Merged PX4Flow driver changes

2026-06-25 12:10:35 +08:00 · 2014-11-26 07:43:19 +01:00
parent 739c407cfd 4724c05047
commit cbcd1ea1d1
155 changed files with 2152 additions and 765 deletions
@@ -206,10 +206,6 @@ const unsigned int loop_interval_alarm = 6500;	// loop interval in microseconds
 			      0,  0,  1.f
 			     };		/**< init: identity matrix */

-	// print text
-	printf("Extended Kalman Filter Attitude Estimator initialized..\n\n");
-	fflush(stdout);
-
 	int overloadcounter = 19;

 	/* Initialize filter */
@@ -223,7 +223,7 @@ BottleDrop::start()
 	_main_task = task_spawn_cmd("bottle_drop",
 				    SCHED_DEFAULT,
 				    SCHED_PRIORITY_DEFAULT + 15,
-				    2048,
+				    1500,
 				    (main_t)&BottleDrop::task_main_trampoline,
 				    nullptr);

@@ -283,7 +283,6 @@ BottleDrop::drop()
 	// force the door open if we have to
 	if (_doors_opened == 0) {
 		open_bay();
-		warnx("bay not ready, forced open");
 	}

 	while (hrt_elapsed_time(&_doors_opened) < 500 * 1000 && hrt_elapsed_time(&starttime) < 2000000) {
@@ -723,16 +722,16 @@ BottleDrop::handle_command(struct vehicle_command_s *cmd)
 		if (cmd->param1 > 0.5f && cmd->param2 > 0.5f) {
 			open_bay();
 			drop();
-			mavlink_log_info(_mavlink_fd, "#audio: drop bottle");
+			mavlink_log_critical(_mavlink_fd, "drop bottle");

 		} else if (cmd->param1 > 0.5f) {
 			open_bay();
-			mavlink_log_info(_mavlink_fd, "#audio: opening bay");
+			mavlink_log_critical(_mavlink_fd, "opening bay");

 		} else {
 			lock_release();
 			close_bay();
-			mavlink_log_info(_mavlink_fd, "#audio: closing bay");
+			mavlink_log_critical(_mavlink_fd, "closing bay");
 		}

 		answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
@@ -743,12 +742,12 @@ BottleDrop::handle_command(struct vehicle_command_s *cmd)
 		switch ((int)(cmd->param1 + 0.5f)) {
 		case 0:
 			_drop_approval = false;
-			mavlink_log_info(_mavlink_fd, "#audio: got drop position, no approval");
+			mavlink_log_critical(_mavlink_fd, "got drop position, no approval");
 			break;

 		case 1:
 			_drop_approval = true;
-			mavlink_log_info(_mavlink_fd, "#audio: got drop position and approval");
+			mavlink_log_critical(_mavlink_fd, "got drop position and approval");
 			break;

 		default:
@@ -818,19 +817,19 @@ BottleDrop::answer_command(struct vehicle_command_s *cmd, enum VEHICLE_CMD_RESUL
 		break;

 	case VEHICLE_CMD_RESULT_DENIED:
-		mavlink_log_critical(_mavlink_fd, "#audio: command denied: %u", cmd->command);
+		mavlink_log_critical(_mavlink_fd, "command denied: %u", cmd->command);
 		break;

 	case VEHICLE_CMD_RESULT_FAILED:
-		mavlink_log_critical(_mavlink_fd, "#audio: command failed: %u", cmd->command);
+		mavlink_log_critical(_mavlink_fd, "command failed: %u", cmd->command);
 		break;

 	case VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED:
-		mavlink_log_critical(_mavlink_fd, "#audio: command temporarily rejected: %u", cmd->command);
+		mavlink_log_critical(_mavlink_fd, "command temporarily rejected: %u", cmd->command);
 		break;

 	case VEHICLE_CMD_RESULT_UNSUPPORTED:
-		mavlink_log_critical(_mavlink_fd, "#audio: command unsupported: %u", cmd->command);
+		mavlink_log_critical(_mavlink_fd, "command unsupported: %u", cmd->command);
 		break;

 	default:
@@ -39,3 +39,7 @@ MODULE_COMMAND		= bottle_drop

 SRCS			= bottle_drop.cpp \
 			  bottle_drop_params.c
+
+MAXOPTIMIZATION	 = -Os
+
+MODULE_STACKSIZE = 1200
@@ -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;
-		}
-
-		if (data_collected[orient]) {
-			mavlink_log_info(mavlink_fd, "%s done, rotate to a different axis", orientation_strs[orient]);
+			mavlink_log_info(mavlink_fd, "invalid motion, hold still...");
+			sleep(3);
 			continue;
 		}

-		mavlink_log_info(mavlink_fd, "accel measurement started: %s axis", orientation_strs[orient]);
+		/* inform user about already handled side */
+		if (data_collected[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, "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;
 				}
 			}
@@ -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;
 	}
@@ -220,8 +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();
@@ -312,12 +310,16 @@ int commander_main(int argc, char *argv[])
 	}

 	if (!strcmp(argv[1], "arm")) {
-		arm_disarm(true, mavlink_fd, "command line");
+		int mavlink_fd_local = open(MAVLINK_LOG_DEVICE, 0);
+		arm_disarm(true, mavlink_fd_local, "command line");
+		close(mavlink_fd_local);
 		exit(0);
 	}

 	if (!strcmp(argv[1], "disarm")) {
-		arm_disarm(false, mavlink_fd, "command line");
+		int mavlink_fd_local = open(MAVLINK_LOG_DEVICE, 0);
+		arm_disarm(false, mavlink_fd_local, "command line");
+		close(mavlink_fd_local);
 		exit(0);
 	}

@@ -760,7 +762,10 @@ 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";
@@ -1407,8 +1412,8 @@ 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. */
@@ -1418,7 +1423,7 @@ 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
+		} 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;
@@ -1543,7 +1548,7 @@ int commander_thread_main(int argc, char *argv[])

 			} else {
 				if (status.rc_signal_lost) {
-					mavlink_log_critical(mavlink_fd, "RC signal regained");
+					mavlink_log_critical(mavlink_fd, "RC SIGNAL REGAINED after %llums",(hrt_absolute_time()-status.rc_signal_lost_timestamp)/1000);
 					status_changed = true;
 				}
 			}
@@ -1644,8 +1649,9 @@ int commander_thread_main(int argc, char *argv[])

 		} else {
 			if (!status.rc_signal_lost) {
-				mavlink_log_critical(mavlink_fd, "RC SIGNAL LOST");
+				mavlink_log_critical(mavlink_fd, "RC SIGNAL LOST (at t=%llums)",hrt_absolute_time()/1000);
 				status.rc_signal_lost = true;
+				status.rc_signal_lost_timestamp=sp_man.timestamp;
 				status_changed = true;
 			}
 		}
@@ -1848,7 +1854,11 @@ 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;
 		}

@@ -2196,6 +2206,59 @@ set_control_mode()
 		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;
+		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 = false;
+		control_mode.flag_control_velocity_enabled = false;
+		control_mode.flag_control_termination_enabled = false;
+		break;
+
+	case NAVIGATION_STATE_POSCTL:
+		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 = 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;
+		control_mode.flag_control_termination_enabled = false;
+		break;
+
+	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;
+		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_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;
+		control_mode.flag_control_termination_enabled = false;
+		break;
+
+	case NAVIGATION_STATE_AUTO_LANDGPSFAIL:
+		control_mode.flag_control_manual_enabled = false;
+		control_mode.flag_control_auto_enabled = false;
+		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 = true;
+		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_ACRO:
 		control_mode.flag_control_manual_enabled = true;
 		control_mode.flag_control_auto_enabled = false;
@@ -2208,18 +2271,46 @@ set_control_mode()
 		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;
+
+	case NAVIGATION_STATE_LAND:
+		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;
+		/* in failsafe LAND mode position may be not available */
+		control_mode.flag_control_position_enabled = status.condition_local_position_valid;
+		control_mode.flag_control_velocity_enabled = status.condition_local_position_valid;
 		control_mode.flag_control_altitude_enabled = true;
 		control_mode.flag_control_climb_rate_enabled = true;
+		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;
+		control_mode.flag_control_auto_enabled = false;
+		control_mode.flag_control_rates_enabled = false;
+		control_mode.flag_control_attitude_enabled = false;
+		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 = false;
+		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;
@@ -2275,73 +2366,6 @@ set_control_mode()
 			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;
-		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;
-		control_mode.flag_control_termination_enabled = false;
-		break;
-
-	case NAVIGATION_STATE_AUTO_MISSION:
-	case NAVIGATION_STATE_AUTO_LOITER:
-	case NAVIGATION_STATE_AUTO_RTL:
-	case NAVIGATION_STATE_AUTO_RTGS:
-	case NAVIGATION_STATE_AUTO_LANDENGFAIL:
-		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_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;
-		control_mode.flag_control_termination_enabled = false;
-		break;
-
-	case NAVIGATION_STATE_AUTO_LANDGPSFAIL:
-		control_mode.flag_control_manual_enabled = false;
-		control_mode.flag_control_auto_enabled = false;
-		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 = true;
-		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;
-		control_mode.flag_control_rates_enabled = true;
-		control_mode.flag_control_attitude_enabled = true;
-		/* in failsafe LAND mode position may be not available */
-		control_mode.flag_control_position_enabled = status.condition_local_position_valid;
-		control_mode.flag_control_velocity_enabled = status.condition_local_position_valid;
-		control_mode.flag_control_altitude_enabled = true;
-		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;
-		control_mode.flag_control_auto_enabled = false;
-		control_mode.flag_control_rates_enabled = false;
-		control_mode.flag_control_attitude_enabled = false;
-		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 = false;
-		control_mode.flag_control_termination_enabled = true;
 		break;

 	default:
@@ -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,
@@ -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;

@@ -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;
@@ -703,7 +706,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
 		}

 		if (fabsf(airspeed.indicated_airspeed_m_s > 6.0f)) {
-			mavlink_log_critical(mavlink_fd, "AIRSPEED WARNING: WIND OR CALIBRATION MISSING");
+			mavlink_log_critical(mavlink_fd, "AIRSPEED WARNING: WIND OR CALIBRATION ISSUE");
 			// XXX do not make this fatal yet
 		}
 	}
@@ -39,3 +39,5 @@ SRCS		 = test_params.c \
 		   block/BlockParam.cpp \
 		   uorb/blocks.cpp \
 		   blocks.cpp
+
+MAXOPTIMIZATION = -Os
@@ -629,9 +629,6 @@ task_main(int argc, char *argv[])
 {
 	work_q_item_t *work;

-	/* inform about start */
-	warnx("Initializing..");
-
 	/* Initialize global variables */
 	g_key_offsets[0] = 0;

@@ -694,16 +691,15 @@ task_main(int argc, char *argv[])
 		if (sys_restart_val == DM_INIT_REASON_POWER_ON) {
 			warnx("Power on restart");
 			_restart(DM_INIT_REASON_POWER_ON);
-		}
-		else if (sys_restart_val == DM_INIT_REASON_IN_FLIGHT) {
+		} else if (sys_restart_val == DM_INIT_REASON_IN_FLIGHT) {
 			warnx("In flight restart");
 			_restart(DM_INIT_REASON_IN_FLIGHT);
-		}
-		else
+		} else {
 			warnx("Unknown restart");
-	}
-	else
+		}
+	} else {
 		warnx("Unknown restart");
+	}

