Moved math library to library dir, improved sensor-level HIL, cleaned up geo / conversion libs

1 files changed, 41 insertions, 9 deletions

diff --git a/src/modules/mavlink/orb_listener.c b/src/modules/mavlink/orb_listener.c
index 2a260861d..c711b1803 100644
--- a/src/modules/mavlink/orb_listener.c
+++ b/src/modules/mavlink/orb_listener.c
@@ -71,7 +71,8 @@ struct vehicle_status_s v_status;
 struct rc_channels_s rc;
 struct rc_input_values rc_raw;
 struct actuator_armed_s armed;
-struct actuator_controls_effective_s actuators_0;
+struct actuator_controls_effective_s actuators_effective_0;
+struct actuator_controls_s actuators_0;
 struct vehicle_attitude_s att;
 
 struct mavlink_subscriptions mavlink_subs;
@@ -112,6 +113,7 @@ static void	l_attitude_setpoint(const struct listener *l);
 static void	l_actuator_outputs(const struct listener *l);
 static void	l_actuator_armed(const struct listener *l);
 static void	l_manual_control_setpoint(const struct listener *l);
+static void	l_vehicle_attitude_controls_effective(const struct listener *l);
 static void	l_vehicle_attitude_controls(const struct listener *l);
 static void	l_debug_key_value(const struct listener *l);
 static void	l_optical_flow(const struct listener *l);
@@ -138,6 +140,7 @@ static const struct listener listeners[] = {
 	{l_actuator_armed,		&mavlink_subs.armed_sub,	0},
 	{l_manual_control_setpoint,	&mavlink_subs.man_control_sp_sub, 0},
 	{l_vehicle_attitude_controls,	&mavlink_subs.actuators_sub,	0},
+	{l_vehicle_attitude_controls_effective,	&mavlink_subs.actuators_effective_sub,	0},
 	{l_debug_key_value,		&mavlink_subs.debug_key_value,	0},
 	{l_optical_flow,		&mavlink_subs.optical_flow,	0},
 	{l_vehicle_rates_setpoint,	&mavlink_subs.rates_setpoint_sub,	0},
@@ -567,28 +570,54 @@ l_manual_control_setpoint(const struct listener *l)
 }
 
 void
-l_vehicle_attitude_controls(const struct listener *l)
+l_vehicle_attitude_controls_effective(const struct listener *l)
 {
-	orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE, mavlink_subs.actuators_sub, &actuators_0);
+	orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE, mavlink_subs.actuators_effective_sub, &actuators_effective_0);
 
 	if (gcs_link) {
 		/* send, add spaces so that string buffer is at least 10 chars long */
 		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
 						   last_sensor_timestamp / 1000,
 						   "eff ctrl0    ",
-						   actuators_0.control_effective[0]);
+						   actuators_effective_0.control_effective[0]);
 		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
 						   last_sensor_timestamp / 1000,
 						   "eff ctrl1    ",
-						   actuators_0.control_effective[1]);
+						   actuators_effective_0.control_effective[1]);
 		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
 						   last_sensor_timestamp / 1000,
 						   "eff ctrl2     ",
-						   actuators_0.control_effective[2]);
+						   actuators_effective_0.control_effective[2]);
 		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
 						   last_sensor_timestamp / 1000,
 						   "eff ctrl3     ",
-						   actuators_0.control_effective[3]);
+						   actuators_effective_0.control_effective[3]);
+	}
+}
+
+void
+l_vehicle_attitude_controls(const struct listener *l)
+{
+	orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, mavlink_subs.actuators_sub, &actuators_0);
+
+	if (gcs_link) {
+		/* send, add spaces so that string buffer is at least 10 chars long */
+		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
+						   last_sensor_timestamp / 1000,
+						   "ctrl0    ",
+						   actuators_0.control[0]);
+		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
+						   last_sensor_timestamp / 1000,
+						   "ctrl1    ",
+						   actuators_0.control[1]);
+		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
+						   last_sensor_timestamp / 1000,
+						   "ctrl2     ",
+						   actuators_0.control[2]);
+		mavlink_msg_named_value_float_send(MAVLINK_COMM_0,
+						   last_sensor_timestamp / 1000,
+						   "ctrl3     ",
+						   actuators_0.control[3]);
 	}
 }
 
@@ -637,7 +666,7 @@ l_airspeed(const struct listener *l)
 	orb_copy(ORB_ID(airspeed), mavlink_subs.airspeed_sub, &airspeed);
 
 	float groundspeed = sqrtf(global_pos.vx * global_pos.vx + global_pos.vy * global_pos.vy);
-	float throttle = actuators_0.control_effective[3] * (UINT16_MAX - 1);
+	float throttle = actuators_effective_0.control_effective[3] * (UINT16_MAX - 1);
 	float alt = global_pos.alt;
 	float climb = global_pos.vz;
 
@@ -773,7 +802,10 @@ uorb_receive_start(void)
 	orb_set_interval(mavlink_subs.man_control_sp_sub, 100);	/* 10Hz updates */
 
 	/* --- ACTUATOR CONTROL VALUE --- */
-	mavlink_subs.actuators_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE);
+	mavlink_subs.actuators_effective_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE);
+	orb_set_interval(mavlink_subs.actuators_effective_sub, 100);	/* 10Hz updates */
+
+	mavlink_subs.actuators_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
 	orb_set_interval(mavlink_subs.actuators_sub, 100);	/* 10Hz updates */
 
 	/* --- DEBUG VALUE OUTPUT --- */