mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-17 20:57:36 +08:00
Merge branch 'master' into acro2
This commit is contained in:
@@ -0,0 +1,80 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 Publication.cpp
|
||||
*
|
||||
*/
|
||||
|
||||
#include "Publication.hpp"
|
||||
#include "topics/vehicle_attitude.h"
|
||||
#include "topics/vehicle_local_position.h"
|
||||
#include "topics/vehicle_global_position.h"
|
||||
#include "topics/debug_key_value.h"
|
||||
#include "topics/actuator_controls.h"
|
||||
#include "topics/vehicle_global_velocity_setpoint.h"
|
||||
#include "topics/vehicle_attitude_setpoint.h"
|
||||
#include "topics/vehicle_rates_setpoint.h"
|
||||
#include "topics/actuator_outputs.h"
|
||||
#include "topics/encoders.h"
|
||||
|
||||
namespace uORB {
|
||||
|
||||
template<class T>
|
||||
Publication<T>::Publication(
|
||||
List<PublicationBase *> * list,
|
||||
const struct orb_metadata *meta) :
|
||||
T(), // initialize data structure to zero
|
||||
PublicationBase(list, meta) {
|
||||
}
|
||||
|
||||
template<class T>
|
||||
Publication<T>::~Publication() {}
|
||||
|
||||
template<class T>
|
||||
void * Publication<T>::getDataVoidPtr() {
|
||||
return (void *)(T *)(this);
|
||||
}
|
||||
|
||||
template class __EXPORT Publication<vehicle_attitude_s>;
|
||||
template class __EXPORT Publication<vehicle_local_position_s>;
|
||||
template class __EXPORT Publication<vehicle_global_position_s>;
|
||||
template class __EXPORT Publication<debug_key_value_s>;
|
||||
template class __EXPORT Publication<actuator_controls_s>;
|
||||
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<encoders_s>;
|
||||
|
||||
}
|
||||
@@ -0,0 +1,111 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 Publication.h
|
||||
*
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <containers/List.hpp>
|
||||
|
||||
|
||||
namespace uORB
|
||||
{
|
||||
|
||||
/**
|
||||
* Base publication warapper class, used in list traversal
|
||||
* of various publications.
|
||||
*/
|
||||
class __EXPORT PublicationBase : public ListNode<uORB::PublicationBase *>
|
||||
{
|
||||
public:
|
||||
|
||||
PublicationBase(
|
||||
List<PublicationBase *> * list,
|
||||
const struct orb_metadata *meta) :
|
||||
_meta(meta),
|
||||
_handle(-1) {
|
||||
if (list != NULL) list->add(this);
|
||||
}
|
||||
void update() {
|
||||
if (_handle > 0) {
|
||||
orb_publish(getMeta(), getHandle(), getDataVoidPtr());
|
||||
} else {
|
||||
setHandle(orb_advertise(getMeta(), getDataVoidPtr()));
|
||||
}
|
||||
}
|
||||
virtual void *getDataVoidPtr() = 0;
|
||||
virtual ~PublicationBase() {
|
||||
orb_unsubscribe(getHandle());
|
||||
}
|
||||
const struct orb_metadata *getMeta() { return _meta; }
|
||||
int getHandle() { return _handle; }
|
||||
protected:
|
||||
void setHandle(orb_advert_t handle) { _handle = handle; }
|
||||
const struct orb_metadata *_meta;
|
||||
orb_advert_t _handle;
|
||||
};
|
||||
|
||||
/**
|
||||
* Publication wrapper class
|
||||
*/
|
||||
template<class T>
|
||||
class Publication :
|
||||
public T, // this must be first!
|
||||
public PublicationBase
|
||||
{
|
||||
public:
|
||||
/**
|
||||
* Constructor
|
||||
*
|
||||
* @param list A list interface for adding to list during construction
|
||||
* @param meta The uORB metadata (usually from the ORB_ID() macro)
|
||||
* for the topic.