 	/* We use two file descriptors, one for the caller context and one for the worker thread */
 	/* They are actually the same but we need to some way to reject caller request while the */
@@ -613,8 +613,11 @@ FixedwingEstimator::check_filter_state()
 			warn_index = max_warn_index;
 		}

-		warnx("reset: %s", feedback[warn_index]);
-		mavlink_log_critical(_mavlink_fd, "[ekf check] %s", feedback[warn_index]);
+		// Do not warn about accel offset if we have no position updates
+		if (!(warn_index == 5 && _ekf->staticMode)) {
+			warnx("reset: %s", feedback[warn_index]);
+			mavlink_log_critical(_mavlink_fd, "[ekf check] %s", feedback[warn_index]);
+		}
 	}

 	struct estimator_status_report rep;
@@ -1557,7 +1560,7 @@ FixedwingEstimator::start()
 	_estimator_task = task_spawn_cmd("ekf_att_pos_estimator",
 					 SCHED_DEFAULT,
 					 SCHED_PRIORITY_MAX - 40,
-					 5000,
+					 7500,
 					 (main_t)&FixedwingEstimator::task_main_trampoline,
 					 nullptr);

@@ -78,11 +78,7 @@ PARAM_DEFINE_INT32(MAV_FWDEXTSP, 1);

 mavlink_system_t mavlink_system = {
 	100,
-	50,
-	MAV_TYPE_FIXED_WING,
-	0,
-	0,
-	0
+	50
 }; // System ID, 1-255, Component/Subsystem ID, 1-255

 /*
@@ -167,8 +167,10 @@ Mavlink::Mavlink() :
 	_param_initialized(false),
 	_param_system_id(0),
 	_param_component_id(0),
-	_param_system_type(0),
+	_param_system_type(MAV_TYPE_FIXED_WING),
 	_param_use_hil_gps(0),
+	_param_forward_externalsp(0),
+	_system_type(0),

 	/* performance counters */
 	_loop_perf(perf_alloc(PC_ELAPSED, "mavlink_el")),
@@ -524,7 +526,7 @@ void Mavlink::mavlink_update_system(void)
 	param_get(_param_system_type, &system_type);

 	if (system_type >= 0 && system_type < MAV_TYPE_ENUM_END) {
-		mavlink_system.type = system_type;
+		_system_type = system_type;
 	}

 	int32_t use_hil_gps;
@@ -755,7 +757,7 @@ Mavlink::send_message(const uint8_t msgid, const void *msg)

 	pthread_mutex_lock(&_send_mutex);

-	int buf_free = get_free_tx_buf();
+	unsigned buf_free = get_free_tx_buf();

 	uint8_t payload_len = mavlink_message_lengths[msgid];
 	unsigned packet_len = payload_len + MAVLINK_NUM_NON_PAYLOAD_BYTES;
@@ -820,14 +822,14 @@ Mavlink::resend_message(mavlink_message_t *msg)

 	pthread_mutex_lock(&_send_mutex);

-	int buf_free = get_free_tx_buf();
+	unsigned buf_free = get_free_tx_buf();

 	_last_write_try_time = hrt_absolute_time();

 	unsigned packet_len = msg->len + MAVLINK_NUM_NON_PAYLOAD_BYTES;

 	/* check if there is space in the buffer, let it overflow else */
-	if (buf_free < TX_BUFFER_GAP) {
+	if ((buf_free < TX_BUFFER_GAP) || (buf_free < packet_len)) {
 		/* no enough space in buffer to send */
 		count_txerr();
 		count_txerrbytes(packet_len);
@@ -1634,7 +1636,7 @@ Mavlink::start(int argc, char *argv[])
 	task_spawn_cmd(buf,
 		       SCHED_DEFAULT,
 		       SCHED_PRIORITY_DEFAULT,
-		       2700,
+		       2800,
 		       (main_t)&Mavlink::start_helper,
 		       (const char **)argv);

@@ -265,6 +265,8 @@ public:

 	struct mavlink_logbuffer	*get_logbuffer() { return &_logbuffer; }

+	unsigned		get_system_type() { return _system_type; }
+
 protected:
 	Mavlink			*next;

@@ -354,6 +356,8 @@ private:
 	param_t			_param_use_hil_gps;
 	param_t			_param_forward_externalsp;

+	unsigned		_system_type;
+
 	perf_counter_t		_loop_perf;			/**< loop performance counter */
 	perf_counter_t		_txerr_perf;			/**< TX error counter */

@@ -302,7 +302,7 @@ protected:
 		msg.base_mode = 0;
 		msg.custom_mode = 0;
 		get_mavlink_mode_state(&status, &pos_sp_triplet, &msg.system_status, &msg.base_mode, &msg.custom_mode);
-		msg.type = mavlink_system.type;
+		msg.type = _mavlink->get_system_type();
 		msg.autopilot = MAV_AUTOPILOT_PX4;
 		msg.mavlink_version = 3;

@@ -382,11 +382,11 @@ protected:
 						clock_gettime(CLOCK_REALTIME, &ts);
 						/* use GPS time for log file naming, e.g. /fs/microsd/2014-01-19/19_37_52.bin */
 						time_t gps_time_sec = ts.tv_sec + (ts.tv_nsec / 1e9);
-						struct tm t;
-						gmtime_r(&gps_time_sec, &t);
+						struct tm tt;
+						gmtime_r(&gps_time_sec, &tt);

 						// XXX we do not want to interfere here with the SD log app
-						strftime(log_file_name, sizeof(log_file_name), "msgs_%Y_%m_%d_%H_%M_%S.txt", &t);
+						strftime(log_file_name, sizeof(log_file_name), "msgs_%Y_%m_%d_%H_%M_%S.txt", &tt);
 						snprintf(log_file_path, sizeof(log_file_path), "/fs/microsd/%s", log_file_name);
 						fp = fopen(log_file_path, "ab");
 					}
@@ -1353,15 +1353,17 @@ protected:

 			const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2;

+			unsigned system_type = _mavlink->get_system_type();
+
 			/* scale outputs depending on system type */
-			if (mavlink_system.type == MAV_TYPE_QUADROTOR ||
-				mavlink_system.type == MAV_TYPE_HEXAROTOR ||
-				mavlink_system.type == MAV_TYPE_OCTOROTOR) {
+			if (system_type == MAV_TYPE_QUADROTOR ||
+				system_type == MAV_TYPE_HEXAROTOR ||
+				system_type == MAV_TYPE_OCTOROTOR) {
 				/* multirotors: set number of rotor outputs depending on type */

 				unsigned n;

-				switch (mavlink_system.type) {
+				switch (system_type) {
 				case MAV_TYPE_QUADROTOR:
 					n = 4;
 					break;
@@ -1717,7 +1719,53 @@ protected:
 			msg.chan16_raw = (rc.channel_count > 15) ? rc.values[15] : UINT16_MAX;
 			msg.chan17_raw = (rc.channel_count > 16) ? rc.values[16] : UINT16_MAX;
 			msg.chan18_raw = (rc.channel_count > 17) ? rc.values[17] : UINT16_MAX;
-			msg.rssi = rc.rssi;
+
+			/* RSSI has a max value of 100, and when Spektrum or S.BUS are
+			 * available, the RSSI field is invalid, as they do not provide
+			 * an RSSI measurement. Use an out of band magic value to signal
+			 * these digital ports. XXX revise MAVLink spec to address this.
+			 * One option would be to use the top bit to toggle between RSSI
+			 * and input source mode.
+			 *
+			 * Full RSSI field: 0b 1 111 1111
+			 *
+			 *                     ^ If bit is set, RSSI encodes type + RSSI
+			 *
+			 *                       ^ These three bits encode a total of 8
+			 *                         digital RC input types.
+			 *                         0: PPM, 1: SBUS, 2: Spektrum, 2: ST24
+			 *                           ^ These four bits encode a total of
+			 *                             16 RSSI levels. 15 = full, 0 = no signal
+			 *
+			 */
+
+			/* Initialize RSSI with the special mode level flag */
+			msg.rssi = (1 << 7);
+
+			/* Set RSSI */
+			msg.rssi |= (rc.rssi <= 100) ? ((rc.rssi / 7) + 1) : 15;
+
+			switch (rc.input_source) {
+				case RC_INPUT_SOURCE_PX4FMU_PPM:
+				/* fallthrough */
+				case RC_INPUT_SOURCE_PX4IO_PPM:
+					msg.rssi |= (0 << 4);
+					break;
+				case RC_INPUT_SOURCE_PX4IO_SPEKTRUM:
+					msg.rssi |= (1 << 4);
+					break;
+				case RC_INPUT_SOURCE_PX4IO_SBUS:
+					msg.rssi |= (2 << 4);
+					break;
+				case RC_INPUT_SOURCE_PX4IO_ST24:
+					msg.rssi |= (3 << 4);
+					break;
+			}
+
+			if (rc.rc_lost) {
+				/* RSSI is by definition zero */
+				msg.rssi = 0;
+			}

 			_mavlink->send_message(MAVLINK_MSG_ID_RC_CHANNELS, &msg);
 		}
@@ -546,12 +546,16 @@ MavlinkReceiver::handle_message_set_position_target_local_ned(mavlink_message_t
 			offboard_control_sp.ignore &=  ~(1 << i);
 			offboard_control_sp.ignore |=  (set_position_target_local_ned.type_mask & (1 << i));
 		}
+
 		offboard_control_sp.ignore &=  ~(1 << OFB_IGN_BIT_YAW);
-			offboard_control_sp.ignore |=  (set_position_target_local_ned.type_mask & (1 << 10)) <<
-					OFB_IGN_BIT_YAW;
+		if (set_position_target_local_ned.type_mask & (1 << 10)) {
+			offboard_control_sp.ignore |=  (1 << OFB_IGN_BIT_YAW);
+		}
+
 		offboard_control_sp.ignore &=  ~(1 << OFB_IGN_BIT_YAWRATE);
-			offboard_control_sp.ignore |=  (set_position_target_local_ned.type_mask & (1 << 11)) <<
-					OFB_IGN_BIT_YAWRATE;
+		if (set_position_target_local_ned.type_mask & (1 << 11)) {
+			offboard_control_sp.ignore |=  (1 << OFB_IGN_BIT_YAWRATE);
+		}

 		offboard_control_sp.timestamp = hrt_absolute_time();

@@ -1404,7 +1408,7 @@ MavlinkReceiver::receive_start(Mavlink *parent)

 	struct sched_param param;
 	(void)pthread_attr_getschedparam(&receiveloop_attr, &param);
-	param.sched_priority = SCHED_PRIORITY_MAX - 40;
+	param.sched_priority = SCHED_PRIORITY_MAX - 80;
 	(void)pthread_attr_setschedparam(&receiveloop_attr, &param);

 	pthread_attr_setstacksize(&receiveloop_attr, 2900);
@@ -721,8 +721,6 @@ MulticopterAttitudeControl::task_main_trampoline(int argc, char *argv[])
 void
 MulticopterAttitudeControl::task_main()
 {
-	warnx("started");
-	fflush(stdout);

