_t timestampModeChanged, float xW, float xR, float xLat, float xLon, float VarW, float VarR, float VarLat, float VarLon, float LoiterRadius, float LoiterDirection, float DistToSoarPoint, float vSinkExp, float z1_LocalUpdraftSpeed, float z2_DeltaRoll, float z1_exp, float z2_exp, float ThermalGSNorth, float ThermalGSEast, float TSE_dot, float DebugVar1, float DebugVar2, uint8_t ControlMode, uint8_t valid)
456{
457#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
458 char *buf = (char *)msgbuf;
459 _mav_put_uint64_t(buf, 0, timestamp);
460 _mav_put_uint64_t(buf, 8, timestampModeChanged);
461 _mav_put_float(buf, 16, xW);
462 _mav_put_float(buf, 20, xR);
463 _mav_put_float(buf, 24, xLat);
464 _mav_put_float(buf, 28, xLon);
465 _mav_put_float(buf, 32, VarW);
466 _mav_put_float(buf, 36, VarR);
467 _mav_put_float(buf, 40, VarLat);
468 _mav_put_float(buf, 44, VarLon);
469 _mav_put_float(buf, 48, LoiterRadius);
470 _mav_put_float(buf, 52, LoiterDirection);
471 _mav_put_float(buf, 56, DistToSoarPoint);
472 _mav_put_float(buf, 60, vSinkExp);
473 _mav_put_float(buf, 64, z1_LocalUpdraftSpeed);
474 _mav_put_float(buf, 68, z2_DeltaRoll);
475 _mav_put_float(buf, 72, z1_exp);
476 _mav_put_float(buf, 76, z2_exp);
477 _mav_put_float(buf, 80, ThermalGSNorth);
478 _mav_put_float(buf, 84, ThermalGSEast);
479 _mav_put_float(buf, 88, TSE_dot);
480 _mav_put_float(buf, 92, DebugVar1);
481 _mav_put_float(buf, 96, DebugVar2);
482 _mav_put_uint8_t(buf, 100, ControlMode);
483 _mav_put_uint8_t(buf, 101, valid);
484
485 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, buf, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
486#else
487 mavlink_fw_soaring_data_t *packet = (mavlink_fw_soaring_data_t *)msgbuf;
488 packet->timestamp = timestamp;
489 packet->timestampModeChanged = timestampModeChanged;
490 packet->xW = xW;
491 packet->xR = xR;
492 packet->xLat = xLat;
493 packet->xLon = xLon;
494 packet->VarW = VarW;
495 packet->VarR = VarR;
496 packet->VarLat = VarLat;
497 packet->VarLon = VarLon;
498 packet->LoiterRadius = LoiterRadius;
499 packet->LoiterDirection = LoiterDirection;
500 packet->DistToSoarPoint = DistToSoarPoint;
501 packet->vSinkExp = vSinkExp;
502 packet->z1_LocalUpdraftSpeed = z1_LocalUpdraftSpeed;
503 packet->z2_DeltaRoll = z2_DeltaRoll;
504 packet->z1_exp = z1_exp;
505 packet->z2_exp = z2_exp;
506 packet->ThermalGSNorth = ThermalGSNorth;
507 packet->ThermalGSEast = ThermalGSEast;
508 packet->TSE_dot = TSE_dot;
509 packet->DebugVar1 = DebugVar1;
510 packet->DebugVar2 = DebugVar2;
511 packet->ControlMode = ControlMode;
512 packet->valid = valid;
513
514 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FW_SOARING_DATA, (const char *)packet, MAVLINK_MSG_ID_FW_SOARING_DATA_MIN_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN, MAVLINK_MSG_ID_FW_SOARING_DATA_CRC);
515#endif
516}
517#endif
518
519#endif
520
521// MESSAGE FW_SOARING_DATA UNPACKING
522
523
524/**
525 * @brief Get field timestamp from fw_soaring_data message
526 *
527 * @return Timestamp [ms]
528 */
529static inline uint64_t mavlink_msg_fw_soaring_data_get_timestamp(const mavlink_message_t* msg)
