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authorLorenz Meier <lm@inf.ethz.ch>2014-07-15 22:07:03 +0200
committerLorenz Meier <lm@inf.ethz.ch>2014-07-15 22:07:03 +0200
commite696ed5509d001e181c33a2379d634e76190c42a (patch)
tree8fd3e88c0782ceb90e6b9589daa1290d548058fd /src/modules/uORB
parent79aa600d29c66e4619aacf73e71e51df13560205 (diff)
parent619433d36911b9c3923bae666d3632beb713935f (diff)
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Merged master
Diffstat (limited to 'src/modules/uORB')
-rw-r--r--src/modules/uORB/Publication.cpp2
-rw-r--r--src/modules/uORB/Subscription.cpp2
-rw-r--r--src/modules/uORB/objects_common.cpp17
-rw-r--r--src/modules/uORB/topics/differential_pressure.h1
-rw-r--r--src/modules/uORB/topics/estimator_status.h6
-rw-r--r--src/modules/uORB/topics/home_position.h5
-rw-r--r--src/modules/uORB/topics/manual_control_setpoint.h1
-rw-r--r--src/modules/uORB/topics/mission.h23
-rw-r--r--src/modules/uORB/topics/mission_result.h7
-rw-r--r--src/modules/uORB/topics/offboard_control_setpoint.h2
-rw-r--r--src/modules/uORB/topics/position_setpoint_triplet.h31
-rw-r--r--src/modules/uORB/topics/rc_channels.h68
-rw-r--r--src/modules/uORB/topics/satellite_info.h89
-rw-r--r--src/modules/uORB/topics/tecs_status.h93
-rw-r--r--src/modules/uORB/topics/telemetry_status.h25
-rw-r--r--src/modules/uORB/topics/vehicle_attitude_setpoint.h2
-rw-r--r--src/modules/uORB/topics/vehicle_control_mode.h1
-rw-r--r--src/modules/uORB/topics/vehicle_force_setpoint.h65
-rw-r--r--src/modules/uORB/topics/vehicle_global_position.h13
-rw-r--r--src/modules/uORB/topics/vehicle_gps_position.h14
-rw-r--r--src/modules/uORB/topics/vehicle_status.h62
-rw-r--r--src/modules/uORB/topics/wind_estimate.h68
22 files changed, 487 insertions, 110 deletions
diff --git a/src/modules/uORB/Publication.cpp b/src/modules/uORB/Publication.cpp
index 5a5981617..cd0b30dd6 100644
--- a/src/modules/uORB/Publication.cpp
+++ b/src/modules/uORB/Publication.cpp
@@ -47,6 +47,7 @@
#include "topics/vehicle_rates_setpoint.h"
#include "topics/actuator_outputs.h"
#include "topics/encoders.h"
+#include "topics/tecs_status.h"
namespace uORB {
@@ -76,5 +77,6 @@ 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<encoders_s>;
+template class __EXPORT Publication<tecs_status_s>;
}
diff --git a/src/modules/uORB/Subscription.cpp b/src/modules/uORB/Subscription.cpp
index c1d1a938f..44b6debc7 100644
--- a/src/modules/uORB/Subscription.cpp
+++ b/src/modules/uORB/Subscription.cpp
@@ -40,6 +40,7 @@
#include "topics/parameter_update.h"
#include "topics/actuator_controls.h"
#include "topics/vehicle_gps_position.h"
+#include "topics/satellite_info.h"
#include "topics/sensor_combined.h"
#include "topics/vehicle_attitude.h"
#include "topics/vehicle_global_position.h"
@@ -88,6 +89,7 @@ T Subscription<T>::getData() {
template class __EXPORT Subscription<parameter_update_s>;
template class __EXPORT Subscription<actuator_controls_s>;
template class __EXPORT Subscription<vehicle_gps_position_s>;
+template class __EXPORT Subscription<satellite_info_s>;
template class __EXPORT Subscription<sensor_combined_s>;
template class __EXPORT Subscription<vehicle_attitude_s>;
template class __EXPORT Subscription<vehicle_global_position_s>;
diff --git a/src/modules/uORB/objects_common.cpp b/src/modules/uORB/objects_common.cpp
index 8340ca28a..679d6ea4f 100644
--- a/src/modules/uORB/objects_common.cpp
+++ b/src/modules/uORB/objects_common.cpp
@@ -79,6 +79,9 @@ ORB_DEFINE(sensor_combined, struct sensor_combined_s);
#include "topics/vehicle_gps_position.h"
ORB_DEFINE(vehicle_gps_position, struct vehicle_gps_position_s);
+#include "topics/satellite_info.h"
+ORB_DEFINE(satellite_info, struct satellite_info_s);
+
#include "topics/home_position.h"
ORB_DEFINE(home_position, struct home_position_s);
@@ -187,7 +190,10 @@ ORB_DEFINE(actuator_outputs_2, struct actuator_outputs_s);
ORB_DEFINE(actuator_outputs_3, struct actuator_outputs_s);
