Merge remote-tracking branch 'upstream/master' into PR_RCLossDur2

6 files changed, 319 insertions, 200 deletions

diff --git a/src/modules/commander/accelerometer_calibration.cpp b/src/modules/commander/accelerometer_calibration.cpp
index 7a4e7a766..0cb41489f 100644
--- a/src/modules/commander/accelerometer_calibration.cpp
+++ b/src/modules/commander/accelerometer_calibration.cpp
@@ -83,7 +83,7 @@
  *     | accel_T[1][i] |
  *     [ accel_T[2][i] ]
  *
- * b = [ accel_corr_ref[0][i] ]	// One measurement per axis is enough
+ * b = [ accel_corr_ref[0][i] ]	// One measurement per side is enough
  *     | accel_corr_ref[2][i] |
  *     [ accel_corr_ref[4][i] ]
  *
@@ -162,6 +162,11 @@ int do_accel_calibration(int mavlink_fd)
 
 	mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
 
+	mavlink_log_info(mavlink_fd, "You need to put the system on all six sides");
+	sleep(3);
+	mavlink_log_info(mavlink_fd, "Follow the instructions on the screen");
+	sleep(5);
+
 	struct accel_scale accel_scale = {
 		0.0f,
 		1.0f,
@@ -258,7 +263,7 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
 	const int samples_num = 2500;
 	float accel_ref[6][3];
 	bool data_collected[6] = { false, false, false, false, false, false };
-	const char *orientation_strs[6] = { "x+", "x-", "y+", "y-", "z+", "z-" };
+	const char *orientation_strs[6] = { "front", "back", "left", "right", "top", "bottom" };
 
 	int sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
 
@@ -287,29 +292,37 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
 			break;
 		}
 
-		mavlink_log_info(mavlink_fd, "directions left: %s%s%s%s%s%s",
-				 (!data_collected[0]) ? "x+ " : "",
-				 (!data_collected[1]) ? "x- " : "",
-				 (!data_collected[2]) ? "y+ " : "",
-				 (!data_collected[3]) ? "y- " : "",
-				 (!data_collected[4]) ? "z+ " : "",
-				 (!data_collected[5]) ? "z- " : "");
+		/* inform user which axes are still needed */
+		mavlink_log_info(mavlink_fd, "pending: %s%s%s%s%s%s",
+				 (!data_collected[0]) ? "front " : "",
+				 (!data_collected[1]) ? "back " : "",
+				 (!data_collected[2]) ? "left " : "",
+				 (!data_collected[3]) ? "right " : "",
+				 (!data_collected[4]) ? "up " : "",
+				 (!data_collected[5]) ? "down " : "");
+
+		/* allow user enough time to read the message */
+		sleep(3);
 
 		int orient = detect_orientation(mavlink_fd, sensor_combined_sub);
 
 		if (orient < 0) {
-			res = ERROR;
-			break;
+			mavlink_log_info(mavlink_fd, "invalid motion, hold still...");
+			sleep(3);
+			continue;
 		}
 
+		/* inform user about already handled side */
 		if (data_collected[orient]) {
-			mavlink_log_info(mavlink_fd, "%s done, rotate to a different axis", orientation_strs[orient]);
+			mavlink_log_info(mavlink_fd, "%s side done, rotate to a different side", orientation_strs[orient]);
+			sleep(4);
 			continue;
 		}
 
-		mavlink_log_info(mavlink_fd, "accel measurement started: %s axis", orientation_strs[orient]);
+		mavlink_log_info(mavlink_fd, "Hold still, starting to measure %s side", orientation_strs[orient]);
+		sleep(1);
 		read_accelerometer_avg(sensor_combined_sub, &(accel_ref[orient][0]), samples_num);
-		mavlink_log_info(mavlink_fd, "result for %s axis: [ %.2f %.2f %.2f ]", orientation_strs[orient],
+		mavlink_log_info(mavlink_fd, "result for %s side: [ %.2f %.2f %.2f ]", orientation_strs[orient],
 				 (double)accel_ref[orient][0],
 				 (double)accel_ref[orient][1],
 				 (double)accel_ref[orient][2]);
@@ -400,7 +413,7 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined)
 				/* is still now */
 				if (t_still == 0) {
 					/* first time */
-					mavlink_log_info(mavlink_fd, "detected rest position, waiting...");
+					mavlink_log_info(mavlink_fd, "detected rest position, hold still...");
 					t_still = t;
 					t_timeout = t + timeout;
 
@@ -418,6 +431,7 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined)
 				/* not still, reset still start time */
 				if (t_still != 0) {
 					mavlink_log_info(mavlink_fd, "detected motion, hold still...");
+					sleep(3);
 					t_still = 0;
 				}
 			}
diff --git a/src/modules/commander/airspeed_calibration.cpp b/src/modules/commander/airspeed_calibration.cpp
index 339b11bbe..cae1d7684 100644
--- a/src/modules/commander/airspeed_calibration.cpp
+++ b/src/modules/commander/airspeed_calibration.cpp
@@ -61,6 +61,15 @@ static const int ERROR = -1;
 
 static const char *sensor_name = "dpress";
 
+#define HUMAN_ASPD_CAL_FAILED_MSG "Calibration failed, see http://px4.io/help/aspd"
+
+static void feedback_calibration_failed(int mavlink_fd)
+{
+	sleep(5);
+	mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+	mavlink_log_critical(mavlink_fd, HUMAN_ASPD_CAL_FAILED_MSG);
+}
+
 int do_airspeed_calibration(int mavlink_fd)
 {
 	/* give directions */
@@ -99,7 +108,7 @@ int do_airspeed_calibration(int mavlink_fd)
 		float analog_scaling = 0.0f;
 		param_get(param_find("SENS_DPRES_ANSC"), &(analog_scaling));
 		if (fabsf(analog_scaling) < 0.1f) {
-			mavlink_log_critical(mavlink_fd, "If analog sens, retry with [SENS_DPRES_ANSC=1000]");
+			mavlink_log_critical(mavlink_fd, "No airspeed sensor, see http://px4.io/help/aspd");
 			close(diff_pres_sub);
 			return ERROR;
 		}
@@ -138,7 +147,7 @@ int do_airspeed_calibration(int mavlink_fd)
 
 		} else if (poll_ret == 0) {
 			/* any poll failure for 1s is a reason to abort */
-			mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+			feedback_calibration_failed(mavlink_fd);
 			close(diff_pres_sub);
 			return ERROR;
 		}
@@ -175,7 +184,7 @@ int do_airspeed_calibration(int mavlink_fd)
 		}
 