 	/*
 	 * do subscriptions
@@ -535,7 +535,7 @@ MulticopterPositionControl::reset_pos_sp()
 				- _params.vel_ff(0) * _sp_move_rate(0)) / _params.pos_p(0);
 		_pos_sp(1) = _pos(1) + (_vel(1) - _att_sp.R_body[1][2] * _att_sp.thrust / _params.vel_p(1)
 				- _params.vel_ff(1) * _sp_move_rate(1)) / _params.pos_p(1);
-		mavlink_log_info(_mavlink_fd, "[mpc] reset pos sp: %.2f, %.2f", (double)_pos_sp(0), (double)_pos_sp(1));
+		mavlink_log_info(_mavlink_fd, "[mpc] reset pos sp: %d, %d", (int)_pos_sp(0), (int)_pos_sp(1));
 	}
 }

@@ -545,7 +545,7 @@ MulticopterPositionControl::reset_alt_sp()
 	if (_reset_alt_sp) {
 		_reset_alt_sp = false;
 		_pos_sp(2) = _pos(2) + (_vel(2) - _params.vel_ff(2) * _sp_move_rate(2)) / _params.pos_p(2);
-		mavlink_log_info(_mavlink_fd, "[mpc] reset alt sp: %.2f", -(double)_pos_sp(2));
+		mavlink_log_info(_mavlink_fd, "[mpc] reset alt sp: %d", -(int)_pos_sp(2));
 	}
 }

@@ -857,10 +857,8 @@ MulticopterPositionControl::control_auto(float dt)
 void
 MulticopterPositionControl::task_main()
 {
-	warnx("started");

 	_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
-	mavlink_log_info(_mavlink_fd, "[mpc] started");

 	/*
 	 * do subscriptions
@@ -156,6 +156,7 @@ DataLinkLoss::set_dll_item()
 		/* Request flight termination from the commander */
 		_navigator->get_mission_result()->flight_termination = true;
 		_navigator->publish_mission_result();
+		reset_mission_item_reached();
 		warnx("not switched to manual: request flight termination");
 		pos_sp_triplet->previous.valid = false;
 		pos_sp_triplet->current.valid = false;
@@ -188,6 +189,7 @@ DataLinkLoss::advance_dll()
 			mavlink_log_info(_navigator->get_mavlink_fd(), "#audio: too many DL losses, fly to airfield home");
 			_navigator->get_mission_result()->stay_in_failsafe = true;
 			_navigator->publish_mission_result();
+			reset_mission_item_reached();
 			_dll_state = DLL_STATE_FLYTOAIRFIELDHOMEWP;
 		} else {
 			if (!_param_skipcommshold.get()) {
@@ -208,6 +210,7 @@ DataLinkLoss::advance_dll()
 		_dll_state = DLL_STATE_FLYTOAIRFIELDHOMEWP;
 		_navigator->get_mission_result()->stay_in_failsafe = true;
 		_navigator->publish_mission_result();
+		reset_mission_item_reached();
 		break;
 	case DLL_STATE_FLYTOAIRFIELDHOMEWP:
 		_dll_state = DLL_STATE_TERMINATE;
@@ -215,6 +218,7 @@ DataLinkLoss::advance_dll()
 		mavlink_log_info(_navigator->get_mavlink_fd(), "#audio: no manual control, terminating");
 		_navigator->get_mission_result()->stay_in_failsafe = true;
 		_navigator->publish_mission_result();
+		reset_mission_item_reached();
 		break;
 	case DLL_STATE_TERMINATE:
 		warnx("dll end");
@@ -371,7 +371,7 @@ Mission::set_mission_items()
 	} else {
 		/* no mission available or mission finished, switch to loiter */
 		if (_mission_type != MISSION_TYPE_NONE) {
-			mavlink_log_critical(_navigator->get_mavlink_fd(), "mission finished, loitering");
+			mavlink_log_critical(_navigator->get_mavlink_fd(), "mission finished");

 			/* use last setpoint for loiter */
 			_navigator->set_can_loiter_at_sp(true);
@@ -595,13 +595,15 @@ Mission::read_mission_item(bool onboard, bool is_current, struct mission_item_s
 		dm_item = DM_KEY_WAYPOINTS_OFFBOARD(_offboard_mission.dataman_id);
 	}

-	if (*mission_index_ptr < 0 || *mission_index_ptr >= (int)mission->count) {
-		/* mission item index out of bounds */
-		return false;
-	}
-
-	/* repeat several to get the mission item because we might have to follow multiple DO_JUMPS */
+	/* Repeat this several times in case there are several DO JUMPS that we need to follow along, however, after
+	 * 10 iterations we have to assume that the DO JUMPS are probably cycling and give up. */
 	for (int i = 0; i < 10; i++) {
+
+		if (*mission_index_ptr < 0 || *mission_index_ptr >= (int)mission->count) {
+			/* mission item index out of bounds */
+			return false;
+		}
+
 		const ssize_t len = sizeof(struct mission_item_s);

 		/* read mission item to temp storage first to not overwrite current mission item if data damaged */
@@ -626,11 +628,12 @@ Mission::read_mission_item(bool onboard, bool is_current, struct mission_item_s
 				if (is_current) {
 					(mission_item_tmp.do_jump_current_count)++;
 					/* save repeat count */
-					if (dm_write(dm_item, *mission_index_ptr, DM_PERSIST_IN_FLIGHT_RESET, &mission_item_tmp, len) != len) {
+					if (dm_write(dm_item, *mission_index_ptr, DM_PERSIST_POWER_ON_RESET,
+					    &mission_item_tmp, len) != len) {
 						/* not supposed to happen unless the datamanager can't access the
 						 * dataman */
 						mavlink_log_critical(_navigator->get_mavlink_fd(),
-								"ERROR DO JUMP waypoint could not be written");
+								     "ERROR DO JUMP waypoint could not be written");
 						return false;
 					}
 				}
@@ -639,8 +642,10 @@ Mission::read_mission_item(bool onboard, bool is_current, struct mission_item_s
 				*mission_index_ptr = mission_item_tmp.do_jump_mission_index;

 			} else {
-				mavlink_log_critical(_navigator->get_mavlink_fd(),
-						 "DO JUMP repetitions completed");
+				if (is_current) {
+					mavlink_log_critical(_navigator->get_mavlink_fd(),
+							     "DO JUMP repetitions completed");
+				}
 				/* no more DO_JUMPS, therefore just try to continue with next mission item */
 				(*mission_index_ptr)++;
 			}
@@ -707,6 +712,7 @@ Mission::set_mission_item_reached()
 	_navigator->get_mission_result()->reached = true;
 	_navigator->get_mission_result()->seq_reached = _current_offboard_mission_index;
 	_navigator->publish_mission_result();
+	reset_mission_item_reached();
 }

 void
@@ -205,6 +205,7 @@ private:

 	bool		_can_loiter_at_sp;			/**< flags if current position SP can be used to loiter */
 	bool		_pos_sp_triplet_updated;		/**< flags if position SP triplet needs to be published */
+	bool 		_pos_sp_triplet_published_invalid_once;	/**< flags if position SP triplet has been published once to UORB */

 	control::BlockParamFloat _param_loiter_radius;	/**< loiter radius for fixedwing */
 	control::BlockParamFloat _param_acceptance_radius;	/**< acceptance for takeoff */
@@ -137,6 +137,7 @@ Navigator::Navigator() :
 	_gpsFailure(this, "GPSF"),
 	_can_loiter_at_sp(false),
 	_pos_sp_triplet_updated(false),
+	_pos_sp_triplet_published_invalid_once(false),
 	_param_loiter_radius(this, "LOITER_RAD"),
 	_param_acceptance_radius(this, "ACC_RAD"),
 	_param_datalinkloss_obc(this, "DLL_OBC"),
@@ -289,8 +290,9 @@ Navigator::task_main()
 	navigation_capabilities_update();
 	params_update();

-	/* rate limit position updates to 50 Hz */
+	/* rate limit position and sensor updates to 50 Hz */
 	orb_set_interval(_global_pos_sub, 20);
+	orb_set_interval(_sensor_combined_sub, 20);

 	hrt_abstime mavlink_open_time = 0;
 	const hrt_abstime mavlink_open_interval = 500000;
@@ -426,12 +428,15 @@ Navigator::task_main()
 				_can_loiter_at_sp = false;
 				break;
 			case NAVIGATION_STATE_AUTO_MISSION:
+				_pos_sp_triplet_published_invalid_once = false;
 				_navigation_mode = &_mission;
 				break;
 			case NAVIGATION_STATE_AUTO_LOITER:
+				_pos_sp_triplet_published_invalid_once = false;
 				_navigation_mode = &_loiter;
 				break;
 			case NAVIGATION_STATE_AUTO_RCRECOVER:
+				_pos_sp_triplet_published_invalid_once = false;
 				if (_param_rcloss_obc.get() != 0) {
 					_navigation_mode = &_rcLoss;
 				} else {
@@ -439,11 +444,13 @@ Navigator::task_main()
 				}
 				break;
 			case NAVIGATION_STATE_AUTO_RTL:
-					_navigation_mode = &_rtl;
+				_pos_sp_triplet_published_invalid_once = false;
+				_navigation_mode = &_rtl;
 				break;
 			case NAVIGATION_STATE_AUTO_RTGS:
 				/* Use complex data link loss mode only when enabled via param
 				* otherwise use rtl */
+				_pos_sp_triplet_published_invalid_once = false;
 				if (_param_datalinkloss_obc.get() != 0) {
 					_navigation_mode = &_dataLinkLoss;
 				} else {
@@ -451,9 +458,11 @@ Navigator::task_main()
 				}
 				break;
 			case NAVIGATION_STATE_AUTO_LANDENGFAIL:
+				_pos_sp_triplet_published_invalid_once = false;
 				_navigation_mode = &_engineFailure;
 				break;
 			case NAVIGATION_STATE_AUTO_LANDGPSFAIL:
+				_pos_sp_triplet_published_invalid_once = false;
 				_navigation_mode = &_gpsFailure;
 				break;
 			default:
@@ -467,9 +476,9 @@ Navigator::task_main()
 			_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
 		}

-		/* if nothing is running, set position setpoint triplet invalid */
-		if (_navigation_mode == nullptr) {
-			// TODO publish empty sp only once
+		/* if nothing is running, set position setpoint triplet invalid once */
+		if (_navigation_mode == nullptr && !_pos_sp_triplet_published_invalid_once) {
+			_pos_sp_triplet_published_invalid_once = true;
 			_pos_sp_triplet.previous.valid = false;
 			_pos_sp_triplet.current.valid = false;
 			_pos_sp_triplet.next.valid = false;
@@ -497,8 +506,8 @@ Navigator::start()
 	/* start the task */
 	_navigator_task = task_spawn_cmd("navigator",
 					 SCHED_DEFAULT,
-					 SCHED_PRIORITY_MAX - 5,
-					 2000,
+					 SCHED_PRIORITY_DEFAULT + 20,
+					 1800,
 					 (main_t)&Navigator::task_main_trampoline,
 					 nullptr);

@@ -630,9 +639,6 @@ Navigator::publish_mission_result()
 		/* advertise and publish */
 		_mission_result_pub = orb_advertise(ORB_ID(mission_result), &_mission_result);
 	}
-	/* reset reached bool */
-	_mission_result.reached = false;
-	_mission_result.finished = false;
 }

 void
@@ -163,6 +163,7 @@ RCLoss::advance_rcl()
 			_rcl_state = RCL_STATE_TERMINATE;
 			_navigator->get_mission_result()->stay_in_failsafe = true;
 			_navigator->publish_mission_result();
+			reset_mission_item_reached();
 		}
 		break;
 	case RCL_STATE_LOITER:
@@ -171,6 +172,7 @@ RCLoss::advance_rcl()
 		mavlink_log_info(_navigator->get_mavlink_fd(), "#audio: RC not regained, terminating");
 		_navigator->get_mission_result()->stay_in_failsafe = true;
 		_navigator->publish_mission_result();
+		reset_mission_item_reached();
 		break;
 	case RCL_STATE_TERMINATE:
 		warnx("rcl end");
@@ -161,7 +161,7 @@ int position_estimator_inav_main(int argc, char *argv[])
 			thread_should_exit = true;