#include "topics/telemetry_status.h"
-ORB_DEFINE(telemetry_status, struct telemetry_status_s);
+ORB_DEFINE(telemetry_status_0, struct telemetry_status_s);
+ORB_DEFINE(telemetry_status_1, struct telemetry_status_s);
+ORB_DEFINE(telemetry_status_2, struct telemetry_status_s);
+ORB_DEFINE(telemetry_status_3, struct telemetry_status_s);
#include "topics/debug_key_value.h"
ORB_DEFINE(debug_key_value, struct debug_key_value_s);
@@ -203,3 +209,12 @@ ORB_DEFINE(encoders, struct encoders_s);
#include "topics/estimator_status.h"
ORB_DEFINE(estimator_status, struct estimator_status_report);
+
+#include "topics/vehicle_force_setpoint.h"
+ORB_DEFINE(vehicle_force_setpoint, struct vehicle_force_setpoint_s);
+
+#include "topics/tecs_status.h"
+ORB_DEFINE(tecs_status, struct tecs_status_s);
+
+#include "topics/wind_estimate.h"
+ORB_DEFINE(wind_estimate, struct wind_estimate_s);
diff --git a/src/modules/uORB/topics/differential_pressure.h b/src/modules/uORB/topics/differential_pressure.h
index 01e14cda9..cd48d3cb2 100644
--- a/src/modules/uORB/topics/differential_pressure.h
+++ b/src/modules/uORB/topics/differential_pressure.h
@@ -58,7 +58,6 @@ struct differential_pressure_s {
float differential_pressure_raw_pa; /**< Raw differential pressure reading (may be negative) */
float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
- float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
};
diff --git a/src/modules/uORB/topics/estimator_status.h b/src/modules/uORB/topics/estimator_status.h
index 5530cdb21..7f26b505b 100644
--- a/src/modules/uORB/topics/estimator_status.h
+++ b/src/modules/uORB/topics/estimator_status.h
@@ -64,9 +64,9 @@ struct estimator_status_report {
uint64_t timestamp; /**< Timestamp in microseconds since boot */
float states[32]; /**< Internal filter states */
float n_states; /**< Number of states effectively used */
- bool states_nan; /**< If set to true, one of the states is NaN */
- bool covariance_nan; /**< If set to true, the covariance matrix went NaN */
- bool kalman_gain_nan; /**< If set to true, the Kalman gain matrix went NaN */
+ uint8_t nan_flags; /**< Bitmask to indicate NaN states */
+ uint8_t health_flags; /**< Bitmask to indicate sensor health states (vel, pos, hgt) */
+ uint8_t timeout_flags; /**< Bitmask to indicate timeout flags (vel, pos, hgt) */
};
diff --git a/src/modules/uORB/topics/home_position.h b/src/modules/uORB/topics/home_position.h
index 08d11abae..70071130d 100644
--- a/src/modules/uORB/topics/home_position.h
+++ b/src/modules/uORB/topics/home_position.h
@@ -59,10 +59,13 @@ struct home_position_s
{
uint64_t timestamp; /**< Timestamp (microseconds since system boot) */
- //bool altitude_is_relative; // TODO what means home relative altitude? we need clear definition of reference altitude then
double lat; /**< Latitude in degrees */
double lon; /**< Longitude in degrees */
float alt; /**< Altitude in meters */
+
+ float x; /**< X coordinate in meters */
+ float y; /**< Y coordinate in meters */
+ float z; /**< Z coordinate in meters */
};
/**
diff --git a/src/modules/uORB/topics/manual_control_setpoint.h b/src/modules/uORB/topics/manual_control_setpoint.h
index 910b8a623..dde237adc 100644
--- a/src/modules/uORB/topics/manual_control_setpoint.h
+++ b/src/modules/uORB/topics/manual_control_setpoint.h
@@ -98,6 +98,7 @@ struct manual_control_setpoint_s {
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 */
/**
diff --git a/src/modules/uORB/topics/mission.h b/src/modules/uORB/topics/mission.h
index ef4bc1def..e4b72f87c 100644
--- a/src/modules/uORB/topics/mission.h
+++ b/src/modules/uORB/topics/mission.h
@@ -1,9 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
- * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
- * @author Julian Oes <joes@student.ethz.ch>
- * @author Lorenz Meier <lm@inf.ethz.ch>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -37,6 +34,9 @@
/**
* @file mission.h
* Definition of a mission consisting of mission items.