530{
531 return _MAV_RETURN_uint64_t(msg, 0);
532}
533
534/**
535 * @brief Get field timestampModeChanged from fw_soaring_data message
536 *
537 * @return Timestamp since last mode change[ms]
538 */
539static inline uint64_t mavlink_msg_fw_soaring_data_get_timestampModeChanged(const mavlink_message_t* msg)
540{
541 return _MAV_RETURN_uint64_t(msg, 8);
542}
543
544/**
545 * @brief Get field xW from fw_soaring_data message
546 *
547 * @return Thermal core updraft strength [m/s]
548 */
549static inline float mavlink_msg_fw_soaring_data_get_xW(const mavlink_message_t* msg)
550{
551 return _MAV_RETURN_float(msg, 16);
552}
553
554/**
555 * @brief Get field xR from fw_soaring_data message
556 *
557 * @return Thermal radius [m]
558 */
559static inline float mavlink_msg_fw_soaring_data_get_xR(const mavlink_message_t* msg)
560{
561 return _MAV_RETURN_float(msg, 20);
562}
563
564/**
565 * @brief Get field xLat from fw_soaring_data message
566 *
567 * @return Thermal center latitude [deg]
568 */
569static inline float mavlink_msg_fw_soaring_data_get_xLat(const mavlink_message_t* msg)
570{
571 return _MAV_RETURN_float(msg, 24);
572}
573
574/**
575 * @brief Get field xLon from fw_soaring_data message
576 *
577 * @return Thermal center longitude [deg]
578 */
579static inline float mavlink_msg_fw_soaring_data_get_xLon(const mavlink_message_t* msg)
580{
581 return _MAV_RETURN_float(msg, 28);
582}
583
584/**
585 * @brief Get field VarW from fw_soaring_data message
586 *
587 * @return Variance W
588 */
589static inline float mavlink_msg_fw_soaring_data_get_VarW(const mavlink_message_t* msg)
590{
591 return _MAV_RETURN_float(msg, 32);
592}
593
594/**
595 * @brief Get field VarR from fw_soaring_data message
596 *
597 * @return Variance R
598 */
599static inline float mavlink_msg_fw_soaring_data_get_VarR(const mavlink_message_t* msg)
600{
601 return _MAV_RETURN_float(msg, 36);
602}
603
604/**
605 * @brief Get field VarLat from fw_soaring_data message
606 *
607 * @return Variance Lat
608 */
609static inline float mavlink_msg_fw_soaring_data_get_VarLat(const mavlink_message_t* msg)
610{
611 return _MAV_RETURN_float(msg, 40);
612}
613
614/**
615 * @brief Get field VarLon from fw_soaring_data message
616 *
617 * @return Variance Lon
618 */
619static inline float mavlink_msg_fw_soaring_data_get_VarLon(const mavlink_message_t* msg)
620{
621 return _MAV_RETURN_float(msg, 44);
622}
623
624/**
625 * @brief Get field LoiterRadius from fw_soaring_data message
626 *
627 * @return Suggested loiter radius [m]
628 */
629static inline float mavlink_msg_fw_soaring_data_get_LoiterRadius(const mavlink_message_t* msg)
630{
631 return _MAV_RETURN_float(msg, 48);
632}
633
634/**
635 * @brief Get field LoiterDirection from fw_soaring_data message
636 *
637 * @return Suggested loiter direction
638 */
639static inline float mavlink_msg_fw_soaring_data_get_LoiterDirection(const mavlink_message_t* msg)
640{
641 return _MAV_RETURN_float(msg, 52);
642}
643
644/**
645 * @brief Get field DistToSoarPoint from fw_soaring_data message
646 *
647 * @return Distance to soar point [m]
648 */