 	} else {
-		mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+		feedback_calibration_failed(mavlink_fd);
 		close(diff_pres_sub);
 		return ERROR;
 	}
@@ -207,7 +216,7 @@ int do_airspeed_calibration(int mavlink_fd)
 
 			if (fabsf(diff_pres.differential_pressure_raw_pa) < 50.0f) {
 				if (calibration_counter % 500 == 0) {
-					mavlink_log_info(mavlink_fd, "Create airflow! (%d, wanted: 50 Pa)",
+					mavlink_log_info(mavlink_fd, "Create air pressure! (got %d, wanted: 50 Pa)",
 						(int)diff_pres.differential_pressure_raw_pa);
 				}
 				continue;
@@ -215,9 +224,9 @@ int do_airspeed_calibration(int mavlink_fd)
 
 			/* do not allow negative values */
 			if (diff_pres.differential_pressure_raw_pa < 0.0f) {
-				mavlink_log_critical(mavlink_fd, "Swap static and dynamic ports!");
 				mavlink_log_info(mavlink_fd, "ERROR: Negative pressure difference detected! (%d Pa)",
 						(int)diff_pres.differential_pressure_raw_pa);
+				mavlink_log_critical(mavlink_fd, "Swap static and dynamic ports!");
 				close(diff_pres_sub);
 
 				/* the user setup is wrong, wipe the calibration to force a proper re-calibration */
@@ -235,7 +244,7 @@ int do_airspeed_calibration(int mavlink_fd)
 
 				close(diff_pres_sub);
 
-				mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+				feedback_calibration_failed(mavlink_fd);
 				return ERROR;
 			} else {
 				mavlink_log_info(mavlink_fd, "Positive pressure: OK (%d Pa)",
@@ -245,14 +254,14 @@ int do_airspeed_calibration(int mavlink_fd)
 
 		} else if (poll_ret == 0) {
 			/* any poll failure for 1s is a reason to abort */
-			mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+			feedback_calibration_failed(mavlink_fd);
 			close(diff_pres_sub);
 			return ERROR;
 		}
 	}
 
 	if (calibration_counter == maxcount) {
-		mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
+		feedback_calibration_failed(mavlink_fd);
 		close(diff_pres_sub);
 		return ERROR;
 	}
diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp
index 1f13aaec4..deb048566 100644
--- a/src/modules/commander/commander.cpp
+++ b/src/modules/commander/commander.cpp
@@ -207,7 +207,9 @@ void usage(const char *reason);
 /**
  * React to commands that are sent e.g. from the mavlink module.
  */
-bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub);
+bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd,
+		    struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos,
+		    orb_advert_t *home_pub);
 
 /**
  * Mainloop of commander.
@@ -218,8 +220,6 @@ void control_status_leds(vehicle_status_s *status, const actuator_armed_s *actua
 
 void check_valid(hrt_abstime timestamp, hrt_abstime timeout, bool valid_in, bool *valid_out, bool *changed);
 
-void check_mode_switches(struct manual_control_setpoint_s *sp_man, struct vehicle_status_s *status);
-
 transition_result_t set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoint_s *sp_man);
 
 void set_control_mode();
@@ -230,7 +230,8 @@ void print_reject_arm(const char *msg);
 
 void print_status();
 
-transition_result_t check_navigation_state_machine(struct vehicle_status_s *status, struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos);
+transition_result_t check_navigation_state_machine(struct vehicle_status_s *status,
+		struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos);
 
 transition_result_t arm_disarm(bool arm, const int mavlink_fd, const char *armedBy);
 
@@ -260,7 +261,7 @@ int commander_main(int argc, char *argv[])
 		daemon_task = task_spawn_cmd("commander",
 					     SCHED_DEFAULT,
 					     SCHED_PRIORITY_MAX - 40,
-					     2950,
+					     3200,
 					     commander_thread_main,
 					     (argv) ? (const char **)&argv[2] : (const char **)NULL);
 
@@ -393,7 +394,8 @@ transition_result_t arm_disarm(bool arm, const int mavlink_fd_local, const char
 
 	// Transition the armed state. By passing mavlink_fd to arming_state_transition it will
 	// output appropriate error messages if the state cannot transition.
-	arming_res = arming_state_transition(&status, &safety, arm ? ARMING_STATE_ARMED : ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */, mavlink_fd_local);
+	arming_res = arming_state_transition(&status, &safety, arm ? ARMING_STATE_ARMED : ARMING_STATE_STANDBY, &armed,
+					     true /* fRunPreArmChecks */, mavlink_fd_local);
 
 	if (arming_res == TRANSITION_CHANGED && mavlink_fd) {
 		mavlink_log_info(mavlink_fd_local, "[cmd] %s by %s", arm ? "ARMED" : "DISARMED", armedBy);
@@ -406,11 +408,12 @@ transition_result_t arm_disarm(bool arm, const int mavlink_fd_local, const char
 }
 
 bool handle_command(struct vehicle_status_s *status_local, const struct safety_s *safety_local,
-	struct vehicle_command_s *cmd, struct actuator_armed_s *armed_local,
-	struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub)
+		    struct vehicle_command_s *cmd, struct actuator_armed_s *armed_local,
+		    struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub)
 {
 	/* only handle commands that are meant to be handled by this system and component */
-	if (cmd->target_system != status_local->system_id || ((cmd->target_component != status_local->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components
+	if (cmd->target_system != status_local->system_id || ((cmd->target_component != status_local->component_id)
+			&& (cmd->target_component != 0))) { // component_id 0: valid for all components
 		return false;
 	}
 
