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let vtol attitude control module publish attitude setpoint during transition
Conflicts: src/modules/commander/commander.cpp src/modules/fw_att_control/fw_att_control_main.cpp src/modules/mc_pos_control/mc_pos_control_main.cpp
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@@ -1599,7 +1599,7 @@ int commander_thread_main(int argc, char *argv[])
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orb_copy(ORB_ID(vtol_vehicle_status), vtol_vehicle_status_sub, &vtol_status);
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status.vtol_fw_permanent_stab = vtol_status.fw_permanent_stab;
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/* Make sure that this is only adjusted if vehicle really is of type vtol*/
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/* Make sure that this is only adjusted if vehicle really is of type vtol */
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if (is_vtol(&status)) {
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status.is_rotary_wing = vtol_status.vtol_in_rw_mode;
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status.in_transition_mode = vtol_status.vtol_in_trans_mode;
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