 		} else {
-			warnx("app not started");
+			warnx("not started");
 		}

 		exit(0);
@@ -169,10 +169,10 @@ int position_estimator_inav_main(int argc, char *argv[])

 	if (!strcmp(argv[1], "status")) {
 		if (thread_running) {
-			warnx("app is running");
+			warnx("is running");

 		} else {
-			warnx("app not started");
+			warnx("not started");
 		}

 		exit(0);
@@ -210,10 +210,8 @@ static void write_debug_log(const char *msg, float dt, float x_est[2], float y_e
 ****************************************************************************/
 int position_estimator_inav_thread_main(int argc, char *argv[])
 {
-	warnx("started");
 	int mavlink_fd;
 	mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
-	mavlink_log_info(mavlink_fd, "[inav] started");

 	float x_est[2] = { 0.0f, 0.0f };	// pos, vel
 	float y_est[2] = { 0.0f, 0.0f };	// pos, vel
@@ -389,8 +387,8 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
 					} else {
 						wait_baro = false;
 						baro_offset /= (float) baro_init_cnt;
-						warnx("baro offs: %.2f", (double)baro_offset);
-						mavlink_log_info(mavlink_fd, "[inav] baro offs: %.2f", (double)baro_offset);
+						warnx("baro offs: %d", (int)baro_offset);
+						mavlink_log_info(mavlink_fd, "[inav] baro offs: %d", (int)baro_offset);
 						local_pos.z_valid = true;
 						local_pos.v_z_valid = true;
 					}
@@ -520,7 +518,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
 							sonar_valid_time = t;
 							sonar_valid = true;
 							local_pos.surface_bottom_timestamp = t;
-							mavlink_log_info(mavlink_fd, "[inav] new surface level: %.2f", (double)surface_offset);
+							mavlink_log_info(mavlink_fd, "[inav] new surface level: %d", (int)surface_offset);
 						}

 					} else {
@@ -722,8 +720,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[])

 							/* initialize projection */
 							map_projection_init(&ref, lat, lon);
-							warnx("init ref: lat=%.7f, lon=%.7f, alt=%.2f", (double)lat, (double)lon, (double)alt);
-							mavlink_log_info(mavlink_fd, "[inav] init ref: %.7f, %.7f, %.2f", (double)lat, (double)lon, (double)alt);
+							// XXX replace this print
+							warnx("init ref: lat=%.7f, lon=%.7f, alt=%8.4f", (double)lat, (double)lon, (double)alt);
+							mavlink_log_info(mavlink_fd, "[inav] init ref: %.7f, %.7f, %8.4f", (double)lat, (double)lon, (double)alt);
 						}
 					}

@@ -41,6 +41,7 @@
 #include <stdbool.h>

 #include <drivers/drv_hrt.h>
+#include <drivers/drv_rc_input.h>
 #include <systemlib/perf_counter.h>
 #include <systemlib/ppm_decode.h>
 #include <rc/st24.h>
@@ -70,7 +71,6 @@ bool dsm_port_input(uint16_t *rssi, bool *dsm_updated, bool *st24_updated)
 	uint8_t *bytes;
 	*dsm_updated = dsm_input(r_raw_rc_values, &temp_count, &n_bytes, &bytes);
 	if (*dsm_updated) {
-		r_raw_rc_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
 		r_raw_rc_count = temp_count & 0x7fff;
 		if (temp_count & 0x8000)
 			r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_RC_DSM11;
@@ -91,6 +91,7 @@ bool dsm_port_input(uint16_t *rssi, bool *dsm_updated, bool *st24_updated)

 	for (unsigned i = 0; i < n_bytes; i++) {
 		/* set updated flag if one complete packet was parsed */
+		st24_rssi = RC_INPUT_RSSI_MAX;
 		*st24_updated |= (OK == st24_decode(bytes[i], &st24_rssi, &rx_count,
 					&st24_channel_count, r_raw_rc_values, PX4IO_RC_INPUT_CHANNELS));
 	}
@@ -170,6 +171,12 @@ controls_tick() {
 	perf_begin(c_gather_dsm);
 	bool dsm_updated, st24_updated;
 	(void)dsm_port_input(&rssi, &dsm_updated, &st24_updated);
+	if (dsm_updated) {
+		r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
+	}
+	if (st24_updated) {
+		r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_ST24;
+	}
 	perf_end(c_gather_dsm);

 	perf_begin(c_gather_sbus);
@@ -417,6 +424,15 @@ controls_tick() {
 		if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && (REG_TO_SIGNED(rc_value_override) < RC_CHANNEL_LOW_THRESH))
 			override = true;

+		/*
+		  if the FMU is dead then enable override if we have a
+		  mixer and OVERRIDE_IMMEDIATE is set
+		 */
+		if (!(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) &&
+		    (r_setup_arming & PX4IO_P_SETUP_ARMING_OVERRIDE_IMMEDIATE) &&
+		    (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK))
+			override = true;                
+
 		if (override) {

 			r_status_flags |= PX4IO_P_STATUS_FLAGS_OVERRIDE;
@@ -353,12 +353,16 @@ static unsigned mixer_text_length = 0;
 int
 mixer_handle_text(const void *buffer, size_t length)
 {
-	/* do not allow a mixer change while safety off */
-	if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)) {
+	/* do not allow a mixer change while safety off and FMU armed */
+	if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) &&
+		(r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED)) {
 		return 1;
 	}

-	/* abort if we're in the mixer */
+	/* disable mixing, will be enabled once load is complete */
+	r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_MIXER_OK);
+
+	/* abort if we're in the mixer - the caller is expected to retry */
 	if (in_mixer) {
 		return 1;
 	}
@@ -367,17 +371,16 @@ mixer_handle_text(const void *buffer, size_t length)

 	isr_debug(2, "mix txt %u", length);

-	if (length < sizeof(px4io_mixdata))
+	if (length < sizeof(px4io_mixdata)) {
 		return 0;
+	}

-	unsigned	text_length = length - sizeof(px4io_mixdata);
+	unsigned text_length = length - sizeof(px4io_mixdata);

 	switch (msg->action) {
 	case F2I_MIXER_ACTION_RESET:
 		isr_debug(2, "reset");

-		/* FIRST mark the mixer as invalid */
-		r_status_flags &= ~PX4IO_P_STATUS_FLAGS_MIXER_OK;
 		/* THEN actually delete it */
 		mixer_group.reset();
 		mixer_text_length = 0;
@@ -386,9 +389,6 @@ mixer_handle_text(const void *buffer, size_t length)
 	case F2I_MIXER_ACTION_APPEND:
 		isr_debug(2, "append %d", length);

-		/* disable mixing during the update */
-		r_status_flags &= ~PX4IO_P_STATUS_FLAGS_MIXER_OK;
-
 		/* check for overflow - this would be really fatal */
 		if ((mixer_text_length + text_length + 1) > sizeof(mixer_text)) {
 			r_status_flags &= ~PX4IO_P_STATUS_FLAGS_MIXER_OK;
@@ -183,6 +183,7 @@
 #define PX4IO_P_SETUP_ARMING_LOCKDOWN		(1 << 7) /* If set, the system operates normally, but won't actuate any servos */
 #define PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE	(1 << 8) /* If set, the system will always output the failsafe values */
 #define PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE	(1 << 9) /* If set, the system will never return from a failsafe, but remain in failsafe once triggered. */
+#define PX4IO_P_SETUP_ARMING_OVERRIDE_IMMEDIATE	(1 << 10) /* If set then on FMU failure override is immediate. Othewise it waits for the mode switch to go past the override thrshold */

 #define PX4IO_P_SETUP_PWM_RATES			2	/* bitmask, 0 = low rate, 1 = high rate */
 #define PX4IO_P_SETUP_PWM_DEFAULTRATE		3	/* 'low' PWM frame output rate in Hz */
@@ -85,6 +85,9 @@ static volatile uint8_t msg_next_out, msg_next_in;
 #define NUM_MSG 2
 static char msg[NUM_MSG][40];

+static void heartbeat_blink(void);
+static void ring_blink(void);
+
 /*
 * add a debug message to be printed on the console
 */
@@ -126,6 +129,65 @@ heartbeat_blink(void)
 	LED_BLUE(heartbeat = !heartbeat);
 }

+static void
+ring_blink(void)
+{
+#ifdef GPIO_LED4
+
+	if (/* IO armed */ (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)
+	/* and FMU is armed */ && (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED)) {
+		LED_RING(1);
+		return;
+	}
+
+	// XXX this led code does have
+	// intentionally a few magic numbers.
+	const unsigned max_brightness = 118;
+
+	static unsigned counter = 0;
+	static unsigned brightness = max_brightness;
+	static unsigned brightness_counter = 0;
+	static unsigned on_counter = 0;
+
+	if (brightness_counter < max_brightness) {
+
+		bool on = ((on_counter * 100) / brightness_counter+1) <= ((brightness * 100) / max_brightness+1);
+
+		// XXX once led is PWM driven,
+		// remove the ! in the line below
+		// to return to the proper breathe
+		// animation / pattern (currently inverted)
+		LED_RING(!on);
+		brightness_counter++;
+
+		if (on) {
+			on_counter++;
+		}
+
+	} else {
+
+		if (counter >= 62) {
+			counter = 0;
+		}
+
+		int n;
+
+		if (counter < 32) {
+			n = counter;
+
+		} else {
+			n = 62 - counter;
+		}
+
+		brightness = (n * n) / 8;
+		brightness_counter = 0;
+		on_counter = 0;
+		counter++;
+	}
+
+#endif
+}
+
 static uint64_t reboot_time;

 /**
@@ -191,6 +253,9 @@ user_start(int argc, char *argv[])
 	LED_AMBER(false);
 	LED_BLUE(false);
 	LED_SAFETY(false);
+#ifdef GPIO_LED4
+	LED_RING(false);
+#endif

 	/* turn on servo power (if supported) */
 #ifdef POWER_SERVO
@@ -294,6 +359,8 @@ user_start(int argc, char *argv[])
                    heartbeat_blink();
                }

+		ring_blink();
+
                check_reboot();

 		/* check for debug activity (default: none) */
@@ -140,6 +140,7 @@ extern pwm_limit_t pwm_limit;
 #define LED_BLUE(_s)			stm32_gpiowrite(GPIO_LED1, !(_s))
 #define LED_AMBER(_s)			stm32_gpiowrite(GPIO_LED2, !(_s))
 #define LED_SAFETY(_s)			stm32_gpiowrite(GPIO_LED3, !(_s))
+#define LED_RING(_s)			stm32_gpiowrite(GPIO_LED4, (_s))