|
||||
*/
|
||||
Publication(List<PublicationBase *> * list,
|
||||
const struct orb_metadata *meta);
|
||||
virtual ~Publication();
|
||||
/*
|
||||
* XXX
|
||||
* This function gets the T struct, assuming
|
||||
* the struct is the first base class, this
|
||||
* should use dynamic cast, but doesn't
|
||||
* seem to be available
|
||||
*/
|
||||
void *getDataVoidPtr();
|
||||
};
|
||||
|
||||
} // namespace uORB
|
||||
@@ -0,0 +1,103 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 Subscription.cpp
|
||||
*
|
||||
*/
|
||||
|
||||
#include "Subscription.hpp"
|
||||
#include "topics/parameter_update.h"
|
||||
#include "topics/actuator_controls.h"
|
||||
#include "topics/vehicle_gps_position.h"
|
||||
#include "topics/sensor_combined.h"
|
||||
#include "topics/vehicle_attitude.h"
|
||||
#include "topics/vehicle_global_position.h"
|
||||
#include "topics/encoders.h"
|
||||
#include "topics/position_setpoint_triplet.h"
|
||||
#include "topics/vehicle_status.h"
|
||||
#include "topics/manual_control_setpoint.h"
|
||||
#include "topics/vehicle_local_position_setpoint.h"
|
||||
#include "topics/vehicle_local_position.h"
|
||||
#include "topics/vehicle_attitude_setpoint.h"
|
||||
#include "topics/vehicle_rates_setpoint.h"
|
||||
|
||||
namespace uORB
|
||||
{
|
||||
|
||||
bool __EXPORT SubscriptionBase::updated()
|
||||
{
|
||||
bool isUpdated = false;
|
||||
orb_check(_handle, &isUpdated);
|
||||
return isUpdated;
|
||||
}
|
||||
|
||||
template<class T>
|
||||
Subscription<T>::Subscription(
|
||||
List<SubscriptionBase *> * list,
|
||||
const struct orb_metadata *meta, unsigned interval) :
|
||||
T(), // initialize data structure to zero
|
||||
SubscriptionBase(list, meta) {
|
||||
setHandle(orb_subscribe(getMeta()));
|
||||
orb_set_interval(getHandle(), interval);
|
||||
}
|
||||
|
||||
template<class T>
|
||||
Subscription<T>::~Subscription() {}
|
||||
|
||||
template<class T>
|
||||
void * Subscription<T>::getDataVoidPtr() {
|
||||
return (void *)(T *)(this);
|
||||
}
|
||||
|
||||
template<class T>
|
||||
T Subscription<T>::getData() {
|
||||
return T(*this);
|
||||
}
|
||||
|
||||
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<sensor_combined_s>;
|
||||
template class __EXPORT Subscription<vehicle_attitude_s>;
|
||||
template class __EXPORT Subscription<vehicle_global_position_s>;
|
||||
template class __EXPORT Subscription<encoders_s>;
|
||||
template class __EXPORT Subscription<position_setpoint_triplet_s>;
|
||||
template class __EXPORT Subscription<vehicle_status_s>;
|
||||
template class __EXPORT Subscription<manual_control_setpoint_s>;
|
||||
template class __EXPORT Subscription<vehicle_local_position_setpoint_s>;
|
||||
template class __EXPORT Subscription<vehicle_local_position_s>;
|
||||
template class __EXPORT Subscription<vehicle_attitude_setpoint_s>;
|
||||
template class __EXPORT Subscription<vehicle_rates_setpoint_s>;
|
||||
|
||||
} // namespace uORB
|
||||
@@ -0,0 +1,128 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 Subscription.h
|
||||
*
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <containers/List.hpp>
|
||||
|
||||
|
||||
namespace uORB
|
||||
{
|
||||
|
||||
/**
|
||||
* Base subscription warapper class, used in list traversal
|
||||
* of various subscriptions.
|
||||
*/
|
||||
class __EXPORT SubscriptionBase :
|
||||
public ListNode<SubscriptionBase *>
|
||||
{
|
||||
public:
|
||||
// methods
|
||||
|
||||
/**
|
||||
* Constructor
|
||||
*
|
||||
* @param meta The uORB metadata (usually from the ORB_ID() macro)
|
||||
* for the topic.