+ * @author Thomas Gubler <thomasgubler@student.ethz.ch>
+ * @author Julian Oes <joes@student.ethz.ch>
+ * @author Lorenz Meier <lm@inf.ethz.ch>
*/
#ifndef TOPIC_MISSION_H_
@@ -50,6 +50,7 @@
/* compatible to mavlink MAV_CMD */
enum NAV_CMD {
+ NAV_CMD_IDLE=0,
NAV_CMD_WAYPOINT=16,
NAV_CMD_LOITER_UNLIMITED=17,
NAV_CMD_LOITER_TURN_COUNT=18,
@@ -58,7 +59,8 @@ enum NAV_CMD {
NAV_CMD_LAND=21,
NAV_CMD_TAKEOFF=22,
NAV_CMD_ROI=80,
- NAV_CMD_PATHPLANNING=81
+ NAV_CMD_PATHPLANNING=81,
+ NAV_CMD_DO_JUMP=177
};
enum ORIGIN {
@@ -91,13 +93,20 @@ struct mission_item_s {
float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
bool autocontinue; /**< true if next waypoint should follow after this one */
enum ORIGIN origin; /**< where the waypoint has been generated */
+ int do_jump_mission_index; /**< index where the do jump will go to */
+ unsigned do_jump_repeat_count; /**< how many times do jump needs to be done */
+ unsigned do_jump_current_count; /**< count how many times the jump has been done */
};
+/**
+ * This topic used to notify navigator about mission changes, mission itself and new mission state
+ * must be stored in dataman before publication.
+ */
struct mission_s
{
- int dataman_id; /**< default -1, there are two offboard storage places in the dataman: 0 or 1 */
- unsigned count; /**< count of the missions stored in the datamanager */
- int current_index; /**< default -1, start at the one changed latest */
+ int dataman_id; /**< default 0, there are two offboard storage places in the dataman: 0 or 1 */
+ unsigned count; /**< count of the missions stored in the dataman */
+ int current_seq; /**< default -1, start at the one changed latest */
};
/**
diff --git a/src/modules/uORB/topics/mission_result.h b/src/modules/uORB/topics/mission_result.h
index 7c3921198..beb797e62 100644
--- a/src/modules/uORB/topics/mission_result.h
+++ b/src/modules/uORB/topics/mission_result.h
@@ -53,9 +53,10 @@
struct mission_result_s
{
- bool mission_reached; /**< true if mission has been reached */
- unsigned mission_index_reached; /**< index of the mission which has been reached */
- unsigned index_current_mission; /**< index of the current mission */
+ unsigned seq_reached; /**< Sequence of the mission item which has been reached */
+ unsigned seq_current; /**< Sequence of the current mission item */
+ bool reached; /**< true if mission has been reached */
+ bool finished; /**< true if mission has been completed */
};
/**
diff --git a/src/modules/uORB/topics/offboard_control_setpoint.h b/src/modules/uORB/topics/offboard_control_setpoint.h
index 68d3e494b..d7b131e3c 100644
--- a/src/modules/uORB/topics/offboard_control_setpoint.h
+++ b/src/modules/uORB/topics/offboard_control_setpoint.h
@@ -69,7 +69,7 @@ struct offboard_control_setpoint_s {
uint64_t timestamp;
enum OFFBOARD_CONTROL_MODE mode; /**< The current control inputs mode */
- bool armed; /**< Armed flag set, yes / no */
+
float p1; /**< ailerons roll / roll rate input */
float p2; /**< elevator / pitch / pitch rate */
float p3; /**< rudder / yaw rate / yaw */
diff --git a/src/modules/uORB/topics/position_setpoint_triplet.h b/src/modules/uORB/topics/position_setpoint_triplet.h
index 34aaa30dd..673c0e491 100644
--- a/src/modules/uORB/topics/position_setpoint_triplet.h
+++ b/src/modules/uORB/topics/position_setpoint_triplet.h
@@ -1,9 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2013 PX4 Development Team. All rights reserved.
- * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
- * @author Julian Oes <joes@student.ethz.ch>
- * @author Lorenz Meier <lm@inf.ethz.ch>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -37,6 +34,10 @@
/**
* @file mission_item_triplet.h
* Definition of the global WGS84 position setpoint uORB topic.