 #ifdef CONFIG_ARCH_BOARD_PX4IO_V1

@@ -191,7 +191,8 @@ volatile uint16_t	r_page_setup[] =
 					 PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED | \
 					 PX4IO_P_SETUP_ARMING_LOCKDOWN | \
 					 PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE | \
-					 PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE)
+					 PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE | \
+					 PX4IO_P_SETUP_ARMING_OVERRIDE_IMMEDIATE)
 #define PX4IO_P_SETUP_RATES_VALID	((1 << PX4IO_SERVO_COUNT) - 1)
 #define PX4IO_P_SETUP_RELAYS_VALID	((1 << PX4IO_RELAY_CHANNELS) - 1)

@@ -406,11 +407,11 @@ registers_set(uint8_t page, uint8_t offset, const uint16_t *values, unsigned num

 		/* handle text going to the mixer parser */
 	case PX4IO_PAGE_MIXERLOAD:
-		if (!(r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) ||
-				    (r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) {
-			return mixer_handle_text(values, num_values * sizeof(*values));
-		}
-		break;
+		/* do not change the mixer if FMU is armed and IO's safety is off
+		 * this state defines an active system. This check is done in the
+		 * text handling function.
+		 */
+		return mixer_handle_text(values, num_values * sizeof(*values));

 	default:
 		/* avoid offset wrap */
@@ -582,8 +583,7 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
 			break;

 		case PX4IO_P_SETUP_REBOOT_BL:
-			if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) ||
-			    (r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) {
+			if (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) {
 				// don't allow reboot while armed
 				break;
 			}
@@ -629,10 +629,9 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
 	case PX4IO_PAGE_RC_CONFIG: {

 		/**
-		 * do not allow a RC config change while outputs armed
+		 * do not allow a RC config change while safety is off
 		 */
-		if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) ||
-			    (r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) {
+		if (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) {
 			break;
 		}

@@ -57,6 +57,7 @@
 #define SBUS_FLAGS_BYTE		23
 #define SBUS_FAILSAFE_BIT	3
 #define SBUS_FRAMELOST_BIT	2
+#define SBUS1_FRAME_DELAY	14000

 /*
  Measured values with Futaba FX-30/R6108SB:
@@ -80,6 +81,7 @@ static int sbus_fd = -1;

 static hrt_abstime last_rx_time;
 static hrt_abstime last_frame_time;
+static hrt_abstime last_txframe_time = 0;

 static uint8_t	frame[SBUS_FRAME_SIZE];

@@ -122,10 +124,42 @@ sbus_init(const char *device)
 void
 sbus1_output(uint16_t *values, uint16_t num_values)
 {
-	char a = 'A';
-	write(sbus_fd, &a, 1);
-}
+	uint8_t byteindex = 1; /*Data starts one byte into the sbus frame. */
+	uint8_t offset = 0;
+	uint16_t value;
+	hrt_abstime now;

+	now = hrt_absolute_time();
+
+	if ((now - last_txframe_time) > SBUS1_FRAME_DELAY) {
+		last_txframe_time = now;
+		uint8_t	oframe[SBUS_FRAME_SIZE] = { 0x0f };
+
+		/* 16 is sbus number of servos/channels minus 2 single bit channels.
+		* currently ignoring single bit channels.  */
+
+		for (unsigned i = 0; (i < num_values) && (i < 16); ++i) {
+			value = (uint16_t)(((values[i] - SBUS_SCALE_OFFSET) / SBUS_SCALE_FACTOR) + .5f);
+
+			/*protect from out of bounds values and limit to 11 bits*/
+			if (value > 0x07ff ) {
+				value = 0x07ff;
+			}
+
+			while (offset >= 8) {
+				++byteindex;
+				offset -= 8;
+			}
+
+			oframe[byteindex] |= (value << (offset)) & 0xff;
+			oframe[byteindex + 1] |= (value >> (8 - offset)) & 0xff;
+			oframe[byteindex + 2] |= (value >> (16 - offset)) & 0xff;
+			offset += 11;
+		}
+
+		write(sbus_fd, oframe, SBUS_FRAME_SIZE);
+	}
+}
 void
 sbus2_output(uint16_t *values, uint16_t num_values)
 {
@@ -43,3 +43,5 @@ SRCS = sdlog2.c \
       logbuffer.c

 MODULE_STACKSIZE = 1200
+
+MAXOPTIMIZATION	 = -Os
@@ -90,6 +90,7 @@
 #include <uORB/topics/system_power.h>
 #include <uORB/topics/servorail_status.h>
 #include <uORB/topics/wind_estimate.h>
+#include <uORB/topics/encoders.h>

 #include <systemlib/systemlib.h>
 #include <systemlib/param/param.h>
@@ -495,6 +496,8 @@ static void *logwriter_thread(void *arg)
 	/* set name */
 	prctl(PR_SET_NAME, "sdlog2_writer", 0);

+	perf_counter_t perf_write = perf_alloc(PC_ELAPSED, "sd write");
+
 	int log_fd = open_log_file();

 	if (log_fd < 0) {
@@ -552,7 +555,9 @@ static void *logwriter_thread(void *arg)
 				n = available;
 			}

+			perf_begin(perf_write);
 			n = write(log_fd, read_ptr, n);
+			perf_end(perf_write);

 			should_wait = (n == available) && !is_part;

@@ -585,6 +590,9 @@ static void *logwriter_thread(void *arg)
 	fsync(log_fd);
 	close(log_fd);

+	/* free performance counter */
+	perf_free(perf_write);
+
 	return NULL;
 }

@@ -954,6 +962,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 		struct servorail_status_s servorail_status;
 		struct satellite_info_s sat_info;
 		struct wind_estimate_s wind_estimate;
+		struct encoders_s encoders;
 	} buf;

 	memset(&buf, 0, sizeof(buf));
@@ -996,6 +1005,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 			struct log_GS1B_s log_GS1B;
 			struct log_TECS_s log_TECS;
 			struct log_WIND_s log_WIND;
+			struct log_ENCD_s log_ENCD;
 		} body;
 	} log_msg = {
 		LOG_PACKET_HEADER_INIT(0)
@@ -1033,6 +1043,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 		int system_power_sub;
 		int servorail_status_sub;
 		int wind_sub;
+		int encoders_sub;
 	} subs;

 	subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command));
@@ -1064,7 +1075,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 	subs.wind_sub = orb_subscribe(ORB_ID(wind_estimate));
 	/* we need to rate-limit wind, as we do not need the full update rate */
 	orb_set_interval(subs.wind_sub, 90);
-
+	subs.encoders_sub = orb_subscribe(ORB_ID(encoders));

 	/* add new topics HERE */

@@ -1670,6 +1681,16 @@ int sdlog2_thread_main(int argc, char *argv[])
 			LOGBUFFER_WRITE_AND_COUNT(WIND);
 		}

+		/* --- ENCODERS --- */
+		if (copy_if_updated(ORB_ID(encoders), subs.encoders_sub, &buf.encoders)) {
+			log_msg.msg_type = LOG_ENCD_MSG;
+			log_msg.body.log_ENCD.cnt0 = buf.encoders.counts[0];
+			log_msg.body.log_ENCD.vel0 = buf.encoders.velocity[0];
+			log_msg.body.log_ENCD.cnt1 = buf.encoders.counts[1];
+			log_msg.body.log_ENCD.vel1 = buf.encoders.velocity[1];
+			LOGBUFFER_WRITE_AND_COUNT(ENCD);
+		}
+
 		/* signal the other thread new data, but not yet unlock */
 		if (logbuffer_count(&lb) > MIN_BYTES_TO_WRITE) {
 			/* only request write if several packets can be written at once */
@@ -413,6 +413,16 @@ struct log_VISN_s {
 	float qw;
 };

+/* --- ENCODERS - ENCODER DATA --- */
+#define LOG_ENCD_MSG 39
+struct log_ENCD_s {
+	int64_t cnt0;
+	float vel0;
+	int64_t cnt1;
+	float vel1;
+};
+
+
 /********** SYSTEM MESSAGES, ID > 0x80 **********/

 /* --- TIME - TIME STAMP --- */
@@ -477,6 +487,7 @@ static const struct log_format_s log_formats[] = {
 	LOG_FORMAT(GS1B, "BBBBBBBBBBBBBBBB",	"s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"),
 	LOG_FORMAT(TECS, "fffffffffffffB",	"ASP,AF,FSP,F,FF,AsSP,AsF,AsDSP,AsD,TERSP,TER,EDRSP,EDR,M"),
 	LOG_FORMAT(WIND, "ffff",	"X,Y,CovX,CovY"),
+	LOG_FORMAT(ENCD, "qfqf",	"cnt0,vel0,cnt1,vel1"),

 	/* system-level messages, ID >= 0x80 */
 	/* FMT: don't write format of format message, it's useless */
@@ -42,3 +42,5 @@ SRCS		= sensors.cpp \
 		  sensor_params.c

 MODULE_STACKSIZE = 1200
+
+MAXOPTIMIZATION	 = -Os
@@ -0,0 +1,109 @@
+/****************************************************************************
+ *
+ *   Copyright (c) 2014 PX4 Development Team. All rights reserved.
+ *
+ * Redistribution and use in source and binary forms, with or without
+ * modification, are permitted provided that the following conditions
+ * are met:
+ *
+ * 1. Redistributions of source code must retain the above copyright
+ *    notice, this list of conditions and the following disclaimer.
+ * 2. Redistributions in binary form must reproduce the above copyright
+ *    notice, this list of conditions and the following disclaimer in
+ *    the documentation and/or other materials provided with the
+ *    distribution.
+ * 3. Neither the name PX4 nor the names of its contributors may be
+ *    used to endorse or promote products derived from this software
+ *    without specific prior written permission.
+ *
+ * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
+ * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
+ * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
+ * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
+ * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
+ * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
+ * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
+ * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
+ * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
+ * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
+ * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
+ * POSSIBILITY OF SUCH DAMAGE.
+ *
+ ****************************************************************************/
+
+/**
+ * @file mcu_version.c
+ * 
+ * Read out the microcontroller version from the board
+ *
+ * @author Lorenz Meier <lorenz@px4.io>
+ *
+ */
+
+#include "mcu_version.h"
+
+#include <nuttx/config.h>
+
+#ifdef CONFIG_ARCH_CHIP_STM32
+#include <up_arch.h>
+
+#define DBGMCU_IDCODE	0xE0042000
+
+#define STM32F40x_41x	0x413
+#define STM32F42x_43x	0x419
+
+#define REVID_MASK	0xFFFF0000
+#define DEVID_MASK	0xFFF
+
+#endif
+
+
+
+int mcu_version(char* rev, char** revstr)
+{
+#ifdef CONFIG_ARCH_CHIP_STM32
+	uint32_t abc = getreg32(DBGMCU_IDCODE);
+
+	int32_t chip_version = abc & DEVID_MASK;
+	enum MCU_REV revid = (abc & REVID_MASK) >> 16;
+
+	switch (chip_version) {
+	case STM32F40x_41x:
+		*revstr = "STM32F40x";
+		break;
+	case STM32F42x_43x:
+		*revstr = "STM32F42x";
+		break;
+	default:
+		*revstr = "STM32F???";
+		break;
+	}
+
+	switch (revid) {
+
+		case MCU_REV_STM32F4_REV_A:
+			*rev = 'A';
+			break;
+		case MCU_REV_STM32F4_REV_Z:
+			*rev = 'Z';
+			break;
+		case MCU_REV_STM32F4_REV_Y:
+			*rev = 'Y';
+			break;
+		case MCU_REV_STM32F4_REV_1:
+			*rev = '1';
+			break;
+		case MCU_REV_STM32F4_REV_3:
+			*rev = '3';
+			break;
+		default:
+			*rev = '?';
+			revid = -1;
+			break;
+	}
+
+	return revid;
+#else
+	return -1;
+#endif
+}
@@ -0,0 +1,52 @@
+/****************************************************************************
+ *
+ *   Copyright (c) 2014 PX4 Development Team. All rights reserved.
+ *
+ * Redistribution and use in source and binary forms, with or without
+ * modification, are permitted provided that the following conditions
+ * are met:
+ *
+ * 1. Redistributions of source code must retain the above copyright
+ *    notice, this list of conditions and the following disclaimer.
+ * 2. Redistributions in binary form must reproduce the above copyright
+ *    notice, this list of conditions and the following disclaimer in
+ *    the documentation and/or other materials provided with the
+ *    distribution.
+ * 3. Neither the name PX4 nor the names of its contributors may be
+ *    used to endorse or promote products derived from this software
+ *    without specific prior written permission.
+ *
+ * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
+ * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
+ * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
+ * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
+ * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
+ * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
+ * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
+ * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
+ * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
+ * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
+ * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
+ * POSSIBILITY OF SUCH DAMAGE.
+ *
+ ****************************************************************************/
+
+#pragma once
+
+/* magic numbers from reference manual */
+enum MCU_REV {
+	MCU_REV_STM32F4_REV_A = 0x1000,
+	MCU_REV_STM32F4_REV_Z = 0x1001,
+	MCU_REV_STM32F4_REV_Y = 0x1003,
+	MCU_REV_STM32F4_REV_1 = 0x1007,
+	MCU_REV_STM32F4_REV_3 = 0x2001
+};
+
+/**
+ * Reports the microcontroller version of the main CPU.
+ *
+ * @param rev The silicon revision character
+ * @param revstr The full chip name string
+ * @return The silicon revision / version number as integer
+ */
+__EXPORT int mcu_version(char* rev, char** revstr);
@@ -91,6 +91,7 @@ int load_mixer_file(const char *fname, char *buf, unsigned maxlen)
 		/* if the line is too long to fit in the buffer, bail */
 		if ((strlen(line) + strlen(buf) + 1) >= maxlen) {
 			warnx("line too long");
+			fclose(fp);
 			return -1;
 		}

