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path: root/src/modules/sdlog2/sdlog2.c
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Diffstat (limited to 'src/modules/sdlog2/sdlog2.c')
-rw-r--r--src/modules/sdlog2/sdlog2.c25
1 files changed, 25 insertions, 0 deletions
diff --git a/src/modules/sdlog2/sdlog2.c b/src/modules/sdlog2/sdlog2.c
index 0b6861d2a..6df677338 100644
--- a/src/modules/sdlog2/sdlog2.c
+++ b/src/modules/sdlog2/sdlog2.c
@@ -941,6 +941,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct vehicle_rates_setpoint_s rates_sp;
struct actuator_outputs_s act_outputs;
struct actuator_controls_s act_controls;
+ struct actuator_controls_s act_controls1;
struct vehicle_local_position_s local_pos;
struct vehicle_local_position_setpoint_s local_pos_sp;
struct vehicle_global_position_s global_pos;
@@ -1022,6 +1023,7 @@ int sdlog2_thread_main(int argc, char *argv[])
int rates_sp_sub;
int act_outputs_sub;
int act_controls_sub;
+ int act_controls_1_sub;
int local_pos_sub;
int local_pos_sp_sub;
int global_pos_sub;
@@ -1055,6 +1057,7 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.rates_sp_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint));
subs.act_outputs_sub = orb_subscribe(ORB_ID_VEHICLE_CONTROLS);
subs.act_controls_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
+ subs.act_controls_1_sub = orb_subscribe(ORB_ID(actuator_controls_1));
subs.local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
subs.local_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_local_position_setpoint));
subs.global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
@@ -1375,6 +1378,18 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.body.log_ATT.gy = buf.att.g_comp[1];
log_msg.body.log_ATT.gz = buf.att.g_comp[2];
LOGBUFFER_WRITE_AND_COUNT(ATT);
+ // secondary attitude
+ log_msg.msg_type = LOG_ATT2_MSG;
+ log_msg.body.log_ATT.roll = buf.att.roll_sec;
+ log_msg.body.log_ATT.pitch = buf.att.pitch_sec;
+ log_msg.body.log_ATT.yaw = buf.att.yaw_sec;
+ log_msg.body.log_ATT.roll_rate = buf.att.rollspeed_sec;
+ log_msg.body.log_ATT.pitch_rate = buf.att.pitchspeed_sec;
+ log_msg.body.log_ATT.yaw_rate = buf.att.yawspeed_sec;
+ log_msg.body.log_ATT.gx = buf.att.g_comp_sec[0];
+ log_msg.body.log_ATT.gy = buf.att.g_comp_sec[1];
+ log_msg.body.log_ATT.gz = buf.att.g_comp_sec[2];
+ LOGBUFFER_WRITE_AND_COUNT(ATT);
}
/* --- ATTITUDE SETPOINT --- */
@@ -1413,6 +1428,16 @@ int sdlog2_thread_main(int argc, char *argv[])
LOGBUFFER_WRITE_AND_COUNT(ATTC);
}
+ /* --- ACTUATOR CONTROL FW VTOL --- */
+ if(copy_if_updated(ORB_ID(actuator_controls_1),subs.act_controls_1_sub,&buf.act_controls)) {
+ log_msg.msg_type = LOG_ATC1_MSG;
+ log_msg.body.log_ATTC.roll = buf.act_controls.control[0];
+ log_msg.body.log_ATTC.pitch = buf.act_controls.control[1];
+ log_msg.body.log_ATTC.yaw = buf.act_controls.control[2];
+ log_msg.body.log_ATTC.thrust = buf.act_controls.control[3];
+ LOGBUFFER_WRITE_AND_COUNT(ATTC);
+ }
+
/* --- LOCAL POSITION --- */
if (copy_if_updated(ORB_ID(vehicle_local_position), subs.local_pos_sub, &buf.local_pos)) {
log_msg.msg_type = LOG_LPOS_MSG;