+ *
+ * @author Thomas Gubler <thomasgubler@student.ethz.ch>
+ * @author Julian Oes <joes@student.ethz.ch>
+ * @author Lorenz Meier <lm@inf.ethz.ch>
*/
#ifndef TOPIC_MISSION_ITEM_TRIPLET_H_
@@ -45,7 +46,6 @@
#include <stdint.h>
#include <stdbool.h>
#include "../uORB.h"
-#include <navigator/navigator_state.h>
/**
* @addtogroup topics
@@ -54,21 +54,32 @@
enum SETPOINT_TYPE
{
- SETPOINT_TYPE_NORMAL = 0, /**< normal setpoint */
- SETPOINT_TYPE_LOITER, /**< loiter setpoint */
- SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */
- SETPOINT_TYPE_LAND, /**< land setpoint, altitude must be ignored, vehicle must descend until landing */
- SETPOINT_TYPE_IDLE, /**< do nothing, switch off motors or keep at idle speed (MC) */
+ SETPOINT_TYPE_POSITION = 0, /**< position setpoint */
+ SETPOINT_TYPE_VELOCITY, /**< velocity setpoint */
+ SETPOINT_TYPE_LOITER, /**< loiter setpoint */
+ SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */
+ SETPOINT_TYPE_LAND, /**< land setpoint, altitude must be ignored, descend until landing */
+ SETPOINT_TYPE_IDLE, /**< do nothing, switch off motors or keep at idle speed (MC) */
+ SETPOINT_TYPE_OFFBOARD, /**< setpoint set by offboard */
};
struct position_setpoint_s
{
bool valid; /**< true if setpoint is valid */
enum SETPOINT_TYPE type; /**< setpoint type to adjust behavior of position controller */
+ float x; /**< local position setpoint in m in NED */
+ float y; /**< local position setpoint in m in NED */
+ float z; /**< local position setpoint in m in NED */
+ bool position_valid; /**< true if local position setpoint valid */
+ float vx; /**< local velocity setpoint in m in NED */
+ float vy; /**< local velocity setpoint in m in NED */
+ float vz; /**< local velocity setpoint in m in NED */
+ bool velocity_valid; /**< true if local velocity setpoint valid */
double lat; /**< latitude, in deg */
double lon; /**< longitude, in deg */
float alt; /**< altitude AMSL, in m */
float yaw; /**< yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw */
+ float yawspeed; /**< yawspeed (only for multirotors, in rad/s) */
float loiter_radius; /**< loiter radius (only for fixed wing), in m */
int8_t loiter_direction; /**< loiter direction: 1 = CW, -1 = CCW */
float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
@@ -84,8 +95,6 @@ struct position_setpoint_triplet_s
struct position_setpoint_s previous;
struct position_setpoint_s current;
struct position_setpoint_s next;
-
- nav_state_t nav_state; /**< navigation state */
};
/**
diff --git a/src/modules/uORB/topics/rc_channels.h b/src/modules/uORB/topics/rc_channels.h
index 370c54442..8978de471 100644
--- a/src/modules/uORB/topics/rc_channels.h
+++ b/src/modules/uORB/topics/rc_channels.h
@@ -1,6 +1,6 @@
/****************************************************************************
*
- * Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
+ * Copyright (c) 2012-2014 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
@@ -43,59 +43,43 @@
#include "../uORB.h"
/**
- * The number of RC channel inputs supported.
- * Current (Q4/2013) radios support up to 18 channels,
- * leaving at a sane value of 16.
- * This number can be greater then number of RC channels,
- * because single RC channel can be mapped to multiple
- * functions, e.g. for various mode switches.
- */
-#define RC_CHANNELS_MAPPED_MAX 16
-
-/**
* This defines the mapping of the RC functions.
* The value assigned to the specific function corresponds to the entry of
- * the channel array chan[].
+ * the channel array channels[].
*/
enum RC_CHANNELS_FUNCTION {
THROTTLE = 0,
- ROLL = 1,
- PITCH = 2,
- YAW = 3,
- MODE = 4,
- RETURN = 5,
- POSCTL = 6,
- LOITER = 7,
- OFFBOARD_MODE = 8,
- ACRO = 9,
- FLAPS = 10,
- AUX_1 = 11,
- AUX_2 = 12,
- AUX_3 = 13,
- AUX_4 = 14,
- AUX_5 = 15,
- RC_CHANNELS_FUNCTION_MAX /**< indicates the number of functions. There can be more functions than RC channels. */
+ ROLL,
+ PITCH,
+ YAW,
+ MODE,
+ RETURN,
+ POSCTL,
+ LOITER,
+ OFFBOARD,
+ ACRO,
+ FLAPS,
+ AUX_1,
+ 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. */
};
/**
* @addtogroup topics
* @{
*/
-
struct rc_channels_s {
-
- uint64_t timestamp; /**< In microseconds since boot time. */
- uint64_t timestamp_last_valid; /**< timestamp of last valid RC signal. */
- struct {
- float scaled; /**< Scaled to -1..1 (throttle: 0..1) */
- } chan[RC_CHANNELS_MAPPED_MAX];
- uint8_t chan_count; /**< number of valid channels */
-
- /*String array to store the names of the functions*/
- char function_name[RC_CHANNELS_FUNCTION_MAX][20];
- int8_t function[RC_CHANNELS_FUNCTION_MAX];
- uint8_t rssi; /**< Overall receive signal strength */
- bool signal_lost; /**< control signal lost, should be checked together with topic timeout */
+ uint64_t timestamp; /**< Timestamp in microseconds since boot time */
+ 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 */
}; /**< radio control channels. */
/**
diff --git a/src/modules/uORB/topics/satellite_info.h b/src/modules/uORB/topics/satellite_info.h
new file mode 100644
index 000000000..37c2faa96
--- /dev/null
+++ b/src/modules/uORB/topics/satellite_info.h
@@ -0,0 +1,89 @@
+/****************************************************************************
+ *
+ * Copyright (C) 2014 PX4 Development Team. All rights reserved.
+ * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
+ * @author Julian Oes <joes@student.ethz.ch>
+ * @author Lorenz Meier <lm@inf.ethz.ch>
+ *
+ * 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 satellite_info.h
+ * Definition of the GNSS satellite info uORB topic.
+ */
+
+#ifndef TOPIC_SAT_INFO_H_
+#define TOPIC_SAT_INFO_H_
+
+#include <stdint.h>
+#include "../uORB.h"
+
+/**
+ * @addtogroup topics
+ * @{
+ */
+
+/**
+ * GNSS Satellite Info.
+ */
+
+#define SAT_INFO_MAX_SATELLITES 20
+
+struct satellite_info_s {
+ uint64_t timestamp; /**< Timestamp of satellite info */
+ uint8_t count; /**< Number of satellites in satellite info */
+ uint8_t svid[SAT_INFO_MAX_SATELLITES]; /**< Space vehicle ID [1..255], see scheme below */
+ uint8_t used[SAT_INFO_MAX_SATELLITES]; /**< 0: Satellite not used, 1: used for navigation */
+ uint8_t elevation[SAT_INFO_MAX_SATELLITES]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
+ uint8_t azimuth[SAT_INFO_MAX_SATELLITES]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
+ uint8_t snr[SAT_INFO_MAX_SATELLITES]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
+};
+
+/**
+ * NAV_SVINFO space vehicle ID (svid) scheme according to u-blox protocol specs
+ * u-bloxM8-V15_ReceiverDescriptionProtocolSpec_Public_(UBX-13003221).pdf
+ *
+ * GPS 1-32
+ * SBAS 120-158
+ * Galileo 211-246
+ * BeiDou 159-163, 33-64
+ * QZSS 193-197
+ * GLONASS 65-96, 255
+ *
+ */
+
+/**
+ * @}
+ */
+
+/* register this as object request broker structure */
+ORB_DECLARE(satellite_info);
+
+#endif
diff --git a/src/modules/uORB/topics/tecs_status.h b/src/modules/uORB/topics/tecs_status.h
new file mode 100644
index 000000000..c4d0c1874
--- /dev/null
+++ b/src/modules/uORB/topics/tecs_status.h
@@ -0,0 +1,93 @@
+/****************************************************************************
+ *
+ * Copyright (c) 2012-2014 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 vehicle_global_position.h
+ * Definition of the global fused WGS84 position uORB topic.
+ *
+ * @author Thomas Gubler <thomasgubler@student.ethz.ch>
+ */
+
+#ifndef TECS_STATUS_T_H_
+#define TECS_STATUS_T_H_
+
+#include <stdint.h>
+#include <stdbool.h>
+#include "../uORB.h"
+
+/**
+ * @addtogroup topics
+ * @{
+ */
+
+typedef enum {
+ TECS_MODE_NORMAL,
+ TECS_MODE_UNDERSPEED,
+ TECS_MODE_TAKEOFF,
+ TECS_MODE_LAND,
+ TECS_MODE_LAND_THROTTLELIM
+} tecs_mode;
+
+ /**
+ * Internal values of the (m)TECS fixed wing speed alnd altitude control system
+ */
+struct tecs_status_s {
+ uint64_t timestamp; /**< timestamp, in microseconds since system start */
+
+ float altitudeSp;
+ float altitude;
+ float flightPathAngleSp;
+ float flightPathAngle;
+ float flightPathAngleFiltered;
+ float airspeedSp;
+ float airspeed;
+ float airspeedFiltered;
+ float airspeedDerivativeSp;
+ float airspeedDerivative;
+
+ float totalEnergyRateSp;
+ float totalEnergyRate;
+ float energyDistributionRateSp;
+ float energyDistributionRate;
+
+ tecs_mode mode;
+};
+
+/**
+ * @}
+ */
+
+/* register this as object request broker structure */
+ORB_DECLARE(tecs_status);
+
+#endif
diff --git a/src/modules/uORB/topics/telemetry_status.h b/src/modules/uORB/topics/telemetry_status.h
index 76693c46e..3347724a5 100644
--- a/src/modules/uORB/topics/telemetry_status.h
+++ b/src/modules/uORB/topics/telemetry_status.h
@@ -57,6 +57,7 @@ enum TELEMETRY_STATUS_RADIO_TYPE {
struct telemetry_status_s {
uint64_t timestamp;
+ uint64_t heartbeat_time; /**< Time of last received heartbeat from remote system */
enum TELEMETRY_STATUS_RADIO_TYPE type; /**< type of the radio hardware */
uint8_t rssi; /**< local signal strength */
uint8_t remote_rssi; /**< remote signal strength */
@@ -71,6 +72,28 @@ struct telemetry_status_s {
* @}
*/
-ORB_DECLARE(telemetry_status);
+ORB_DECLARE(telemetry_status_0);
+ORB_DECLARE(telemetry_status_1);
+ORB_DECLARE(telemetry_status_2);
+ORB_DECLARE(telemetry_status_3);
+
+#define TELEMETRY_STATUS_ORB_ID_NUM 4
+
+static const struct orb_metadata *telemetry_status_orb_id[TELEMETRY_STATUS_ORB_ID_NUM] = {
+ ORB_ID(telemetry_status_0),
+ ORB_ID(telemetry_status_1),
+ ORB_ID(telemetry_status_2),
+ ORB_ID(telemetry_status_3),
+};
+
+// This is a hack to quiet an unused-variable warning for when telemetry_status.h is
+// included but telemetry_status_orb_id is not referenced. The inline works if you
+// choose to use it, but you can continue to just directly index into the array as well.