@@ -537,13 +540,13 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
 
 			} else {
 				mavlink_log_critical(mavlink_fd, "REJ CMD: %.1f %.1f %.1f %.1f %.1f %.1f %.1f %.1f",
-					(double)cmd->param1,
-					(double)cmd->param2,
-					(double)cmd->param3,
-					(double)cmd->param4,
-					(double)cmd->param5,
-					(double)cmd->param6,
-					(double)cmd->param7);
+						     (double)cmd->param1,
+						     (double)cmd->param2,
+						     (double)cmd->param3,
+						     (double)cmd->param4,
+						     (double)cmd->param5,
+						     (double)cmd->param6,
+						     (double)cmd->param7);
 			}
 		}
 		break;
@@ -554,35 +557,43 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
 				//XXX update state machine?
 				armed_local->force_failsafe = true;
 				warnx("forcing failsafe (termination)");
+
 			} else {
 				armed_local->force_failsafe = false;
 				warnx("disabling failsafe (termination)");
 			}
+
 			/* param2 is currently used for other failsafe modes */
 			status_local->engine_failure_cmd = false;
 			status_local->data_link_lost_cmd = false;
 			status_local->gps_failure_cmd = false;
 			status_local->rc_signal_lost_cmd = false;
+
 			if ((int)cmd->param2 <= 0) {
 				/* reset all commanded failure modes */
 				warnx("reset all non-flighttermination failsafe commands");
+
 			} else if ((int)cmd->param2 == 1) {
 				/* trigger engine failure mode */
 				status_local->engine_failure_cmd = true;
 				warnx("engine failure mode commanded");
+
 			} else if ((int)cmd->param2 == 2) {
 				/* trigger data link loss mode */
 				status_local->data_link_lost_cmd = true;
 				warnx("data link loss mode commanded");
+
 			} else if ((int)cmd->param2 == 3) {
 				/* trigger gps loss mode */
 				status_local->gps_failure_cmd = true;
 				warnx("gps loss mode commanded");
+
 			} else if ((int)cmd->param2 == 4) {
 				/* trigger rc loss mode */
 				status_local->rc_signal_lost_cmd = true;
 				warnx("rc loss mode commanded");
 			}
+
 			cmd_result = VEHICLE_CMD_RESULT_ACCEPTED;
 		}
 		break;
@@ -633,21 +644,27 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
 			}
 		}
 		break;
+
 	case VEHICLE_CMD_NAV_GUIDED_ENABLE: {
 			transition_result_t res = TRANSITION_DENIED;
 			static main_state_t main_state_pre_offboard = MAIN_STATE_MANUAL;
+
 			if (status_local->main_state != MAIN_STATE_OFFBOARD) {
 				main_state_pre_offboard = status_local->main_state;
 			}
+
 			if (cmd->param1 > 0.5f) {
 				res = main_state_transition(status_local, MAIN_STATE_OFFBOARD);
+
 				if (res == TRANSITION_DENIED) {
 					print_reject_mode(status_local, "OFFBOARD");
 					status_local->offboard_control_set_by_command = false;
+
 				} else {
 					/* Set flag that offboard was set via command, main state is not overridden by rc */
 					status_local->offboard_control_set_by_command = true;
 				}
+
 			} else {
 				/* If the mavlink command is used to enable or disable offboard control:
 				 * switch back to previous mode when disabling */
@@ -656,6 +673,7 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
 			}
 		}
 		break;
+
 	case VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
 	case VEHICLE_CMD_PREFLIGHT_CALIBRATION:
 	case VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS:
@@ -740,7 +758,10 @@ int commander_thread_main(int argc, char *argv[])
 	nav_states_str[NAVIGATION_STATE_AUTO_MISSION]		= "AUTO_MISSION";
 	nav_states_str[NAVIGATION_STATE_AUTO_LOITER]		= "AUTO_LOITER";
 	nav_states_str[NAVIGATION_STATE_AUTO_RTL]		= "AUTO_RTL";
+	nav_states_str[NAVIGATION_STATE_AUTO_RCRECOVER]		= "AUTO_RCRECOVER";
 	nav_states_str[NAVIGATION_STATE_AUTO_RTGS]		= "AUTO_RTGS";
+	nav_states_str[NAVIGATION_STATE_AUTO_LANDENGFAIL]	= "AUTO_LANDENGFAIL";
+	nav_states_str[NAVIGATION_STATE_AUTO_LANDGPSFAIL]	= "AUTO_LANDGPSFAIL";
 	nav_states_str[NAVIGATION_STATE_ACRO]			= "ACRO";
 	nav_states_str[NAVIGATION_STATE_LAND]			= "LAND";
 	nav_states_str[NAVIGATION_STATE_DESCEND]		= "DESCEND";
@@ -802,6 +823,7 @@ int commander_thread_main(int argc, char *argv[])
 
 	/* publish initial state */
 	status_pub = orb_advertise(ORB_ID(vehicle_status), &status);
+
 	if (status_pub < 0) {
 		warnx("ERROR: orb_advertise for topic vehicle_status failed (uorb app running?).\n");
 		warnx("exiting.");
@@ -827,11 +849,14 @@ int commander_thread_main(int argc, char *argv[])
 	/* init mission state, do it here to allow navigator to use stored mission even if mavlink failed to start */
 	orb_advert_t mission_pub = -1;
 	mission_s mission;
+
 	if (dm_read(DM_KEY_MISSION_STATE, 0, &mission, sizeof(mission_s)) == sizeof(mission_s)) {
 		if (mission.dataman_id >= 0 && mission.dataman_id <= 1) {
-			warnx("loaded mission state: dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count, mission.current_seq);
+			warnx("loaded mission state: dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count,
+			      mission.current_seq);
 			mavlink_log_info(mavlink_fd, "[cmd] dataman_id=%d, count=%u, current=%d",
-												mission.dataman_id, mission.count, mission.current_seq);
+					 mission.dataman_id, mission.count, mission.current_seq);
+
 		} else {
 			const char *missionfail = "reading mission state failed";
 			warnx("%s", missionfail);
@@ -1097,6 +1122,7 @@ int commander_thread_main(int argc, char *argv[])
 				status.offboard_control_signal_lost = false;
 				status_changed = true;
 			}
+
 		} else {
 			if (!status.offboard_control_signal_lost) {
 				status.offboard_control_signal_lost = true;
@@ -1115,9 +1141,9 @@ int commander_thread_main(int argc, char *argv[])
 
 				/* perform system checks when new telemetry link connected */
 				if (mavlink_fd &&
-					telemetry_last_heartbeat[i] == 0 &&
-					telemetry.heartbeat_time > 0 &&
-					hrt_elapsed_time(&telemetry.heartbeat_time) < datalink_loss_timeout * 1e6) {
+				    telemetry_last_heartbeat[i] == 0 &&
+				    telemetry.heartbeat_time > 0 &&
+				    hrt_elapsed_time(&telemetry.heartbeat_time) < datalink_loss_timeout * 1e6) {
 
 					(void)rc_calibration_check(mavlink_fd);
 				}
@@ -1130,6 +1156,7 @@ int commander_thread_main(int argc, char *argv[])
 
 		if (updated) {
 			orb_copy(ORB_ID(sensor_combined), sensor_sub, &sensors);
+
 			/* Check if the barometer is healthy and issue a warning in the GCS if not so.
 			 * Because the barometer is used for calculating AMSL altitude which is used to ensure
 			 * vertical separation from other airtraffic the operator has to know when the
@@ -1142,6 +1169,7 @@ int commander_thread_main(int argc, char *argv[])
 					status_changed = true;
 					mavlink_log_critical(mavlink_fd, "baro healthy");
 				}
+
 			} else {
 				if (!status.barometer_failure) {
 					status.barometer_failure = true;
@@ -1164,10 +1192,11 @@ int commander_thread_main(int argc, char *argv[])
 
 			if (hrt_elapsed_time(&system_power.timestamp) < 200000) {
 				if (system_power.servo_valid &&
-					!system_power.brick_valid &&
-					!system_power.usb_connected) {
+				    !system_power.brick_valid &&
+				    !system_power.usb_connected) {
 					/* flying only on servo rail, this is unsafe */
 					status.condition_power_input_valid = false;
+
 				} else {
 					status.condition_power_input_valid = true;
 				}
@@ -1187,9 +1216,11 @@ int commander_thread_main(int argc, char *argv[])
 
