diff options
Diffstat (limited to 'src/modules/commander/commander.cpp')
| -rw-r--r-- | src/modules/commander/commander.cpp | 6 |
1 files changed, 3 insertions, 3 deletions
diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index dc0594bf2..086f291f6 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -1267,7 +1267,7 @@ int commander_thread_main(int argc, char *argv[]) if (updated) { /* vtol status changed */ orb_copy(ORB_ID(vtol_vehicle_status), vtol_vehicle_status_sub, &vtol_status); - + status.vtol_fw_permanent_stab = vtol_status.fw_permanent_stab; /* Make sure that this is only adjusted if vehicle realy is of type vtol*/ if (status.system_type == VEHICLE_TYPE_VTOL_DUOROTOR || VEHICLE_TYPE_VTOL_QUADROTOR) { status.is_rotary_wing = vtol_status.vtol_in_rw_mode; @@ -2246,8 +2246,8 @@ set_control_mode() case NAVIGATION_STATE_MANUAL: control_mode.flag_control_manual_enabled = true; control_mode.flag_control_auto_enabled = false; - control_mode.flag_control_rates_enabled = status.is_rotary_wing; - control_mode.flag_control_attitude_enabled = status.is_rotary_wing; + control_mode.flag_control_rates_enabled = (status.is_rotary_wing || status.vtol_fw_permanent_stab); + control_mode.flag_control_attitude_enabled = (status.is_rotary_wing || status.vtol_fw_permanent_stab); control_mode.flag_control_altitude_enabled = false; control_mode.flag_control_climb_rate_enabled = false; control_mode.flag_control_position_enabled = false; |