+// If you don't use the inline this ends up being a no-op with no additional code emitted.
+extern inline const struct orb_metadata *telemetry_status_orb_id_lookup(size_t index);
+extern inline const struct orb_metadata *telemetry_status_orb_id_lookup(size_t index)
+{
+ return telemetry_status_orb_id[index];
+}
#endif /* TOPIC_TELEMETRY_STATUS_H */
diff --git a/src/modules/uORB/topics/vehicle_attitude_setpoint.h b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
index d526a8ff2..8446e9c6e 100644
--- a/src/modules/uORB/topics/vehicle_attitude_setpoint.h
+++ b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
@@ -72,6 +72,8 @@ struct vehicle_attitude_setpoint_s {
float thrust; /**< Thrust in Newton the power system should generate */
bool roll_reset_integral; /**< Reset roll integral part (navigation logic change) */
+ bool pitch_reset_integral; /**< Reset pitch integral part (navigation logic change) */
+ bool yaw_reset_integral; /**< Reset yaw integral part (navigation logic change) */
};
diff --git a/src/modules/uORB/topics/vehicle_control_mode.h b/src/modules/uORB/topics/vehicle_control_mode.h
index ea554006f..49e2ba4b5 100644
--- a/src/modules/uORB/topics/vehicle_control_mode.h
+++ b/src/modules/uORB/topics/vehicle_control_mode.h
@@ -74,6 +74,7 @@ struct vehicle_control_mode_s {
bool flag_control_manual_enabled; /**< true if manual input is mixed in */
bool flag_control_auto_enabled; /**< true if onboard autopilot should act */
+ bool flag_control_offboard_enabled; /**< true if offboard control should be used */
bool flag_control_rates_enabled; /**< true if rates are stabilized */
bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */
bool flag_control_velocity_enabled; /**< true if horizontal velocity (implies direction) is controlled */
diff --git a/src/modules/uORB/topics/vehicle_force_setpoint.h b/src/modules/uORB/topics/vehicle_force_setpoint.h
new file mode 100644
index 000000000..e3a7360b2
--- /dev/null
+++ b/src/modules/uORB/topics/vehicle_force_setpoint.h
@@ -0,0 +1,65 @@
+/****************************************************************************
+ *
+ * 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 vehicle_force_setpoint.h
+ * @author Thomas Gubler <thomasgubler@gmail.com>
+ * Definition of force (NED) setpoint uORB topic. Typically this can be used
+ * by a position control app together with an attitude control app.
+ */
+
+#ifndef TOPIC_VEHICLE_FORCE_SETPOINT_H_
+#define TOPIC_VEHICLE_FORCE_SETPOINT_H_
+
+#include "../uORB.h"
+
+/**
+ * @addtogroup topics
+ * @{
+ */
+
+struct vehicle_force_setpoint_s {
+ float x; /**< in N NED */
+ float y; /**< in N NED */
+ float z; /**< in N NED */
+ float yaw; /**< right-hand rotation around downward axis (rad, equivalent to Tait-Bryan yaw) */
+}; /**< Desired force in NED frame */
+
+/**
+ * @}
+ */
+
+/* register this as object request broker structure */
+ORB_DECLARE(vehicle_force_setpoint);
+
+#endif
diff --git a/src/modules/uORB/topics/vehicle_global_position.h b/src/modules/uORB/topics/vehicle_global_position.h
index 4897ca737..e32529cb4 100644
--- a/src/modules/uORB/topics/vehicle_global_position.h
+++ b/src/modules/uORB/topics/vehicle_global_position.h
@@ -36,7 +36,7 @@
* Definition of the global fused WGS84 position uORB topic.
*
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
- * @author Julian Oes <joes@student.ethz.ch>
+ * @author Julian Oes <julian@oes.ch>
* @author Lorenz Meier <lm@inf.ethz.ch>
*/
@@ -61,15 +61,14 @@
* e.g. control inputs of the vehicle in a Kalman-filter implementation.