@@ -98,6 +99,7 @@ int load_mixer_file(const char *fname, char *buf, unsigned maxlen)
 		strcat(buf, line);
 	}

+	fclose(fp);
 	return 0;
 }

@@ -53,5 +53,7 @@ SRCS		 = err.c \
 		   otp.c \
 		   board_serial.c \
 		   pwm_limit/pwm_limit.c \
-		   circuit_breaker.c
+		   circuit_breaker.c \
+		   mcu_version.c

+MAXOPTIMIZATION	 = -Os
@@ -46,6 +46,7 @@
 #include "topics/vehicle_attitude_setpoint.h"
 #include "topics/vehicle_rates_setpoint.h"
 #include "topics/actuator_outputs.h"
+#include "topics/actuator_direct.h"
 #include "topics/encoders.h"
 #include "topics/tecs_status.h"

@@ -76,6 +77,7 @@ template class __EXPORT Publication<vehicle_global_velocity_setpoint_s>;
 template class __EXPORT Publication<vehicle_attitude_setpoint_s>;
 template class __EXPORT Publication<vehicle_rates_setpoint_s>;
 template class __EXPORT Publication<actuator_outputs_s>;
+template class __EXPORT Publication<actuator_direct_s>;
 template class __EXPORT Publication<encoders_s>;
 template class __EXPORT Publication<tecs_status_s>;

@@ -44,3 +44,5 @@ SRCS			= uORB.cpp \
 			  objects_common.cpp \
 			  Publication.cpp \
 			  Subscription.cpp
+
+MAXOPTIMIZATION	 = -Os
@@ -192,6 +192,9 @@ ORB_DEFINE(actuator_outputs_1, struct actuator_outputs_s);
 ORB_DEFINE(actuator_outputs_2, struct actuator_outputs_s);
 ORB_DEFINE(actuator_outputs_3, struct actuator_outputs_s);

+#include "topics/actuator_direct.h"
+ORB_DEFINE(actuator_direct, struct actuator_direct_s);
+
 #include "topics/multirotor_motor_limits.h"
 ORB_DEFINE(multirotor_motor_limits, struct multirotor_motor_limits_s);

@@ -0,0 +1,69 @@
+/****************************************************************************
+ *
+ *   Copyright (C) 2012 PX4 Development Team. All rights reserved.
+ *
+ * Redistribution and use in source and binary forms, with or without
+ * modification, are permitted provided that the following conditions
+ * are met:
+ *
+ * 1. Redistributions of source code must retain the above copyright
+ *    notice, this list of conditions and the following disclaimer.
+ * 2. Redistributions in binary form must reproduce the above copyright
+ *    notice, this list of conditions and the following disclaimer in
+ *    the documentation and/or other materials provided with the
+ *    distribution.
+ * 3. Neither the name PX4 nor the names of its contributors may be
+ *    used to endorse or promote products derived from this software
+ *    without specific prior written permission.
+ *
+ * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
+ * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
+ * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
+ * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
+ * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
+ * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
+ * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
+ * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
+ * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
+ * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
+ * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
+ * POSSIBILITY OF SUCH DAMAGE.
+ *
+ ****************************************************************************/
+
+/**
+ * @file actuator_direct.h
+ *
+ * Actuator direct values.
+ *
+ * Values published to this topic are the direct actuator values which
+ * should be passed to actuators, bypassing mixing
+ */
+
+#ifndef TOPIC_ACTUATOR_DIRECT_H
+#define TOPIC_ACTUATOR_DIRECT_H
+
+#include <stdint.h>
+#include "../uORB.h"
+
+#define NUM_ACTUATORS_DIRECT		16
+
+/**
+ * @addtogroup topics
+ * @{
+ */
+
+struct actuator_direct_s {
+	uint64_t timestamp;				/**< timestamp in us since system boot */
+	float values[NUM_ACTUATORS_DIRECT];		/**< actuator values, from -1 to 1 */
+	unsigned nvalues;				/**< number of valid values */
+};
+
+/**
+ * @}
+ */
+
+/* actuator direct ORB */
+ORB_DECLARE(actuator_direct);
+
+#endif // TOPIC_ACTUATOR_DIRECT_H
@@ -47,7 +47,7 @@
 * Switch position
 */
 typedef enum {
-	SWITCH_POS_NONE = 0,	/**< switch is not mapped */
+	SWITCH_POS_NONE = 0,		/**< switch is not mapped */
 	SWITCH_POS_ON,			/**< switch activated (value = 1) */
 	SWITCH_POS_MIDDLE,		/**< middle position (value = 0) */
 	SWITCH_POS_OFF			/**< switch not activated (value = -1) */
@@ -93,13 +93,13 @@ struct manual_control_setpoint_s {
 	float aux4;			/**< default function: camera roll */
 	float aux5;			/**< default function: payload drop */

-	switch_pos_t mode_switch;			/**< main mode 3 position switch (mandatory): _MANUAL_, ASSIST, AUTO */
-	switch_pos_t return_switch;			/**< return to launch 2 position switch (mandatory): _NORMAL_, RTL */
-	switch_pos_t posctl_switch;			/**< position control 2 position switch (optional): _ALTCTL_, POSCTL */
-	switch_pos_t loiter_switch;			/**< loiter 2 position switch (optional): _MISSION_, LOITER */
-	switch_pos_t acro_switch;			/**< acro 2 position switch (optional): _MANUAL_, ACRO */
-	switch_pos_t offboard_switch;		/**< offboard 2 position switch (optional): _NORMAL_, OFFBOARD */
-}; /**< manual control inputs */
+	switch_pos_t mode_switch;	/**< main mode 3 position switch (mandatory): _MANUAL_, ASSIST, AUTO */
+	switch_pos_t return_switch;	/**< return to launch 2 position switch (mandatory): _NORMAL_, RTL */
+	switch_pos_t posctl_switch;	/**< position control 2 position switch (optional): _ALTCTL_, POSCTL */
+	switch_pos_t loiter_switch;	/**< loiter 2 position switch (optional): _MISSION_, LOITER */
+	switch_pos_t acro_switch;	/**< acro 2 position switch (optional): _MANUAL_, ACRO */
+	switch_pos_t offboard_switch;	/**< offboard 2 position switch (optional): _NORMAL_, OFFBOARD */
+};

 /**
 * @}
@@ -34,6 +34,8 @@
 /**
 * @file rc_channels.h
 * Definition of the rc_channels uORB topic.
+ *
+ * @deprecated DO NOT USE FOR NEW CODE
 */

 #ifndef RC_CHANNELS_H_
@@ -63,10 +65,13 @@ enum RC_CHANNELS_FUNCTION {
 	AUX_2,
 	AUX_3,
 	AUX_4,
-	AUX_5,
-	RC_CHANNELS_FUNCTION_MAX /**< Indicates the number of functions. There can be more functions than RC channels. */
+	AUX_5
 };

+// MAXIMUM FUNCTIONS IS != MAXIMUM RC INPUT CHANNELS
+
+#define RC_CHANNELS_FUNCTION_MAX 18
+
 /**
 * @addtogroup topics
 * @{
@@ -76,7 +81,6 @@ struct rc_channels_s {
 	uint64_t timestamp_last_valid;						/**< Timestamp of last valid RC signal */
 	float channels[RC_CHANNELS_FUNCTION_MAX];			/**< Scaled to -1..1 (throttle: 0..1) */
 	uint8_t channel_count;								/**< Number of valid channels */
-	char function_name[RC_CHANNELS_FUNCTION_MAX][20];	/**< String array to store the names of the functions */
 	int8_t function[RC_CHANNELS_FUNCTION_MAX];			/**< Functions mapping */
 	uint8_t rssi;										/**< Receive signal strength index */
 	bool signal_lost;									/**< Control signal lost, should be checked together with topic timeout */
@@ -57,7 +57,7 @@
 struct test_motor_s {
 	uint64_t 	timestamp;				/**< output timestamp in us since system boot */
 	unsigned 	motor_number;				/**< number of motor to spin */
-	float		value;					/**< output data, in natural output units */
+	float		value;					/**< output power, range [0..1] */
 };

 /**
@@ -108,7 +108,7 @@ typedef enum {
 	NAVIGATION_STATE_AUTO_LANDGPSFAIL,	/**< Auto land on gps failure (e.g. open loop loiter down) */
 	NAVIGATION_STATE_ACRO,			/**< Acro mode */
 	NAVIGATION_STATE_LAND,			/**< Land mode */
-	NAVIGATION_STATE_DESCEND,			/**< Descend mode (no position control) */
+	NAVIGATION_STATE_DESCEND,		/**< Descend mode (no position control) */
 	NAVIGATION_STATE_TERMINATION,		/**< Termination mode */
 	NAVIGATION_STATE_OFFBOARD,
 	NAVIGATION_STATE_MAX,
@@ -201,6 +201,7 @@ struct vehicle_status_s {

 	bool rc_signal_found_once;
 	bool rc_signal_lost;				/**< true if RC reception lost */
+	uint64_t rc_signal_lost_timestamp;		/**< Time at which the RC reception was lost */
 	bool rc_signal_lost_cmd;				/**< true if RC lost mode is commanded */
 	bool rc_input_blocked;				/**< set if RC input should be ignored */