 			/* disarm if safety is now on and still armed */
 			if (status.hil_state == HIL_STATE_OFF && safety.safety_switch_available && !safety.safety_off && armed.armed) {
-				arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
+				arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY :
+								   ARMING_STATE_STANDBY_ERROR);
 
-				if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */, mavlink_fd)) {
+				if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed,
+						true /* fRunPreArmChecks */, mavlink_fd)) {
 					mavlink_log_info(mavlink_fd, "DISARMED by safety switch");
 					arming_state_changed = true;
 				}
@@ -1233,7 +1264,8 @@ int commander_thread_main(int argc, char *argv[])
 			}
 		}
 
-		check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_good, &(status.condition_global_position_valid), &status_changed);
+		check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_good, &(status.condition_global_position_valid),
+			    &status_changed);
 
 		/* update home position */
 		if (!status.condition_home_position_valid && status.condition_global_position_valid && !armed.armed &&
@@ -1283,8 +1315,11 @@ int commander_thread_main(int argc, char *argv[])
 				local_eph_good = false;
 			}
 		}
-		check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid && local_eph_good, &(status.condition_local_position_valid), &status_changed);
-		check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid, &(status.condition_local_altitude_valid), &status_changed);
+
+		check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid
+			    && local_eph_good, &(status.condition_local_position_valid), &status_changed);
+		check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid,
+			    &(status.condition_local_altitude_valid), &status_changed);
 
 		if (status.condition_local_altitude_valid) {
 			if (status.condition_landed != local_position.landed) {
@@ -1315,7 +1350,8 @@ int commander_thread_main(int argc, char *argv[])
 
 				/* get throttle (if armed), as we only care about energy negative throttle also counts */
 				float throttle = (armed.armed) ? fabsf(actuator_controls.control[3]) : 0.0f;
-				status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah, throttle);
+				status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah,
+							   throttle);
 			}
 		}
 
@@ -1372,8 +1408,8 @@ int commander_thread_main(int argc, char *argv[])
 			last_idle_time = system_load.tasks[0].total_runtime;
 
 			/* check if board is connected via USB */
-			//struct stat statbuf;
-			//on_usb_power = (stat("/dev/ttyACM0", &statbuf) == 0);
+			struct stat statbuf;
+			on_usb_power = (stat("/dev/ttyACM0", &statbuf) == 0);
 		}
 
 		/* if battery voltage is getting lower, warn using buzzer, etc. */
@@ -1383,26 +1419,30 @@ int commander_thread_main(int argc, char *argv[])
 			status.battery_warning = VEHICLE_BATTERY_WARNING_LOW;
 			status_changed = true;
 
-		} else if (status.condition_battery_voltage_valid && status.battery_remaining < 0.09f && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) {
+		} else if (!on_usb_power && status.condition_battery_voltage_valid && status.battery_remaining < 0.09f
+			   && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) {
 			/* critical battery voltage, this is rather an emergency, change state machine */
 			critical_battery_voltage_actions_done = true;
 			mavlink_log_emergency(mavlink_fd, "CRITICAL BATTERY, LAND IMMEDIATELY");
 			status.battery_warning = VEHICLE_BATTERY_WARNING_CRITICAL;
 
 			if (armed.armed) {
-				arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed, true /* fRunPreArmChecks */, mavlink_fd);
+				arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed, true /* fRunPreArmChecks */,
+								     mavlink_fd);
 
 				if (arming_ret == TRANSITION_CHANGED) {
 					arming_state_changed = true;
 				}
 
 			} else {
-				arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed, true /* fRunPreArmChecks */, mavlink_fd);
+				arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed, true /* fRunPreArmChecks */,
+								     mavlink_fd);
 
 				if (arming_ret == TRANSITION_CHANGED) {
 					arming_state_changed = true;
 				}
 			}
+
 			status_changed = true;
 		}
 
@@ -1411,7 +1451,8 @@ int commander_thread_main(int argc, char *argv[])
 		/* If in INIT state, try to proceed to STANDBY state */
 		if (status.arming_state == ARMING_STATE_INIT && low_prio_task == LOW_PRIO_TASK_NONE) {
 			/* TODO: check for sensors */
-			arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */, mavlink_fd);
+			arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */,
+							     mavlink_fd);
 
 			if (arming_ret == TRANSITION_CHANGED) {
 				arming_state_changed = true;
@@ -1439,23 +1480,25 @@ int commander_thread_main(int argc, char *argv[])
 
 		/* Initialize map projection if gps is valid */
 		if (!map_projection_global_initialized()
-				&& (gps_position.eph < eph_threshold)
-				&& (gps_position.epv < epv_threshold)
-				&& hrt_elapsed_time((hrt_abstime*)&gps_position.timestamp_position) < 1e6) {
+		    && (gps_position.eph < eph_threshold)
+		    && (gps_position.epv < epv_threshold)
+		    && hrt_elapsed_time((hrt_abstime *)&gps_position.timestamp_position) < 1e6) {
 			/* set reference for global coordinates <--> local coordiantes conversion and map_projection */
-			globallocalconverter_init((double)gps_position.lat * 1.0e-7, (double)gps_position.lon * 1.0e-7, (float)gps_position.alt * 1.0e-3f, hrt_absolute_time());
+			globallocalconverter_init((double)gps_position.lat * 1.0e-7, (double)gps_position.lon * 1.0e-7,
+						  (float)gps_position.alt * 1.0e-3f, hrt_absolute_time());
 		}
 
 		/* check if GPS fix is ok */
 		if (status.circuit_breaker_engaged_gpsfailure_check ||
-				(gps_position.fix_type >= 3 &&
-				hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT)) {
+		    (gps_position.fix_type >= 3 &&
+		     hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT)) {
 			/* handle the case where gps was regained */
 			if (status.gps_failure) {
 				status.gps_failure = false;
 				status_changed = true;
 				mavlink_log_critical(mavlink_fd, "gps regained");
 			}
+
 		} else {
 			if (!status.gps_failure) {
 				status.gps_failure = true;
@@ -1477,12 +1520,14 @@ int commander_thread_main(int argc, char *argv[])
 				armed.force_failsafe = true;
 				status_changed = true;
 				static bool flight_termination_printed = false;
+
 				if (!flight_termination_printed) {
 					warnx("Flight termination because of navigator request or geofence");
 					mavlink_log_critical(mavlink_fd, "GF violation: flight termination");
 					flight_termination_printed = true;
 				}
-				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
+
+				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
 					mavlink_log_critical(mavlink_fd, "GF violation: flight termination");
 				}
 			} // no reset is done here on purpose, on geofence violation we want to stay in flighttermination
@@ -1490,7 +1535,7 @@ int commander_thread_main(int argc, char *argv[])
 