|
||||
*/
|
||||
SubscriptionBase(
|
||||
List<SubscriptionBase *> * list,
|
||||
const struct orb_metadata *meta) :
|
||||
_meta(meta),
|
||||
_handle() {
|
||||
if (list != NULL) list->add(this);
|
||||
}
|
||||
bool updated();
|
||||
void update() {
|
||||
if (updated()) {
|
||||
orb_copy(_meta, _handle, getDataVoidPtr());
|
||||
}
|
||||
}
|
||||
virtual void *getDataVoidPtr() = 0;
|
||||
virtual ~SubscriptionBase() {
|
||||
orb_unsubscribe(_handle);
|
||||
}
|
||||
// accessors
|
||||
const struct orb_metadata *getMeta() { return _meta; }
|
||||
int getHandle() { return _handle; }
|
||||
protected:
|
||||
// accessors
|
||||
void setHandle(int handle) { _handle = handle; }
|
||||
// attributes
|
||||
const struct orb_metadata *_meta;
|
||||
int _handle;
|
||||
};
|
||||
|
||||
/**
|
||||
* Subscription wrapper class
|
||||
*/
|
||||
template<class T>
|
||||
class __EXPORT Subscription :
|
||||
public T, // this must be first!
|
||||
public SubscriptionBase
|
||||
{
|
||||
public:
|
||||
/**
|
||||
* Constructor
|
||||
*
|
||||
* @param list A list interface for adding to list during construction
|
||||
* @param meta The uORB metadata (usually from the ORB_ID() macro)
|
||||
* for the topic.
|
||||
* @param interval The minimum interval in milliseconds between updates
|
||||
*/
|
||||
Subscription(
|
||||
List<SubscriptionBase *> * list,
|
||||
const struct orb_metadata *meta, unsigned interval);
|
||||
/**
|
||||
* Deconstructor
|
||||
*/
|
||||
virtual ~Subscription();
|
||||
|
||||
/*
|
||||
* XXX
|
||||
* This function gets the T struct, assuming
|
||||
* the struct is the first base class, this
|
||||
* should use dynamic cast, but doesn't
|
||||
* seem to be available
|
||||
*/
|
||||
void *getDataVoidPtr();
|
||||
T getData();
|
||||
};
|
||||
|
||||
} // namespace uORB
|
||||
@@ -41,4 +41,6 @@ MODULE_COMMAND = uorb
|
||||
MODULE_STACKSIZE = 4096
|
||||
|
||||
SRCS = uORB.cpp \
|
||||
objects_common.cpp
|
||||
objects_common.cpp \
|
||||
Publication.cpp \
|
||||
Subscription.cpp
|
||||
|
||||
@@ -90,6 +90,9 @@ ORB_DEFINE(battery_status, struct battery_status_s);
|
||||
#include "topics/servorail_status.h"
|
||||
ORB_DEFINE(servorail_status, struct servorail_status_s);
|
||||
|
||||
#include "topics/system_power.h"
|
||||
ORB_DEFINE(system_power, struct system_power_s);
|
||||
|
||||
#include "topics/vehicle_global_position.h"
|
||||
ORB_DEFINE(vehicle_global_position, struct vehicle_global_position_s);
|
||||
|
||||
@@ -124,7 +127,7 @@ ORB_DEFINE(position_setpoint_triplet, struct position_setpoint_triplet_s);
|
||||
ORB_DEFINE(vehicle_global_velocity_setpoint, struct vehicle_global_velocity_setpoint_s);
|
||||
|
||||
#include "topics/mission.h"
|
||||
ORB_DEFINE(mission, struct mission_s);
|
||||
ORB_DEFINE(offboard_mission, struct mission_s);
|
||||
ORB_DEFINE(onboard_mission, struct mission_s);
|
||||
|
||||
#include "topics/mission_result.h"
|
||||
@@ -190,3 +193,9 @@ ORB_DEFINE(navigation_capabilities, struct navigation_capabilities_s);
|
||||
|
||||
#include "topics/esc_status.h"
|
||||
ORB_DEFINE(esc_status, struct esc_status_s);
|
||||
|
||||
#include "topics/encoders.h"
|
||||
ORB_DEFINE(encoders, struct encoders_s);
|
||||
|
||||
#include "topics/estimator_status.h"
|
||||
ORB_DEFINE(estimator_status, struct estimator_status_report);
|
||||
|
||||
@@ -52,9 +52,10 @@
|
||||
* Airspeed
|
||||
*/
|
||||
struct airspeed_s {
|
||||
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
|
||||
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
|
||||
float indicated_airspeed_m_s; /**< indicated airspeed in meters per second, -1 if unknown */
|
||||
float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
|
||||
float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
|
||||
float air_temperature_celsius; /**< air temperature in degrees celsius, -1000 if unknown */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -52,12 +52,14 @@
|
||||
* Differential pressure.