*/
struct vehicle_global_position_s {
- uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */
-
- uint64_t time_gps_usec; /**< GPS timestamp in microseconds */
+ uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */
+ uint64_t time_gps_usec; /**< GPS timestamp in microseconds */
double lat; /**< Latitude in degrees */
double lon; /**< Longitude in degrees */
float alt; /**< Altitude AMSL in meters */
- float vel_n; /**< Ground north velocity, m/s */
- float vel_e; /**< Ground east velocity, m/s */
- float vel_d; /**< Ground downside velocity, m/s */
+ float vel_n; /**< Ground north velocity, m/s */
+ float vel_e; /**< Ground east velocity, m/s */
+ float vel_d; /**< Ground downside velocity, m/s */
float yaw; /**< Yaw in radians -PI..+PI. */
float eph;
float epv;
diff --git a/src/modules/uORB/topics/vehicle_gps_position.h b/src/modules/uORB/topics/vehicle_gps_position.h
index 5924a324d..80d65cd69 100644
--- a/src/modules/uORB/topics/vehicle_gps_position.h
+++ b/src/modules/uORB/topics/vehicle_gps_position.h
@@ -61,12 +61,11 @@ struct vehicle_gps_position_s {
uint64_t timestamp_variance;
float s_variance_m_s; /**< speed accuracy estimate m/s */
- float p_variance_m; /**< position accuracy estimate m */
float c_variance_rad; /**< course accuracy estimate rad */
uint8_t fix_type; /**< 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. */
- float eph_m; /**< GPS HDOP horizontal dilution of position in m */
- float epv_m; /**< GPS VDOP horizontal dilution of position in m */
+ float eph; /**< GPS HDOP horizontal dilution of position in m */
+ float epv; /**< GPS VDOP horizontal dilution of position in m */
unsigned noise_per_ms; /**< */
unsigned jamming_indicator; /**< */
@@ -82,14 +81,7 @@ struct vehicle_gps_position_s {
uint64_t timestamp_time; /**< Timestamp for time information */
uint64_t time_gps_usec; /**< Timestamp (microseconds in GPS format), this is the timestamp which comes from the gps module */
- uint64_t timestamp_satellites; /**< Timestamp for sattelite information */
- uint8_t satellites_visible; /**< Number of satellites visible. If unknown, set to 255 */
- uint8_t satellite_prn[20]; /**< Global satellite ID */
- uint8_t satellite_used[20]; /**< 0: Satellite not used, 1: used for localization */
- uint8_t satellite_elevation[20]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
- uint8_t satellite_azimuth[20]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
- uint8_t satellite_snr[20]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
- bool satellite_info_available; /**< 0 for no info, 1 for info available */
+ uint8_t satellites_used; /**< Number of satellites used */
};
/**
diff --git a/src/modules/uORB/topics/vehicle_status.h b/src/modules/uORB/topics/vehicle_status.h
index ea20a317a..b46c00b75 100644
--- a/src/modules/uORB/topics/vehicle_status.h
+++ b/src/modules/uORB/topics/vehicle_status.h
@@ -1,10 +1,6 @@
/****************************************************************************
*
- * Copyright (C) 2012 PX4 Development Team. All rights reserved.
- * Author: @author Lorenz Meier <lm@inf.ethz.ch>
- * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch>
- * @author Thomas Gubler <thomasgubler@student.ethz.ch>
- * @author Julian Oes <joes@student.ethz.ch>
+ * Copyright (C) 2012 - 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
@@ -45,6 +41,11 @@
* All apps should write to subsystem_info:
*
* (any app) --> subsystem_info (published) --> (commander app state machine) --> vehicle_status --> (mavlink app)
+ *
+ * @author Lorenz Meier <lm@inf.ethz.ch>
+ * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch>
+ * @author Thomas Gubler <thomasgubler@student.ethz.ch>
+ * @author Julian Oes <julian@oes.ch>
*/
#ifndef VEHICLE_STATUS_H_
@@ -54,19 +55,22 @@
#include <stdbool.h>
#include "../uORB.h"
-#include <navigator/navigator_state.h>
-
/**
* @addtogroup topics @{
*/
-/* main state machine */
+/**
+ * Main state, i.e. what user wants. Controlled by RC or from ground station via telemetry link.
+ */
typedef enum {
MAIN_STATE_MANUAL = 0,
MAIN_STATE_ALTCTL,
MAIN_STATE_POSCTL,
- MAIN_STATE_AUTO,
+ MAIN_STATE_AUTO_MISSION,
+ MAIN_STATE_AUTO_LOITER,
+ MAIN_STATE_AUTO_RTL,
MAIN_STATE_ACRO,
+ MAIN_STATE_OFFBOARD,
MAIN_STATE_MAX
} main_state_t;
@@ -80,7 +84,7 @@ typedef enum {
ARMING_STATE_STANDBY_ERROR,
ARMING_STATE_REBOOT,
ARMING_STATE_IN_AIR_RESTORE,
- ARMING_STATE_MAX
+ ARMING_STATE_MAX,
} arming_state_t;
typedef enum {
@@ -88,13 +92,24 @@ typedef enum {
HIL_STATE_ON
} hil_state_t;
+/**
+ * Navigation state, i.e. "what should vehicle do".