 		/* RC input check */
 		if (!status.rc_input_blocked && sp_man.timestamp != 0 &&
-				hrt_absolute_time() < sp_man.timestamp + (uint64_t)(rc_loss_timeout * 1e6f)) {
+		    hrt_absolute_time() < sp_man.timestamp + (uint64_t)(rc_loss_timeout * 1e6f)) {
 			/* handle the case where RC signal was regained */
 			if (!status.rc_signal_found_once) {
 				status.rc_signal_found_once = true;
@@ -1515,11 +1560,15 @@ int commander_thread_main(int argc, char *argv[])
 
 				if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) {
 					/* disarm to STANDBY if ARMED or to STANDBY_ERROR if ARMED_ERROR */
-					arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
-					arming_ret = arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */, mavlink_fd);
+					arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY :
+									   ARMING_STATE_STANDBY_ERROR);
+					arming_ret = arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */,
+									     mavlink_fd);
+
 					if (arming_ret == TRANSITION_CHANGED) {
 						arming_state_changed = true;
 					}
+
 					stick_off_counter = 0;
 
 				} else {
@@ -1541,8 +1590,11 @@ int commander_thread_main(int argc, char *argv[])
 					 */
 					if (status.main_state != MAIN_STATE_MANUAL) {
 						print_reject_arm("NOT ARMING: Switch to MANUAL mode first.");
+
 					} else {
-						arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, true /* fRunPreArmChecks */, mavlink_fd);
+						arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, true /* fRunPreArmChecks */,
+										     mavlink_fd);
+
 						if (arming_ret == TRANSITION_CHANGED) {
 							arming_state_changed = true;
 						}
@@ -1565,6 +1617,7 @@ int commander_thread_main(int argc, char *argv[])
 				} else {
 					mavlink_log_info(mavlink_fd, "DISARMED by RC");
 				}
+
 				arming_state_changed = true;
 
 			} else if (arming_ret == TRANSITION_DENIED) {
@@ -1601,18 +1654,20 @@ int commander_thread_main(int argc, char *argv[])
 
 		/* data links check */
 		bool have_link = false;
+
 		for (int i = 0; i < TELEMETRY_STATUS_ORB_ID_NUM; i++) {
 			if (telemetry_last_heartbeat[i] != 0 &&
-					hrt_elapsed_time(&telemetry_last_heartbeat[i]) < datalink_loss_timeout * 1e6) {
+			    hrt_elapsed_time(&telemetry_last_heartbeat[i]) < datalink_loss_timeout * 1e6) {
 				/* handle the case where data link was regained,
 				 * accept datalink as healthy only after datalink_regain_timeout seconds
 				 * */
 				if (telemetry_lost[i] &&
-					hrt_elapsed_time(&telemetry_last_dl_loss[i]) > datalink_regain_timeout * 1e6) {
+				    hrt_elapsed_time(&telemetry_last_dl_loss[i]) > datalink_regain_timeout * 1e6) {
 
 					mavlink_log_critical(mavlink_fd, "data link %i regained", i);
 					telemetry_lost[i] = false;
 					have_link = true;
+
 				} else if (!telemetry_lost[i]) {
 					/* telemetry was healthy also in last iteration
 					 * we don't have to check a timeout */
@@ -1621,6 +1676,7 @@ int commander_thread_main(int argc, char *argv[])
 
 			} else {
 				telemetry_last_dl_loss[i]  = hrt_absolute_time();
+
 				if (!telemetry_lost[i]) {
 					mavlink_log_critical(mavlink_fd, "data link %i lost", i);
 					telemetry_lost[i] = true;
@@ -1648,24 +1704,26 @@ int commander_thread_main(int argc, char *argv[])
 		 * only for fixed wing for now
 		 */
 		if (!status.circuit_breaker_engaged_enginefailure_check &&
-				status.is_rotary_wing == false &&
-				armed.armed &&
-				((actuator_controls.control[3] > ef_throttle_thres &&
-				battery.current_a/actuator_controls.control[3] <
-				ef_current2throttle_thres) ||
-				 (status.engine_failure))) {
+		    status.is_rotary_wing == false &&
+		    armed.armed &&
+		    ((actuator_controls.control[3] > ef_throttle_thres &&
+		      battery.current_a / actuator_controls.control[3] <
+		      ef_current2throttle_thres) ||
+		     (status.engine_failure))) {
 			/* potential failure, measure time */
 			if (timestamp_engine_healthy > 0 &&
-					hrt_elapsed_time(&timestamp_engine_healthy) >
-					ef_time_thres * 1e6 &&
-					!status.engine_failure) {
-					status.engine_failure = true;
-					status_changed = true;
-					mavlink_log_critical(mavlink_fd, "Engine Failure");
+			    hrt_elapsed_time(&timestamp_engine_healthy) >
+			    ef_time_thres * 1e6 &&
+			    !status.engine_failure) {
+				status.engine_failure = true;
+				status_changed = true;
+				mavlink_log_critical(mavlink_fd, "Engine Failure");
 			}
+
 		} else {
 			/* no failure reset flag */
 			timestamp_engine_healthy = hrt_absolute_time();
+
 			if (status.engine_failure) {
 				status.engine_failure = false;
 				status_changed = true;
@@ -1692,20 +1750,22 @@ int commander_thread_main(int argc, char *argv[])
 			 * If  we are not in a manual (RC stick controlled mode)
 			 * and both failed we want to terminate the flight */
 			if (status.main_state != MAIN_STATE_MANUAL &&
-					status.main_state != MAIN_STATE_ACRO &&
-					status.main_state != MAIN_STATE_ALTCTL &&
-					status.main_state != MAIN_STATE_POSCTL &&
-					((status.data_link_lost && status.gps_failure) ||
-					(status.data_link_lost_cmd && status.gps_failure_cmd))) {
+			    status.main_state != MAIN_STATE_ACRO &&
+			    status.main_state != MAIN_STATE_ALTCTL &&
+			    status.main_state != MAIN_STATE_POSCTL &&
+			    ((status.data_link_lost && status.gps_failure) ||
+			     (status.data_link_lost_cmd && status.gps_failure_cmd))) {
 				armed.force_failsafe = true;
 				status_changed = true;
 				static bool flight_termination_printed = false;
+
 				if (!flight_termination_printed) {
 					warnx("Flight termination because of data link loss && gps failure");
 					mavlink_log_critical(mavlink_fd, "DL and GPS lost: flight termination");
 					flight_termination_printed = true;
 				}
-				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
+
+				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
 					mavlink_log_critical(mavlink_fd, "DL and GPS lost: flight termination");
 				}
 			}
@@ -1714,19 +1774,21 @@ int commander_thread_main(int argc, char *argv[])
 			 * If we are in manual (controlled with RC):
 			 * if both failed we want to terminate the flight */
 			if ((status.main_state == MAIN_STATE_ACRO ||
-					status.main_state == MAIN_STATE_MANUAL ||
-					status.main_state == MAIN_STATE_ALTCTL ||
-					status.main_state == MAIN_STATE_POSCTL) &&
-					((status.rc_signal_lost && status.gps_failure) ||
-					(status.rc_signal_lost_cmd && status.gps_failure_cmd))) {
+			     status.main_state == MAIN_STATE_MANUAL ||
+			     status.main_state == MAIN_STATE_ALTCTL ||
+			     status.main_state == MAIN_STATE_POSCTL) &&
+			    ((status.rc_signal_lost && status.gps_failure) ||
+			     (status.rc_signal_lost_cmd && status.gps_failure_cmd))) {
 				armed.force_failsafe = true;
 				status_changed = true;
 				static bool flight_termination_printed = false;
+
 				if (!flight_termination_printed) {
 					warnx("Flight termination because of RC signal loss && gps failure");
 					flight_termination_printed = true;
 				}
-				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
+
+				if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
 					mavlink_log_critical(mavlink_fd, "RC and GPS lost: flight termination");
 				}
 			}
@@ -1767,6 +1829,7 @@ int commander_thread_main(int argc, char *argv[])
 				/* mark home position as set */
 				status.condition_home_position_valid = true;
 			}
+
 			arming_state_changed = false;
 		}
 
