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Merge remote-tracking branch 'upstream/master' into offboard2_externalsetpointmessages

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Conflicts:
	src/modules/navigator/navigator.h
	src/modules/navigator/navigator_main.cpp
This commit is contained in:
Thomas Gubler
2014-10-05 13:17:32 +02:00
parent 9bda573151 80ed01a5b4
commit 7f9a231b40
116 changed files with 6051 additions and 1308 deletions
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src/modules/uORB/objects_common.cpp
+3
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@@ -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/multirotor_motor_limits.h"
ORB_DEFINE(multirotor_motor_limits, struct multirotor_motor_limits_s);
#include "topics/telemetry_status.h"
ORB_DEFINE(telemetry_status_0, struct telemetry_status_s);
ORB_DEFINE(telemetry_status_1, struct telemetry_status_s);
src/modules/uORB/topics/mission_result.h
+5 -2
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@@ -55,8 +55,11 @@ struct mission_result_s
{
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 */
bool reached; /**< true if mission has been reached */
bool finished; /**< true if mission has been completed */
bool stay_in_failsafe; /**< true if the commander should not switch out of the failsafe mode*/
bool geofence_violated; /**< true if the geofence is violated */
bool flight_termination; /**< true if the navigator demands a flight termination from the commander app */
};
/**
src/modules/uORB/topics/multirotor_motor_limits.h
+69
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@@ -0,0 +1,69 @@
/****************************************************************************
*
* Copyright (C) 2012-2013 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 multirotor_motor_limits.h
*
* Definition of multirotor_motor_limits topic
*/
#ifndef MULTIROTOR_MOTOR_LIMITS_H_
#define MULTIROTOR_MOTOR_LIMITS_H_
#include "../uORB.h"
#include <stdint.h>
/**
* @addtogroup topics
* @{
*/
/**
* Motor limits
*/
struct multirotor_motor_limits_s {
uint8_t roll_pitch : 1; // roll/pitch limit reached
uint8_t yaw : 1; // yaw limit reached
uint8_t throttle_lower : 1; // lower throttle limit reached
uint8_t throttle_upper : 1; // upper throttle limit reached
uint8_t reserved : 4;
};
/**
* @}
*/
/* register this as object request broker structure */
ORB_DECLARE(multirotor_motor_limits);
#endif
src/modules/uORB/topics/telemetry_status.h
+2
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@@ -67,6 +67,8 @@ struct telemetry_status_s {
uint8_t noise; /**< background noise level */
uint8_t remote_noise; /**< remote background noise level */
uint8_t txbuf; /**< how full the tx buffer is as a percentage */
uint8_t system_id; /**< system id of the remote system */
uint8_t component_id; /**< component id of the remote system */
};
/**
src/modules/uORB/topics/vehicle_command.h
+12 -7
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@@ -1,9 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2008-2012 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>
* 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
@@ -37,6 +34,10 @@
/**
* @file vehicle_command.h
* Definition of the vehicle command 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_VEHICLE_COMMAND_H_
@@ -52,6 +53,9 @@
* but can contain additional ones.
*/
enum VEHICLE_CMD {
VEHICLE_CMD_CUSTOM_0 = 0, /* test command */
VEHICLE_CMD_CUSTOM_1 = 1, /* test command */
VEHICLE_CMD_CUSTOM_2 = 2, /* test command */
VEHICLE_CMD_NAV_WAYPOINT = 16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
VEHICLE_CMD_NAV_LOITER_UNLIM = 17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
VEHICLE_CMD_NAV_LOITER_TURNS = 18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -90,7 +94,8 @@ enum VEHICLE_CMD {
VEHICLE_CMD_MISSION_START = 300, /* start running a mission |first_item: the first mission item to run| last_item: the last mission item to run (after this item is run, the mission ends)| */
VEHICLE_CMD_COMPONENT_ARM_DISARM = 400, /* Arms / Disarms a component |1 to arm, 0 to disarm| */
VEHICLE_CMD_START_RX_PAIR = 500, /* Starts receiver pairing |0:Spektrum| 0:Spektrum DSM2, 1:Spektrum DSMX| */
VEHICLE_CMD_ENUM_END = 501, /* | */
VEHICLE_CMD_PAYLOAD_PREPARE_DEPLOY = 30001, /**< Prepare a payload deployment in the flight plan */
VEHICLE_CMD_PAYLOAD_CONTROL_DEPLOY = 30002 /**< Control a pre-programmed payload deployment */
};
/**
@@ -118,8 +123,8 @@ struct vehicle_command_s {
float param2; /**< Parameter 2, as defined by MAVLink VEHICLE_CMD enum. */
float param3; /**< Parameter 3, as defined by MAVLink VEHICLE_CMD enum. */
float param4; /**< Parameter 4, as defined by MAVLink VEHICLE_CMD enum. */
float param5; /**< Parameter 5, as defined by MAVLink VEHICLE_CMD enum. */
float param6; /**< Parameter 6, as defined by MAVLink VEHICLE_CMD enum. */
double param5; /**< Parameter 5, as defined by MAVLink VEHICLE_CMD enum. */
double param6; /**< Parameter 6, as defined by MAVLink VEHICLE_CMD enum. */
float param7; /**< Parameter 7, as defined by MAVLink VEHICLE_CMD enum. */
enum VEHICLE_CMD command; /**< Command ID, as defined MAVLink by VEHICLE_CMD enum. */
uint8_t target_system; /**< System which should execute the command */
src/modules/uORB/topics/vehicle_global_position.h
+2
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@@ -72,6 +72,8 @@ struct vehicle_global_position_s {
float yaw; /**< Yaw in radians -PI..+PI. */
float eph; /**< Standard deviation of position estimate horizontally */
float epv; /**< Standard deviation of position vertically */
float terrain_alt; /**< Terrain altitude in m, WGS84 */
bool terrain_alt_valid; /**< Terrain altitude estimate is valid */
};
/**
src/modules/uORB/topics/vehicle_status.h
+15 -1
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@@ -102,7 +102,10 @@ typedef enum {
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_RCRECOVER, /**< RC recover mode */
NAVIGATION_STATE_AUTO_RTGS, /**< Auto return to groundstation on data link loss */
NAVIGATION_STATE_AUTO_LANDENGFAIL, /**< Auto land on engine failure */
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) */
@@ -198,9 +201,18 @@ struct vehicle_status_s {
bool rc_signal_found_once;
bool rc_signal_lost; /**< true if RC reception lost */
bool rc_signal_lost_cmd; /**< true if RC lost mode is commanded */
bool rc_input_blocked; /**< set if RC input should be ignored */
bool data_link_lost; /**< datalink to GCS lost */
bool data_link_lost; /**< datalink to GCS lost */
bool data_link_lost_cmd; /**< datalink to GCS lost mode commanded */
uint8_t data_link_lost_counter; /**< counts unique data link lost events */
bool engine_failure; /** Set to true if an engine failure is detected */
bool engine_failure_cmd; /** Set to true if an engine failure mode is commanded */
bool gps_failure; /** Set to true if a gps failure is detected */
bool gps_failure_cmd; /** Set to true if a gps failure mode is commanded */
bool barometer_failure; /** Set to true if a barometer failure is detected */
bool offboard_control_signal_found_once;
bool offboard_control_signal_lost;
@@ -229,6 +241,8 @@ struct vehicle_status_s {
bool circuit_breaker_engaged_power_check;
bool circuit_breaker_engaged_airspd_check;
bool circuit_breaker_engaged_enginefailure_check;
bool circuit_breaker_engaged_gpsfailure_check;
};
/**