diff options
Diffstat (limited to 'apps/commander/state_machine_helper.c')
| -rw-r--r-- | apps/commander/state_machine_helper.c | 18 |
1 files changed, 9 insertions, 9 deletions
diff --git a/apps/commander/state_machine_helper.c b/apps/commander/state_machine_helper.c index f30fd975b..fdd32ca40 100644 --- a/apps/commander/state_machine_helper.c +++ b/apps/commander/state_machine_helper.c @@ -522,20 +522,20 @@ void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *c current_status->flag_control_manual_enabled = true; /* set behaviour based on airframe */ - if ((current_status.system_type == MAV_TYPE_QUADROTOR) || - (current_status.system_type == MAV_TYPE_HEXAROTOR) || - (current_status.system_type == MAV_TYPE_OCTOROTOR)) { + if ((current_status->system_type == VEHICLE_TYPE_QUADROTOR) || + (current_status->system_type == VEHICLE_TYPE_HEXAROTOR) || + (current_status->system_type == VEHICLE_TYPE_OCTOROTOR)) { /* assuming a rotary wing, set to SAS */ - current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - current_status.flag_control_attitude_enabled = true; - current_status.flag_control_rates_enabled = true; + current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; + current_status->flag_control_attitude_enabled = true; + current_status->flag_control_rates_enabled = true; } else { /* assuming a fixed wing, set to direct pass-through */ - current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT; - current_status.flag_control_attitude_enabled = false; - current_status.flag_control_rates_enabled = false; + current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT; + current_status->flag_control_attitude_enabled = false; + current_status->flag_control_rates_enabled = false; } if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd); |