@@ -1787,7 +1850,11 @@ int commander_thread_main(int argc, char *argv[])
 
 		if (status.failsafe != failsafe_old) {
 			status_changed = true;
-			mavlink_log_info(mavlink_fd, "[cmd] failsafe state: %i", status.failsafe);
+			if (status.failsafe) {
+				mavlink_log_critical(mavlink_fd, "failsafe mode on");
+			} else {
+				mavlink_log_critical(mavlink_fd, "failsafe mode off");
+			}
 			failsafe_old = status.failsafe;
 		}
 
@@ -1811,7 +1878,8 @@ int commander_thread_main(int argc, char *argv[])
 		}
 
 		/* play arming and battery warning tunes */
-		if (!arm_tune_played && armed.armed && (!safety.safety_switch_available || (safety.safety_switch_available && safety.safety_off))) {
+		if (!arm_tune_played && armed.armed && (!safety.safety_switch_available || (safety.safety_switch_available
+							&& safety.safety_off))) {
 			/* play tune when armed */
 			set_tune(TONE_ARMING_WARNING_TUNE);
 			arm_tune_played = true;
@@ -1989,6 +2057,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 	/* offboard switch overrides main switch */
 	if (sp_man->offboard_switch == SWITCH_POS_ON) {
 		res = main_state_transition(status_local, MAIN_STATE_OFFBOARD);
+
 		if (res == TRANSITION_DENIED) {
 			print_reject_mode(status_local, "OFFBOARD");
 
@@ -2010,6 +2079,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 		} else {
 			res = main_state_transition(status_local, MAIN_STATE_MANUAL);
 		}
+
 		// TRANSITION_DENIED is not possible here
 		break;
 
@@ -2024,7 +2094,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 			print_reject_mode(status_local, "POSCTL");
 		}
 
-        // fallback to ALTCTL
+		// fallback to ALTCTL
 		res = main_state_transition(status_local, MAIN_STATE_ALTCTL);
 
 		if (res != TRANSITION_DENIED) {
@@ -2048,14 +2118,14 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 				break;	// changed successfully or already in this state
 			}
 
-            print_reject_mode(status_local, "AUTO_RTL");
+			print_reject_mode(status_local, "AUTO_RTL");
 
-            // fallback to LOITER if home position not set
-            res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
+			// fallback to LOITER if home position not set
+			res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
 
-            if (res != TRANSITION_DENIED) {
-                break;  // changed successfully or already in this state
-            }
+			if (res != TRANSITION_DENIED) {
+				break;  // changed successfully or already in this state
+			}
 
 		} else if (sp_man->loiter_switch == SWITCH_POS_ON) {
 			res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
@@ -2064,7 +2134,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 				break;	// changed successfully or already in this state
 			}
 
-            print_reject_mode(status_local, "AUTO_LOITER");
+			print_reject_mode(status_local, "AUTO_LOITER");
 
 		} else {
 			res = main_state_transition(status_local, MAIN_STATE_AUTO_MISSION);
@@ -2073,22 +2143,22 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
 				break;	// changed successfully or already in this state
 			}
 
-            print_reject_mode(status_local, "AUTO_MISSION");
+			print_reject_mode(status_local, "AUTO_MISSION");
 
-            // fallback to LOITER if home position not set
-            res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
+			// fallback to LOITER if home position not set
+			res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
 
-            if (res != TRANSITION_DENIED) {
-                break;  // changed successfully or already in this state
-            }
+			if (res != TRANSITION_DENIED) {
+				break;  // changed successfully or already in this state
+			}
 		}
 
-        // fallback to POSCTL
-        res = main_state_transition(status_local, MAIN_STATE_POSCTL);
+		// fallback to POSCTL
+		res = main_state_transition(status_local, MAIN_STATE_POSCTL);
 
-        if (res != TRANSITION_DENIED) {
-            break;  // changed successfully or already in this state
-        }
+		if (res != TRANSITION_DENIED) {
+			break;  // changed successfully or already in this state
+		}
 
 		// fallback to ALTCTL
 		res = main_state_transition(status_local, MAIN_STATE_ALTCTL);
@@ -2132,18 +2202,6 @@ set_control_mode()
 		control_mode.flag_control_termination_enabled = false;
 		break;
 
-	case NAVIGATION_STATE_ACRO:
-		control_mode.flag_control_manual_enabled = true;
-		control_mode.flag_control_auto_enabled = false;
-		control_mode.flag_control_rates_enabled = true;
-		control_mode.flag_control_attitude_enabled = false;
-		control_mode.flag_control_altitude_enabled = false;
-		control_mode.flag_control_climb_rate_enabled = false;
-		control_mode.flag_control_position_enabled = false;
-		control_mode.flag_control_velocity_enabled = false;
-		control_mode.flag_control_termination_enabled = false;
-		break;
-
 	case NAVIGATION_STATE_ALTCTL:
 		control_mode.flag_control_manual_enabled = true;
 		control_mode.flag_control_auto_enabled = false;
@@ -2156,59 +2214,6 @@ set_control_mode()
 		control_mode.flag_control_termination_enabled = false;
 		break;
 
