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-rw-r--r--apps/fixedwing_att_control/fixedwing_att_control_main.c2
1 files changed, 1 insertions, 1 deletions
diff --git a/apps/fixedwing_att_control/fixedwing_att_control_main.c b/apps/fixedwing_att_control/fixedwing_att_control_main.c
index c51d06579..cd479d40d 100644
--- a/apps/fixedwing_att_control/fixedwing_att_control_main.c
+++ b/apps/fixedwing_att_control/fixedwing_att_control_main.c
@@ -240,7 +240,7 @@ int fixedwing_att_control_thread_main(int argc, char *argv[])
/* set flaps to zero */
actuators.control[4] = 0.0f;
- } else {
+ } else if (vstatus.state_machine == SYSTEM_STATE_MANUAL) {
if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) {
/* if the RC signal is lost, try to stay level and go slowly back down to ground */