+ */
typedef enum {
- FAILSAFE_STATE_NORMAL = 0, /**< Normal operation */
- FAILSAFE_STATE_RTL, /**< Return To Launch */
- FAILSAFE_STATE_LAND, /**< Land without position control */
- FAILSAFE_STATE_TERMINATION, /**< Disable motors and use parachute, can't be recovered */
- FAILSAFE_STATE_MAX
-} failsafe_state_t;
+ NAVIGATION_STATE_MANUAL = 0, /**< Manual mode */
+ NAVIGATION_STATE_ALTCTL, /**< Altitude control mode */
+ NAVIGATION_STATE_POSCTL, /**< Position control mode */
+ NAVIGATION_STATE_AUTO_MISSION, /**< Auto mission mode */
+ NAVIGATION_STATE_AUTO_LOITER, /**< Auto loiter mode */
+ NAVIGATION_STATE_AUTO_RTL, /**< Auto return to launch mode */
+ NAVIGATION_STATE_AUTO_RTGS, /**< Auto return to groundstation on data link loss */
+ NAVIGATION_STATE_ACRO, /**< Acro mode */
+ NAVIGATION_STATE_LAND, /**< Land mode */
+ NAVIGATION_STATE_DESCEND, /**< Descend mode (no position control) */
+ NAVIGATION_STATE_TERMINATION, /**< Termination mode */
+ NAVIGATION_STATE_OFFBOARD,
+ NAVIGATION_STATE_MAX,
+} navigation_state_t;
enum VEHICLE_MODE_FLAG {
VEHICLE_MODE_FLAG_SAFETY_ARMED = 128,
@@ -154,12 +169,11 @@ struct vehicle_status_s {
uint16_t counter; /**< incremented by the writing thread everytime new data is stored */
uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
- main_state_t main_state; /**< main state machine */
- unsigned int set_nav_state; /**< set navigation state machine to specified value */
- uint64_t set_nav_state_timestamp; /**< timestamp of latest change of set_nav_state */
+ main_state_t main_state; /**< main state machine */
+ navigation_state_t nav_state; /**< set navigation state machine to specified value */
arming_state_t arming_state; /**< current arming state */
- hil_state_t hil_state; /**< current hil state */
- failsafe_state_t failsafe_state; /**< current failsafe state */
+ hil_state_t hil_state; /**< current hil state */
+ bool failsafe; /**< true if system is in failsafe state */
int32_t system_type; /**< system type, inspired by MAVLink's VEHICLE_TYPE enum */
int32_t system_id; /**< system id, inspired by MAVLink's system ID field */
@@ -179,11 +193,15 @@ struct vehicle_status_s {
bool condition_local_altitude_valid;
bool condition_airspeed_valid; /**< set to true by the commander app if there is a valid airspeed measurement available */
bool condition_landed; /**< true if vehicle is landed, always true if disarmed */
+ bool condition_power_input_valid; /**< set if input power is valid */
+ float avionics_power_rail_voltage; /**< voltage of the avionics power rail */
bool rc_signal_found_once;
bool rc_signal_lost; /**< true if RC reception lost */
bool rc_input_blocked; /**< set if RC input should be ignored */
+ bool data_link_lost; /**< datalink to GCS lost */
+
bool offboard_control_signal_found_once;
bool offboard_control_signal_lost;
bool offboard_control_signal_weak;
@@ -206,6 +224,8 @@ struct vehicle_status_s {
uint16_t errors_count2;
uint16_t errors_count3;
uint16_t errors_count4;
+
+ bool circuit_breaker_engaged_power_check;
};
/**
diff --git a/src/modules/uORB/topics/wind_estimate.h b/src/modules/uORB/topics/wind_estimate.h
new file mode 100644
index 000000000..58333a64f
--- /dev/null
+++ b/src/modules/uORB/topics/wind_estimate.h
@@ -0,0 +1,68 @@
+/****************************************************************************
+ *
+ * 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 wind_estimate.h
+ *
+ * Wind estimate topic topic
+ *
+ */
+
+#ifndef TOPIC_WIND_ESTIMATE_H
+#define TOPIC_WIND_ESTIMATE_H
+
+#include <stdint.h>
+#include "../uORB.h"
+
+/**
+ * @addtogroup topics
+ * @{
+ */
+
+/** Wind estimate */
+struct wind_estimate_s {
+
+ uint64_t timestamp; /**< Microseconds since system boot */
+ float windspeed_north; /**< Wind component in north / X direction */
+ float windspeed_east; /**< Wind component in east / Y direction */
+ float covariance_north; /**< Uncertainty - set to zero (no uncertainty) if not estimated */
+ float covariance_east; /**< Uncertainty - set to zero (no uncertainty) if not estimated */
+};
+
+/**
+ * @}
+ */
+
+ORB_DECLARE(wind_estimate);
+
+#endif \ No newline at end of file