-	case NAVIGATION_STATE_OFFBOARD:
-		control_mode.flag_control_manual_enabled = false;
-		control_mode.flag_control_auto_enabled = false;
-		control_mode.flag_control_offboard_enabled = true;
-
-		switch (sp_offboard.mode) {
-		case OFFBOARD_CONTROL_MODE_DIRECT_RATES:
-			control_mode.flag_control_rates_enabled = true;
-			control_mode.flag_control_attitude_enabled = false;
-			control_mode.flag_control_altitude_enabled = false;
-			control_mode.flag_control_climb_rate_enabled = false;
-			control_mode.flag_control_position_enabled = false;
-			control_mode.flag_control_velocity_enabled = false;
-			break;
-		case OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE:
-			control_mode.flag_control_rates_enabled = true;
-			control_mode.flag_control_attitude_enabled = true;
-			control_mode.flag_control_altitude_enabled = false;
-			control_mode.flag_control_climb_rate_enabled = false;
-			control_mode.flag_control_position_enabled = false;
-			control_mode.flag_control_velocity_enabled = false;
-			break;
-		case OFFBOARD_CONTROL_MODE_DIRECT_FORCE:
-			control_mode.flag_control_rates_enabled = true;
-			control_mode.flag_control_attitude_enabled = false;
-			control_mode.flag_control_force_enabled = true;
-			control_mode.flag_control_altitude_enabled = false;
-			control_mode.flag_control_climb_rate_enabled = false;
-			control_mode.flag_control_position_enabled = false;
-			control_mode.flag_control_velocity_enabled = false;
-			break;
-		case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_NED:
-		case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_OFFSET_NED:
-		case OFFBOARD_CONTROL_MODE_DIRECT_BODY_NED:
-		case OFFBOARD_CONTROL_MODE_DIRECT_BODY_OFFSET_NED:
-			control_mode.flag_control_rates_enabled = true;
-			control_mode.flag_control_attitude_enabled = true;
-			control_mode.flag_control_altitude_enabled = true;
-			control_mode.flag_control_climb_rate_enabled = true;
-			control_mode.flag_control_position_enabled = true;
-			control_mode.flag_control_velocity_enabled = true;
-			//XXX: the flags could depend on sp_offboard.ignore
-			break;
-		default:
-			control_mode.flag_control_rates_enabled = false;
-			control_mode.flag_control_attitude_enabled = false;
-			control_mode.flag_control_altitude_enabled = false;
-			control_mode.flag_control_climb_rate_enabled = false;
-			control_mode.flag_control_position_enabled = false;
-			control_mode.flag_control_velocity_enabled = false;
-		}
-		break;
-
 	case NAVIGATION_STATE_POSCTL:
 		control_mode.flag_control_manual_enabled = true;
 		control_mode.flag_control_auto_enabled = false;
@@ -2224,6 +2229,7 @@ set_control_mode()
 	case NAVIGATION_STATE_AUTO_MISSION:
 	case NAVIGATION_STATE_AUTO_LOITER:
 	case NAVIGATION_STATE_AUTO_RTL:
+	case NAVIGATION_STATE_AUTO_RCRECOVER:
 	case NAVIGATION_STATE_AUTO_RTGS:
 	case NAVIGATION_STATE_AUTO_LANDENGFAIL:
 		control_mode.flag_control_manual_enabled = false;
@@ -2249,6 +2255,19 @@ set_control_mode()
 		control_mode.flag_control_termination_enabled = false;
 		break;
 
+	case NAVIGATION_STATE_ACRO:
+		control_mode.flag_control_manual_enabled = true;
+		control_mode.flag_control_auto_enabled = false;
+		control_mode.flag_control_rates_enabled = true;
+		control_mode.flag_control_attitude_enabled = false;
+		control_mode.flag_control_altitude_enabled = false;
+		control_mode.flag_control_climb_rate_enabled = false;
+		control_mode.flag_control_position_enabled = false;
+		control_mode.flag_control_velocity_enabled = false;
+		control_mode.flag_control_termination_enabled = false;
+		break;
+
+
 	case NAVIGATION_STATE_LAND:
 		control_mode.flag_control_manual_enabled = false;
 		control_mode.flag_control_auto_enabled = true;
@@ -2262,6 +2281,19 @@ set_control_mode()
 		control_mode.flag_control_termination_enabled = false;
 		break;
 
+	case NAVIGATION_STATE_DESCEND:
+		/* TODO: check if this makes sense */
+		control_mode.flag_control_manual_enabled = false;
+		control_mode.flag_control_auto_enabled = true;
+		control_mode.flag_control_rates_enabled = true;
+		control_mode.flag_control_attitude_enabled = true;
+		control_mode.flag_control_position_enabled = false;
+		control_mode.flag_control_velocity_enabled = false;
+		control_mode.flag_control_altitude_enabled = false;
+		control_mode.flag_control_climb_rate_enabled = true;
+		control_mode.flag_control_termination_enabled = false;
+		break;
+
 	case NAVIGATION_STATE_TERMINATION:
 		/* disable all controllers on termination */
 		control_mode.flag_control_manual_enabled = false;
@@ -2275,6 +2307,63 @@ set_control_mode()
 		control_mode.flag_control_termination_enabled = true;
 		break;
 
+	case NAVIGATION_STATE_OFFBOARD:
+		control_mode.flag_control_manual_enabled = false;
+		control_mode.flag_control_auto_enabled = false;
+		control_mode.flag_control_offboard_enabled = true;
+
+		switch (sp_offboard.mode) {
+		case OFFBOARD_CONTROL_MODE_DIRECT_RATES:
+			control_mode.flag_control_rates_enabled = true;
+			control_mode.flag_control_attitude_enabled = false;
+			control_mode.flag_control_altitude_enabled = false;
+			control_mode.flag_control_climb_rate_enabled = false;
+			control_mode.flag_control_position_enabled = false;
+			control_mode.flag_control_velocity_enabled = false;
+			break;
+
+		case OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE:
+			control_mode.flag_control_rates_enabled = true;
+			control_mode.flag_control_attitude_enabled = true;
+			control_mode.flag_control_altitude_enabled = false;
+			control_mode.flag_control_climb_rate_enabled = false;
+			control_mode.flag_control_position_enabled = false;
+			control_mode.flag_control_velocity_enabled = false;
+			break;
+
+		case OFFBOARD_CONTROL_MODE_DIRECT_FORCE:
+			control_mode.flag_control_rates_enabled = true;
+			control_mode.flag_control_attitude_enabled = false;
+			control_mode.flag_control_force_enabled = true;
+			control_mode.flag_control_altitude_enabled = false;
+			control_mode.flag_control_climb_rate_enabled = false;
+			control_mode.flag_control_position_enabled = false;
+			control_mode.flag_control_velocity_enabled = false;
+			break;
+
+		case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_NED:
+		case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_OFFSET_NED:
+		case OFFBOARD_CONTROL_MODE_DIRECT_BODY_NED:
+		case OFFBOARD_CONTROL_MODE_DIRECT_BODY_OFFSET_NED:
+			control_mode.flag_control_rates_enabled = true;
+			control_mode.flag_control_attitude_enabled = true;
+			control_mode.flag_control_altitude_enabled = true;
+			control_mode.flag_control_climb_rate_enabled = true;
+			control_mode.flag_control_position_enabled = true;
+			control_mode.flag_control_velocity_enabled = true;
+			//XXX: the flags could depend on sp_offboard.ignore
+			break;
+
+		default:
+			control_mode.flag_control_rates_enabled = false;
+			control_mode.flag_control_attitude_enabled = false;
+			control_mode.flag_control_altitude_enabled = false;
+			control_mode.flag_control_climb_rate_enabled = false;
+			control_mode.flag_control_position_enabled = false;
+			control_mode.flag_control_velocity_enabled = false;
+		}
+		break;
+
 	default:
 		break;
 	}
@@ -2416,7 +2505,8 @@ void *commander_low_prio_loop(void *arg)
 				int calib_ret = ERROR;
 