@@ -40,6 +40,9 @@
 #include "esc.hpp"
 #include <systemlib/err.h>

+
+#define MOTOR_BIT(x) (1<<(x))
+
 UavcanEscController::UavcanEscController(uavcan::INode &node) :
 	_node(node),
 	_uavcan_pub_raw_cmd(node),
@@ -73,7 +76,9 @@ int UavcanEscController::init()

 void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
 {
-	if ((outputs == nullptr) || (num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize)) {
+	if ((outputs == nullptr) || 
+            (num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize) ||
+            (num_outputs > CONNECTED_ESC_MAX)) {
 		perf_count(_perfcnt_invalid_input);
 		return;
 	}
@@ -95,14 +100,18 @@ void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)

 	static const int cmd_max = uavcan::equipment::esc::RawCommand::FieldTypes::cmd::RawValueType::max();

-	if (_armed) {
-		for (unsigned i = 0; i < num_outputs; i++) {
-
+	for (unsigned i = 0; i < num_outputs; i++) {
+		if (_armed_mask & MOTOR_BIT(i)) {
 			float scaled = (outputs[i] + 1.0F) * 0.5F * cmd_max;
-			if (scaled < 1.0F) {
-				scaled = 1.0F;  // Since we're armed, we don't want to stop it completely
-			}
-
+                        // trim negative values back to 0. Previously
+                        // we set this to 0.1, which meant motors kept
+                        // spinning when armed, but that should be a
+                        // policy decision for a specific vehicle
+                        // type, as it is not appropriate for all
+                        // types of vehicles (eg. fixed wing).
+			if (scaled < 0.0F) {
+				scaled = 0.0F;
+                        }
 			if (scaled > cmd_max) {
 				scaled = cmd_max;
 				perf_count(_perfcnt_scaling_error);
@@ -111,6 +120,8 @@ void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
 			msg.cmd.push_back(static_cast<int>(scaled));

 			_esc_status.esc[i].esc_setpoint_raw = abs(static_cast<int>(scaled));
+		} else {
+			msg.cmd.push_back(static_cast<unsigned>(0));
 		}
 	}

@@ -121,9 +132,22 @@ void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
 	(void)_uavcan_pub_raw_cmd.broadcast(msg);
 }

-void UavcanEscController::arm_esc(bool arm)
+void UavcanEscController::arm_all_escs(bool arm)
 {
-	_armed = arm;
+	if (arm) {
+		_armed_mask = -1;
+	} else {
+		_armed_mask = 0;
+	}
+}
+
+void UavcanEscController::arm_single_esc(int num, bool arm)
+{
+	if (arm) {
+		_armed_mask = MOTOR_BIT(num);
+	} else {
+		_armed_mask = 0;
+	}
 }

 void UavcanEscController::esc_status_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::esc::Status> &msg)
@@ -61,7 +61,8 @@ public:

 	void update_outputs(float *outputs, unsigned num_outputs);

-	void arm_esc(bool arm);
+	void arm_all_escs(bool arm);
+	void arm_single_esc(int num, bool arm);

 private:
 	/**
@@ -98,6 +99,11 @@ private:
 	uavcan::Subscriber<uavcan::equipment::esc::Status, StatusCbBinder>	_uavcan_sub_status;
 	uavcan::TimerEventForwarder<TimerCbBinder>				_orb_timer;

+	/*
+	 * ESC states
+	 */
+	uint32_t 			_armed_mask = 0;
+
 	/*
 	 * Perf counters
 	 */
@@ -91,11 +91,7 @@ void UavcanBarometerBridge::air_data_sub_cb(const uavcan::ReceivedDataStructure<
 {
 	auto report = ::baro_report();

-	report.timestamp = msg.getUtcTimestamp().toUSec();
-	if (report.timestamp == 0) {
-		report.timestamp = msg.getMonotonicTimestamp().toUSec();
-	}
-
+	report.timestamp   = msg.getMonotonicTimestamp().toUSec();
 	report.temperature = msg.static_temperature;
 	report.pressure    = msg.static_pressure / 100.0F;  // Convert to millibar

@@ -92,7 +92,7 @@ void UavcanGnssBridge::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavca

 	auto report = ::vehicle_gps_position_s();

-	report.timestamp_position = hrt_absolute_time();
+	report.timestamp_position = msg.getMonotonicTimestamp().toUSec();
 	report.lat = msg.latitude_deg_1e8 / 10;
 	report.lon = msg.longitude_deg_1e8 / 10;
 	report.alt = msg.height_msl_mm;
@@ -43,8 +43,6 @@

 #pragma once

-#include <drivers/drv_hrt.h>
-
 #include <uORB/uORB.h>
 #include <uORB/topics/vehicle_gps_position.h>

@@ -37,6 +37,8 @@

 #include "mag.hpp"

+#include <systemlib/err.h>
+
 static const orb_id_t MAG_TOPICS[3] = {
 	ORB_ID(sensor_mag0),
 	ORB_ID(sensor_mag1),
@@ -49,6 +51,8 @@ UavcanMagnetometerBridge::UavcanMagnetometerBridge(uavcan::INode& node) :
 UavcanCDevSensorBridgeBase("uavcan_mag", "/dev/uavcan/mag", MAG_DEVICE_PATH, MAG_TOPICS),
 _sub_mag(node)
 {
+	_device_id.devid_s.devtype = DRV_MAG_DEVTYPE_HMC5883;
+
 	_scale.x_scale = 1.0F;
 	_scale.y_scale = 1.0F;
 	_scale.z_scale = 1.0F;
@@ -69,9 +73,36 @@ int UavcanMagnetometerBridge::init()
 	return 0;
 }

+ssize_t UavcanMagnetometerBridge::read(struct file *filp, char *buffer, size_t buflen)
+{
+	static uint64_t last_read = 0;
+	struct mag_report *mag_buf = reinterpret_cast<struct mag_report *>(buffer);
+
+	/* buffer must be large enough */
+	unsigned count = buflen / sizeof(struct mag_report);
+	if (count < 1) {
+		return -ENOSPC;
+	}
+
+	if (last_read < _report.timestamp) {
+		/* copy report */
+		lock();
+		*mag_buf = _report;
+		last_read = _report.timestamp;
+		unlock();
+		return sizeof(struct mag_report);
+	} else {
+		/* no new data available, warn caller */
+		return -EAGAIN;
+	}
+}
+
 int UavcanMagnetometerBridge::ioctl(struct file *filp, int cmd, unsigned long arg)
 {
 	switch (cmd) {
+	case SENSORIOCSQUEUEDEPTH: {
+		return OK;			// Pretend that this stuff is supported to keep APM happy
+	}
 	case MAGIOCSSCALE: {
 		std::memcpy(&_scale, reinterpret_cast<const void*>(arg), sizeof(_scale));
 		return 0;
@@ -84,7 +115,7 @@ int UavcanMagnetometerBridge::ioctl(struct file *filp, int cmd, unsigned long ar
 		return 0;           // Nothing to do
 	}
 	case MAGIOCGEXTERNAL: {
-		return 0;           // We don't want anyone to transform the coordinate frame, so we declare it onboard
+		return 1;           // declare it external rise it's priority and to allow for correct orientation compensation
 	}
 	case MAGIOCSSAMPLERATE: {
 		return 0;           // Pretend that this stuff is supported to keep the sensor app happy
@@ -106,18 +137,14 @@ int UavcanMagnetometerBridge::ioctl(struct file *filp, int cmd, unsigned long ar

 void UavcanMagnetometerBridge::mag_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::ahrs::Magnetometer> &msg)
 {
-	auto report = ::mag_report();
+	lock();
+	_report.range_ga = 1.3F;   // Arbitrary number, doesn't really mean anything
+	_report.timestamp = msg.getMonotonicTimestamp().toUSec();

-	report.range_ga = 1.3F;   // Arbitrary number, doesn't really mean anything
+	_report.x = (msg.magnetic_field[0] - _scale.x_offset) * _scale.x_scale;
+	_report.y = (msg.magnetic_field[1] - _scale.y_offset) * _scale.y_scale;
+	_report.z = (msg.magnetic_field[2] - _scale.z_offset) * _scale.z_scale;
+	unlock();

-	report.timestamp = msg.getUtcTimestamp().toUSec();
-	if (report.timestamp == 0) {
-		report.timestamp = msg.getMonotonicTimestamp().toUSec();
-	}
-
-	report.x = (msg.magnetic_field[0] - _scale.x_offset) * _scale.x_scale;
-	report.y = (msg.magnetic_field[1] - _scale.y_offset) * _scale.y_scale;
-	report.z = (msg.magnetic_field[2] - _scale.z_offset) * _scale.z_scale;
-
-	publish(msg.getSrcNodeID().get(), &report);
+	publish(msg.getSrcNodeID().get(), &_report);
 }
@@ -54,6 +54,7 @@ public:
 	int init() override;

 private:
+	ssize_t	read(struct file *filp, char *buffer, size_t buflen);
 	int ioctl(struct file *filp, int cmd, unsigned long arg) override;

 	void mag_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::ahrs::Magnetometer> &msg);
@@ -65,4 +66,5 @@ private:

 	uavcan::Subscriber<uavcan::equipment::ahrs::Magnetometer, MagCbBinder> _sub_mag;
 	mag_scale _scale = {};
+	mag_report _report =  {};
 };
@@ -103,6 +103,9 @@ void UavcanCDevSensorBridgeBase::publish(const int node_id, const void *report)
 			return;
 		}

+		// update device id as we now know our device node_id
+		_device_id.devid_s.address = static_cast<uint8_t>(node_id);
+
 		// Ask the CDev helper which class instance we can take
 		const int class_instance = register_class_devname(_class_devname);
 		if (class_instance < 0 || class_instance >= int(_max_channels)) {
@@ -112,6 +112,8 @@ protected:
 	_channels(new Channel[MaxChannels])
 	{
 		memcpy(_orb_topics, orb_topics, sizeof(orb_id_t) * MaxChannels);
+		_device_id.devid_s.bus_type = DeviceBusType_UAVCAN;
+		_device_id.devid_s.bus = 0;
 	}

 	/**
@@ -269,6 +269,24 @@ void UavcanNode::node_spin_once()
 	}
 }

+/*
+  add a fd to the list of polled events. This assumes you want
+  POLLIN for now.
+ */
+int UavcanNode::add_poll_fd(int fd)
+{
+	int ret = _poll_fds_num;
+	if (_poll_fds_num >= UAVCAN_NUM_POLL_FDS) {
+		errx(1, "uavcan: too many poll fds, exiting");
+	}
+	_poll_fds[_poll_fds_num] = ::pollfd();
+	_poll_fds[_poll_fds_num].fd = fd;
+	_poll_fds[_poll_fds_num].events = POLLIN;
+	_poll_fds_num += 1;
+	return ret;
+}
+
+
 int UavcanNode::run()
 {
 	(void)pthread_mutex_lock(&_node_mutex);
@@ -279,9 +297,10 @@ int UavcanNode::run()
 	_output_count = 2;

 	_armed_sub = orb_subscribe(ORB_ID(actuator_armed));
+	_test_motor_sub = orb_subscribe(ORB_ID(test_motor));
+	_actuator_direct_sub = orb_subscribe(ORB_ID(actuator_direct));