649static inline float mavlink_msg_fw_soaring_data_get_DistToSoarPoint(const mavlink_message_t* msg)
650{
651 return _MAV_RETURN_float(msg, 56);
652}
653
654/**
655 * @brief Get field vSinkExp from fw_soaring_data message
656 *
657 * @return Expected sink rate at current airspeed, roll and throttle [m/s]
658 */
659static inline float mavlink_msg_fw_soaring_data_get_vSinkExp(const mavlink_message_t* msg)
660{
661 return _MAV_RETURN_float(msg, 60);
662}
663
664/**
665 * @brief Get field z1_LocalUpdraftSpeed from fw_soaring_data message
666 *
667 * @return Measurement / updraft speed at current/local airplane position [m/s]
668 */
669static inline float mavlink_msg_fw_soaring_data_get_z1_LocalUpdraftSpeed(const mavlink_message_t* msg)
670{
671 return _MAV_RETURN_float(msg, 64);
672}
673
674/**
675 * @brief Get field z2_DeltaRoll from fw_soaring_data message
676 *
677 * @return Measurement / roll angle tracking error [deg]
678 */
679static inline float mavlink_msg_fw_soaring_data_get_z2_DeltaRoll(const mavlink_message_t* msg)
680{
681 return _MAV_RETURN_float(msg, 68);
682}
683
684/**
685 * @brief Get field z1_exp from fw_soaring_data message
686 *
687 * @return Expected measurement 1
688 */
689static inline float mavlink_msg_fw_soaring_data_get_z1_exp(const mavlink_message_t* msg)
690{
691 return _MAV_RETURN_float(msg, 72);
692}
693
694/**
695 * @brief Get field z2_exp from fw_soaring_data message
696 *
697 * @return Expected measurement 2
698 */
699static inline float mavlink_msg_fw_soaring_data_get_z2_exp(const mavlink_message_t* msg)
700{
701 return _MAV_RETURN_float(msg, 76);
702}
703
704/**
705 * @brief Get field ThermalGSNorth from fw_soaring_data message
706 *
707 * @return Thermal drift (from estimator prediction step only) [m/s]
708 */
709static inline float mavlink_msg_fw_soaring_data_get_ThermalGSNorth(const mavlink_message_t* msg)
710{
711 return _MAV_RETURN_float(msg, 80);
712}
713
714/**
715 * @brief Get field ThermalGSEast from fw_soaring_data message
716 *
717 * @return Thermal drift (from estimator prediction step only) [m/s]
718 */
719static inline float mavlink_msg_fw_soaring_data_get_ThermalGSEast(const mavlink_message_t* msg)
720{
721 return _MAV_RETURN_float(msg, 84);
722}
723
724/**
725 * @brief Get field TSE_dot from fw_soaring_data message
726 *
727 * @return Total specific energy change (filtered) [m/s]
728 */
729static inline float mavlink_msg_fw_soaring_data_get_TSE_dot(const mavlink_message_t* msg)
730{
731 return _MAV_RETURN_float(msg, 88);
732}
733
734/**
735 * @brief Get field DebugVar1 from fw_soaring_data message
736 *
737 * @return Debug variable 1
738 */
739static inline float mavlink_msg_fw_soaring_data_get_DebugVar1(const mavlink_message_t* msg)
740{
741 return _MAV_RETURN_float(msg, 92);
742}
743
744/**
745 * @brief Get field DebugVar2 from fw_soaring_data message
746 *
747 * @return Debug variable 2
748 */
749static inline float mavlink_msg_fw_soaring_data_get_DebugVar2(const mavlink_message_t* msg)
750{
751 return _MAV_RETURN_float(msg, 96);
752}
753
754/**
755 * @brief Get field ControlMode from fw_soaring_data message
756 *
757 * @return Control Mode [-]