 				/* try to go to INIT/PREFLIGHT arming state */
-				if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed, true /* fRunPreArmChecks */, mavlink_fd)) {
+				if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed,
+						true /* fRunPreArmChecks */, mavlink_fd)) {
 					answer_command(cmd, VEHICLE_CMD_RESULT_DENIED);
 					break;
 				}
diff --git a/src/modules/commander/gyro_calibration.cpp b/src/modules/commander/gyro_calibration.cpp
index d89c67c2b..8ab14dd52 100644
--- a/src/modules/commander/gyro_calibration.cpp
+++ b/src/modules/commander/gyro_calibration.cpp
@@ -63,7 +63,10 @@ static const char *sensor_name = "gyro";
 int do_gyro_calibration(int mavlink_fd)
 {
 	mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
-	mavlink_log_info(mavlink_fd, "don't move system");
+	mavlink_log_info(mavlink_fd, "HOLD STILL");
+
+	/* wait for the user to respond */
+	sleep(2);
 
 	struct gyro_scale gyro_scale = {
 		0.0f,
diff --git a/src/modules/commander/mag_calibration.cpp b/src/modules/commander/mag_calibration.cpp
index 23900f386..7be8de9c6 100644
--- a/src/modules/commander/mag_calibration.cpp
+++ b/src/modules/commander/mag_calibration.cpp
@@ -155,7 +155,7 @@ int do_mag_calibration(int mavlink_fd)
 		uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval;
 		unsigned poll_errcount = 0;
 
-		mavlink_log_info(mavlink_fd, "rotate in a figure 8 around all axis");
+		mavlink_log_info(mavlink_fd, "Turn on all sides: front/back,left/right,up/down");
 
 		calibration_counter = 0;
 
diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp
index 9568752ae..e37019d02 100644
--- a/src/modules/commander/state_machine_helper.cpp
+++ b/src/modules/commander/state_machine_helper.cpp
@@ -444,7 +444,7 @@ transition_result_t hil_state_transition(hil_state_t new_state, int status_pub,
  * Check failsafe and main status and set navigation status for navigator accordingly
  */
 bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_enabled, const bool mission_finished,
-		const bool stay_in_failsafe)
+		   const bool stay_in_failsafe)
 {
 	navigation_state_t nav_state_old = status->nav_state;
 
@@ -497,11 +497,13 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
 		break;
 
 	case MAIN_STATE_AUTO_MISSION:
+
 		/* go into failsafe
 		 * - if commanded to do so
 		 * - if we have an engine failure
-		 * - if either the datalink is enabled and lost as well as RC is lost
-		 * - if there is no datalink and the mission is finished */
+		 * - depending on datalink, RC and if the mission is finished */
+
+		/* first look at the commands */
 		if (status->engine_failure_cmd) {
 			status->nav_state = NAVIGATION_STATE_AUTO_LANDENGFAIL;
 		} else if (status->data_link_lost_cmd) {
@@ -509,14 +511,17 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
 		} else if (status->gps_failure_cmd) {
 			status->nav_state = NAVIGATION_STATE_AUTO_LANDGPSFAIL;
 		} else if (status->rc_signal_lost_cmd) {
-			status->nav_state = NAVIGATION_STATE_AUTO_RTGS; //XXX
-		/* Finished handling commands which have priority , now handle failures */
+			status->nav_state = NAVIGATION_STATE_AUTO_RCRECOVER;
+
+		/* finished handling commands which have priority, now handle failures */
 		} else if (status->gps_failure) {
 			status->nav_state = NAVIGATION_STATE_AUTO_LANDGPSFAIL;
 		} else if (status->engine_failure) {
 			status->nav_state = NAVIGATION_STATE_AUTO_LANDENGFAIL;
-		} else if (((status->data_link_lost && data_link_loss_enabled) && status->rc_signal_lost) ||
-		    (!data_link_loss_enabled && status->rc_signal_lost && mission_finished)) {
+
+		/* datalink loss enabled:
+		 * check for datalink lost: this should always trigger RTGS */
+		} else if (data_link_loss_enabled && status->data_link_lost) {
 			status->failsafe = true;
 
 			if (status->condition_global_position_valid && status->condition_home_position_valid) {
@@ -529,12 +534,15 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
 				status->nav_state = NAVIGATION_STATE_TERMINATION;
 			}
 
-		/* also go into failsafe if just datalink is lost */
-		} else if (status->data_link_lost && data_link_loss_enabled) {
+		/* datalink loss disabled:
+		 * check if both, RC and datalink are lost during the mission
+		 * or RC is lost after the mission is finished: this should always trigger RCRECOVER */
+		} else if (!data_link_loss_enabled && ((status->rc_signal_lost && status->data_link_lost) ||
+						       (status->rc_signal_lost && mission_finished))) {
 			status->failsafe = true;
 
 			if (status->condition_global_position_valid && status->condition_home_position_valid) {
-				status->nav_state = NAVIGATION_STATE_AUTO_RTGS;
+				status->nav_state = NAVIGATION_STATE_AUTO_RCRECOVER;
 			} else if (status->condition_local_position_valid) {
 				status->nav_state = NAVIGATION_STATE_LAND;
 			} else if (status->condition_local_altitude_valid) {
@@ -543,13 +551,8 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
 				status->nav_state = NAVIGATION_STATE_TERMINATION;
 			}
 
-		/* don't bother if RC is lost and mission is not yet finished */
-		} else if (status->rc_signal_lost && !stay_in_failsafe) {
-
-			/* this mode is ok, we don't need RC for missions */
-			status->nav_state = NAVIGATION_STATE_AUTO_MISSION;
+		/* stay where you are if you should stay in failsafe, otherwise everything is perfect */
 		} else if (!stay_in_failsafe){
-			/* everything is perfect */
 			status->nav_state = NAVIGATION_STATE_AUTO_MISSION;
 		}
 		break;