-	actuator_outputs_s outputs;
-	memset(&outputs, 0, sizeof(outputs));
+	memset(&_outputs, 0, sizeof(_outputs));

 	const int busevent_fd = ::open(uavcan_stm32::BusEvent::DevName, 0);
 	if (busevent_fd < 0)
@@ -303,11 +322,15 @@ int UavcanNode::run()
 	 * the value returned from poll() to detect whether actuator control has timed out or not.
 	 * Instead, all ORB events need to be checked individually (see below).
 	 */
-	_poll_fds_num = 0;
-	_poll_fds[_poll_fds_num] = ::pollfd();
-	_poll_fds[_poll_fds_num].fd = busevent_fd;
-	_poll_fds[_poll_fds_num].events = POLLIN;
-	_poll_fds_num += 1;
+	add_poll_fd(busevent_fd);
+
+	/*
+	 * setup poll to look for actuator direct input if we are
+	 * subscribed to the topic
+	 */
+	if (_actuator_direct_sub != -1) {
+		_actuator_direct_poll_fd_num = add_poll_fd(_actuator_direct_sub);
+	}

 	while (!_task_should_exit) {
 		// update actuator controls subscriptions if needed
@@ -325,6 +348,8 @@ int UavcanNode::run()

 		node_spin_once();  // Non-blocking

+		bool new_output = false;
+
 		// this would be bad...
 		if (poll_ret < 0) {
 			log("poll error %d", errno);
@@ -332,67 +357,102 @@ int UavcanNode::run()
 		} else {
 			// get controls for required topics
 			bool controls_updated = false;
-			unsigned poll_id = 1;
 			for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) {
 				if (_control_subs[i] > 0) {
-					if (_poll_fds[poll_id].revents & POLLIN) {
+					if (_poll_fds[_poll_ids[i]].revents & POLLIN) {
 						controls_updated = true;
 						orb_copy(_control_topics[i], _control_subs[i], &_controls[i]);
 					}
-					poll_id++;
 				}
 			}

+			/*
+			  see if we have any direct actuator updates
+			 */
+			if (_actuator_direct_sub != -1 && 
+			    (_poll_fds[_actuator_direct_poll_fd_num].revents & POLLIN) &&
+			    orb_copy(ORB_ID(actuator_direct), _actuator_direct_sub, &_actuator_direct) == OK &&
+			    !_test_in_progress) {
+				if (_actuator_direct.nvalues > NUM_ACTUATOR_OUTPUTS) {
+					_actuator_direct.nvalues = NUM_ACTUATOR_OUTPUTS;
+				}
+				memcpy(&_outputs.output[0], &_actuator_direct.values[0], 
+				       _actuator_direct.nvalues*sizeof(float));
+				_outputs.noutputs = _actuator_direct.nvalues;
+				new_output = true;
+			}
+
 			// can we mix?
-			if (controls_updated && (_mixers != nullptr)) {
+			if (_test_in_progress) {
+				memset(&_outputs, 0, sizeof(_outputs));
+				if (_test_motor.motor_number < NUM_ACTUATOR_OUTPUTS) {
+					_outputs.output[_test_motor.motor_number] = _test_motor.value*2.0f-1.0f;
+					_outputs.noutputs = _test_motor.motor_number+1;
+				}
+				new_output = true;
+			} else if (controls_updated && (_mixers != nullptr)) {

 				// XXX one output group has 8 outputs max,
 				// but this driver could well serve multiple groups.
 				unsigned num_outputs_max = 8;

 				// Do mixing
-				outputs.noutputs = _mixers->mix(&outputs.output[0], num_outputs_max);
-				outputs.timestamp = hrt_absolute_time();
+				_outputs.noutputs = _mixers->mix(&_outputs.output[0], num_outputs_max);

-				// iterate actuators
-				for (unsigned i = 0; i < outputs.noutputs; i++) {
-					// last resort: catch NaN, INF and out-of-band errors
-					if (!isfinite(outputs.output[i])) {
-						/*
-						 * Value is NaN, INF or out of band - set to the minimum value.
-						 * This will be clearly visible on the servo status and will limit the risk of accidentally
-						 * spinning motors. It would be deadly in flight.
-						 */
-						outputs.output[i] = -1.0f;
-					}
-
-					// limit outputs to valid range
-
-					// never go below min
-					if (outputs.output[i] < -1.0f) {
-						outputs.output[i] = -1.0f;
-					}
-
-					// never go below max
-					if (outputs.output[i] > 1.0f) {
-						outputs.output[i] = 1.0f;
-					}
-				}
-
-				// Output to the bus
-				_esc_controller.update_outputs(outputs.output, outputs.noutputs);
+				new_output = true;
 			}
 		}

-		// Check arming state
+		if (new_output) {
+			// iterate actuators, checking for valid values
+			for (uint8_t i = 0; i < _outputs.noutputs; i++) {
+				// last resort: catch NaN, INF and out-of-band errors
+				if (!isfinite(_outputs.output[i])) {
+					/*
+					 * Value is NaN, INF or out of band - set to the minimum value.
+					 * This will be clearly visible on the servo status and will limit the risk of accidentally
+					 * spinning motors. It would be deadly in flight.
+					 */
+					_outputs.output[i] = -1.0f;
+				}
+
+				// never go below min
+				if (_outputs.output[i] < -1.0f) {
+					_outputs.output[i] = -1.0f;
+				}
+
+				// never go above max
+				if (_outputs.output[i] > 1.0f) {
+					_outputs.output[i] = 1.0f;
+				}
+			}
+			// Output to the bus
+			_outputs.timestamp = hrt_absolute_time();
+			_esc_controller.update_outputs(_outputs.output, _outputs.noutputs);
+		}
+
+
+		// Check motor test state
 		bool updated = false;
+		orb_check(_test_motor_sub, &updated);
+
+		if (updated) {
+			orb_copy(ORB_ID(test_motor), _test_motor_sub, &_test_motor);
+
+			// Update the test status and check that we're not locked down
+			_test_in_progress = (_test_motor.value > 0);
+			_esc_controller.arm_single_esc(_test_motor.motor_number, _test_in_progress);
+		}
+
+		// Check arming state
 		orb_check(_armed_sub, &updated);

 		if (updated) {
 			orb_copy(ORB_ID(actuator_armed), _armed_sub, &_armed);

-			// Update the armed status and check that we're not locked down
-			bool set_armed = _armed.armed && !_armed.lockdown;
+			// Update the armed status and check that we're not locked down and motor 
+			// test is not running
+			bool set_armed = _armed.armed && !_armed.lockdown && !_test_in_progress;

 			arm_actuators(set_armed);
 		}
@@ -429,7 +489,7 @@ int
 UavcanNode::arm_actuators(bool arm)
 {
 	_is_armed = arm;
-	_esc_controller.arm_esc(arm);
+	_esc_controller.arm_all_escs(arm);
 	return OK;
 }

@@ -440,7 +500,6 @@ UavcanNode::subscribe()
 	uint32_t sub_groups = _groups_required & ~_groups_subscribed;
 	uint32_t unsub_groups = _groups_subscribed & ~_groups_required;
 	// the first fd used by CAN
-	_poll_fds_num = 1;
 	for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) {
 		if (sub_groups & (1 << i)) {
 			warnx("subscribe to actuator_controls_%d", i);
@@ -453,9 +512,7 @@ UavcanNode::subscribe()
 		}

 		if (_control_subs[i] > 0) {
-			_poll_fds[_poll_fds_num].fd = _control_subs[i];
-			_poll_fds[_poll_fds_num].events = POLLIN;
-			_poll_fds_num++;
+			_poll_ids[i] = add_poll_fd(_control_subs[i]);
 		}
 	}
 }
@@ -553,6 +610,14 @@ UavcanNode::print_info()
 	       (unsigned)_groups_subscribed, (unsigned)_groups_required, _poll_fds_num);
 	printf("ESC mixer: %s\n", (_mixers == nullptr) ? "NONE" : "OK");

+	if (_outputs.noutputs != 0) {
+		printf("ESC output: ");
+		for (uint8_t i=0; i<_outputs.noutputs; i++) {
+			printf("%d ", (int)(_outputs.output[i]*1000));
+		}
+		printf("\n");
+	}
+
 	// Sensor bridges
 	auto br = _sensor_bridges.getHead();
 	while (br != nullptr) {
@@ -571,7 +636,7 @@ UavcanNode::print_info()
 static void print_usage()
 {
 	warnx("usage: \n"
-	      "\tuavcan {start|status|stop}");
+	      "\tuavcan {start|status|stop|arm|disarm}");
 }

 extern "C" __EXPORT int uavcan_main(int argc, char *argv[]);
@@ -618,6 +683,16 @@ int uavcan_main(int argc, char *argv[])
 		::exit(0);
 	}

+	if (!std::strcmp(argv[1], "arm")) {
+		inst->arm_actuators(true);
+		::exit(0);
+	}
+
+	if (!std::strcmp(argv[1], "disarm")) {
+		inst->arm_actuators(false);
+		::exit(0);
+	}
+
 	if (!std::strcmp(argv[1], "stop")) {
 		delete inst;
 		::exit(0);
@@ -41,6 +41,8 @@
 #include <uORB/topics/actuator_controls.h>
 #include <uORB/topics/actuator_outputs.h>
 #include <uORB/topics/actuator_armed.h>
+#include <uORB/topics/test_motor.h>
+#include <uORB/topics/actuator_direct.h>

 #include "actuators/esc.hpp"
 #include "sensors/sensor_bridge.hpp"
@@ -56,6 +58,9 @@
 #define NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN	4
 #define UAVCAN_DEVICE_PATH	"/dev/uavcan/esc"

+// we add two to allow for actuator_direct and busevent
+#define UAVCAN_NUM_POLL_FDS (NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN+2)
+
 /**
 * A UAVCAN node.
 */
@@ -96,6 +101,8 @@ private:
 	int		init(uavcan::NodeID node_id);
 	void		node_spin_once();
 	int		run();
+	int		add_poll_fd(int fd);			///< add a fd to poll list, returning index into _poll_fds[]
+

 	int			_task = -1;			///< handle to the OS task
 	bool			_task_should_exit = false;	///< flag to indicate to tear down the CAN driver
@@ -103,6 +110,10 @@ private:
 	actuator_armed_s	_armed;				///< the arming request of the system
 	bool			_is_armed = false;		///< the arming status of the actuators on the bus

+	int			_test_motor_sub = -1;   ///< uORB subscription of the test_motor status
+	test_motor_s		_test_motor;
+	bool			_test_in_progress = false;
+
 	unsigned		_output_count = 0;		///< number of actuators currently available

 	static UavcanNode	*_instance;			///< singleton pointer
@@ -120,6 +131,15 @@ private:
 	int			_control_subs[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
 	actuator_controls_s 	_controls[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
 	orb_id_t		_control_topics[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
-	pollfd			_poll_fds[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN + 1] = {};	///< +1 for /dev/uavcan/busevent
+	pollfd			_poll_fds[UAVCAN_NUM_POLL_FDS] = {};
 	unsigned		_poll_fds_num = 0;
+
+	int			_actuator_direct_sub = -1;   ///< uORB subscription of the actuator_direct topic
+	uint8_t			_actuator_direct_poll_fd_num;
+	actuator_direct_s	_actuator_direct;
+
+	actuator_outputs_s	_outputs;
+
+	// index into _poll_fds for each _control_subs handle
+	uint8_t			_poll_ids[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN];
 };