|
||||
*/
|
||||
struct differential_pressure_s {
|
||||
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
|
||||
uint64_t error_count;
|
||||
float differential_pressure_pa; /**< 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 */
|
||||
uint64_t timestamp; /**< Microseconds since system boot, needed to integrate */
|
||||
uint64_t error_count; /**< Number of errors detected by driver */
|
||||
float differential_pressure_pa; /**< Differential pressure reading */
|
||||
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 */
|
||||
|
||||
};
|
||||
|
||||
|
||||
@@ -0,0 +1,66 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 encoders.h
|
||||
*
|
||||
* Encoders topic.
|
||||
*
|
||||
*/
|
||||
|
||||
#ifndef TOPIC_ENCODERS_H
|
||||
#define TOPIC_ENCODERS_H
|
||||
|
||||
#include <stdint.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
|
||||
#define NUM_ENCODERS 4
|
||||
|
||||
struct encoders_s {
|
||||
uint64_t timestamp;
|
||||
int64_t counts[NUM_ENCODERS]; // counts of encoder
|
||||
float velocity[NUM_ENCODERS]; // counts of encoder/ second
|
||||
};
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
ORB_DECLARE(encoders);
|
||||
|
||||
#endif
|
||||
@@ -60,7 +60,7 @@
|
||||
enum ESC_VENDOR {
|
||||
ESC_VENDOR_GENERIC = 0, /**< generic ESC */
|
||||
ESC_VENDOR_MIKROKOPTER, /**< Mikrokopter */
|
||||
ESC_VENDOR_GRAUPNER_HOTT /**< Graupner HoTT ESC */
|
||||
ESC_VENDOR_GRAUPNER_HOTT /**< Graupner HoTT ESC */
|
||||
};
|
||||
|
||||
enum ESC_CONNECTION_TYPE {
|
||||
@@ -79,16 +79,15 @@ enum ESC_CONNECTION_TYPE {
|
||||
/**
|
||||
* Electronic speed controller status.
|
||||
*/
|
||||
struct esc_status_s
|
||||
{
|
||||
struct esc_status_s {
|
||||
/* use of a counter and timestamp recommended (but not necessary) */
|
||||
|
||||
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 */
|
||||
|
||||
|
||||
uint8_t esc_count; /**< number of connected ESCs */
|
||||
enum ESC_CONNECTION_TYPE esc_connectiontype; /**< how ESCs connected to the system */
|
||||
|
||||
|
||||
struct {
|
||||
uint16_t esc_address; /**< Address of current ESC (in most cases 1-8 / must be set by driver) */
|
||||
enum ESC_VENDOR esc_vendor; /**< Vendor of current ESC */
|
||||
|
||||
@@ -0,0 +1,80 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 estimator_status.h
|
||||
* Definition of the estimator_status_report uORB topic.
|
||||
*
|
||||
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||
*/
|
||||
|
||||
#ifndef ESTIMATOR_STATUS_H_
|
||||
#define ESTIMATOR_STATUS_H_
|
||||
|
||||
#include <stdint.h>
|
||||
#include <stdbool.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
|
||||
/**
|
||||
* Estimator status report.
|
||||
*
|
||||
* This is a generic status report struct which allows any of the onboard estimators
|
||||
* to write the internal state to the system log.
|
||||
*
|
||||
*/
|
||||
struct estimator_status_report {
|
||||
|
||||
/* NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes - change with consideration only */
|
||||
|
||||
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 */
|
||||
|
||||
};
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(estimator_status);
|
||||
|
||||
#endif
|
||||
@@ -53,8 +53,7 @@
|
||||
/**
|
||||
* Filtered bottom flow in bodyframe.