758 */
759static inline uint8_t mavlink_msg_fw_soaring_data_get_ControlMode(const mavlink_message_t* msg)
760{
761 return _MAV_RETURN_uint8_t(msg, 100);
762}
763
764/**
765 * @brief Get field valid from fw_soaring_data message
766 *
767 * @return Data valid [-]
768 */
769static inline uint8_t mavlink_msg_fw_soaring_data_get_valid(const mavlink_message_t* msg)
770{
771 return _MAV_RETURN_uint8_t(msg, 101);
772}
773
774/**
775 * @brief Decode a fw_soaring_data message into a struct
776 *
777 * @param msg The message to decode
778 * @param fw_soaring_data C-struct to decode the message contents into
779 */
780static inline void mavlink_msg_fw_soaring_data_decode(const mavlink_message_t* msg, mavlink_fw_soaring_data_t* fw_soaring_data)
781{
782#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
783 fw_soaring_data->timestamp = mavlink_msg_fw_soaring_data_get_timestamp(msg);
784 fw_soaring_data->timestampModeChanged = mavlink_msg_fw_soaring_data_get_timestampModeChanged(msg);
785 fw_soaring_data->xW = mavlink_msg_fw_soaring_data_get_xW(msg);
786 fw_soaring_data->xR = mavlink_msg_fw_soaring_data_get_xR(msg);
787 fw_soaring_data->xLat = mavlink_msg_fw_soaring_data_get_xLat(msg);
788 fw_soaring_data->xLon = mavlink_msg_fw_soaring_data_get_xLon(msg);
789 fw_soaring_data->VarW = mavlink_msg_fw_soaring_data_get_VarW(msg);
790 fw_soaring_data->VarR = mavlink_msg_fw_soaring_data_get_VarR(msg);
791 fw_soaring_data->VarLat = mavlink_msg_fw_soaring_data_get_VarLat(msg);
792 fw_soaring_data->VarLon = mavlink_msg_fw_soaring_data_get_VarLon(msg);
793 fw_soaring_data->LoiterRadius = mavlink_msg_fw_soaring_data_get_LoiterRadius(msg);
794 fw_soaring_data->LoiterDirection = mavlink_msg_fw_soaring_data_get_LoiterDirection(msg);
795 fw_soaring_data->DistToSoarPoint = mavlink_msg_fw_soaring_data_get_DistToSoarPoint(msg);
796 fw_soaring_data->vSinkExp = mavlink_msg_fw_soaring_data_get_vSinkExp(msg);
797 fw_soaring_data->z1_LocalUpdraftSpeed = mavlink_msg_fw_soaring_data_get_z1_LocalUpdraftSpeed(msg);
798 fw_soaring_data->z2_DeltaRoll = mavlink_msg_fw_soaring_data_get_z2_DeltaRoll(msg);
799 fw_soaring_data->z1_exp = mavlink_msg_fw_soaring_data_get_z1_exp(msg);
800 fw_soaring_data->z2_exp = mavlink_msg_fw_soaring_data_get_z2_exp(msg);
801 fw_soaring_data->ThermalGSNorth = mavlink_msg_fw_soaring_data_get_ThermalGSNorth(msg);
802 fw_soaring_data->ThermalGSEast = mavlink_msg_fw_soaring_data_get_ThermalGSEast(msg);
803 fw_soaring_data->TSE_dot = mavlink_msg_fw_soaring_data_get_TSE_dot(msg);
804 fw_soaring_data->DebugVar1 = mavlink_msg_fw_soaring_data_get_DebugVar1(msg);
805 fw_soaring_data->DebugVar2 = mavlink_msg_fw_soaring_data_get_DebugVar2(msg);
806 fw_soaring_data->ControlMode = mavlink_msg_fw_soaring_data_get_ControlMode(msg);
807 fw_soaring_data->valid = mavlink_msg_fw_soaring_data_get_valid(msg);
808#else
809 uint8_t len = msg->len < MAVLINK_MSG_ID_FW_SOARING_DATA_LEN? msg->len : MAVLINK_MSG_ID_FW_SOARING_DATA_LEN;
810 memset(fw_soaring_data, 0, MAVLINK_MSG_ID_FW_SOARING_DATA_LEN);
811 memcpy(fw_soaring_data, _MAV_PAYLOAD(msg), len);
812#endif
813}
制作者 doxygen 1.11.0