|
||||
*/
|
||||
struct filtered_bottom_flow_s
|
||||
{
|
||||
struct filtered_bottom_flow_s {
|
||||
uint64_t timestamp; /**< time of this estimate, in microseconds since system start */
|
||||
|
||||
float sumx; /**< Integrated bodyframe x flow in meters */
|
||||
|
||||
@@ -43,6 +43,16 @@
|
||||
#include <stdint.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
/**
|
||||
* Switch position
|
||||
*/
|
||||
typedef enum {
|
||||
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) */
|
||||
} switch_pos_t;
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
@@ -51,33 +61,43 @@
|
||||
struct manual_control_setpoint_s {
|
||||
uint64_t timestamp;
|
||||
|
||||
float roll; /**< ailerons roll / roll rate input */
|
||||
float pitch; /**< elevator / pitch / pitch rate */
|
||||
float yaw; /**< rudder / yaw rate / yaw */
|
||||
float throttle; /**< throttle / collective thrust / altitude */
|
||||
|
||||
float mode_switch; /**< mode 3 position switch (mandatory): manual, assisted, auto */
|
||||
float return_switch; /**< land 2 position switch (mandatory): land, no effect */
|
||||
float assisted_switch; /**< assisted 2 position switch (optional): seatbelt, simple */
|
||||
float mission_switch; /**< mission 2 position switch (optional): mission, loiter */
|
||||
float acro_switch; /**< acro 2 position switch (optional): normal, acro */
|
||||
|
||||
/**
|
||||
* Any of the channels below may not be available and be set to NaN
|
||||
* Any of the channels may not be available and be set to NaN
|
||||
* to indicate that it does not contain valid data.
|
||||
* The variable names follow the definition of the
|
||||
* MANUAL_CONTROL mavlink message.
|
||||
* The default range is from -1 to 1 (mavlink message -1000 to 1000)
|
||||
* The range for the z variable is defined from 0 to 1. (The z field of
|
||||
* the MANUAL_CONTROL mavlink message is defined from -1000 to 1000)
|
||||
*/
|
||||
float x; /**< stick position in x direction -1..1
|
||||
in general corresponds to forward/back motion or pitch of vehicle,
|
||||
in general a positive value means forward or negative pitch and
|
||||
a negative value means backward or positive pitch */
|
||||
float y; /**< stick position in y direction -1..1
|
||||
in general corresponds to right/left motion or roll of vehicle,
|
||||
in general a positive value means right or positive roll and
|
||||
a negative value means left or negative roll */
|
||||
float z; /**< throttle stick position 0..1
|
||||
in general corresponds to up/down motion or thrust of vehicle,
|
||||
in general the value corresponds to the demanded throttle by the user,
|
||||
if the input is used for setting the setpoint of a vertical position
|
||||
controller any value > 0.5 means up and any value < 0.5 means down */
|
||||
float r; /**< yaw stick/twist positon, -1..1
|
||||
in general corresponds to the righthand rotation around the vertical
|
||||
(downwards) axis of the vehicle */
|
||||
float flaps; /**< flap position */
|
||||
float aux1; /**< default function: camera yaw / azimuth */
|
||||
float aux2; /**< default function: camera pitch / tilt */
|
||||
float aux3; /**< default function: camera trigger */
|
||||
float aux4; /**< default function: camera roll */
|
||||
float aux5; /**< default function: payload drop */
|
||||
|
||||
// XXX needed or parameter?
|
||||
//float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */
|
||||
|
||||
float flaps; /**< flap position */
|
||||
|
||||
float aux1; /**< default function: camera yaw / azimuth */
|
||||
float aux2; /**< default function: camera pitch / tilt */
|
||||
float aux3; /**< default function: camera trigger */
|
||||
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 */
|
||||
}; /**< manual control inputs */
|
||||
|
||||
/**
|
||||
|
||||
@@ -77,8 +77,7 @@ enum ORIGIN {
|
||||
* This is the position the MAV is heading towards. If it of type loiter,
|
||||
* the MAV is circling around it with the given loiter radius in meters.
|
||||
*/
|
||||
struct mission_item_s
|
||||
{
|
||||
struct mission_item_s {
|
||||
bool altitude_is_relative; /**< true if altitude is relative from start point */
|
||||
double lat; /**< latitude in degrees */
|
||||
double lon; /**< longitude in degrees */
|
||||
@@ -106,7 +105,7 @@ struct mission_s
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(mission);
|
||||
ORB_DECLARE(offboard_mission);
|
||||
ORB_DECLARE(onboard_mission);
|
||||
|
||||
#endif
|
||||
|
||||
@@ -54,7 +54,8 @@
|
||||
struct mission_result_s
|
||||
{
|
||||
bool mission_reached; /**< true if mission has been reached */
|
||||
unsigned mission_index; /**< index of the mission which has been reached */
|
||||
unsigned mission_index_reached; /**< index of the mission which has been reached */
|
||||
unsigned index_current_mission; /**< index of the current mission */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -52,12 +52,12 @@
|
||||
* Airspeed
|
||||
*/
|
||||
struct navigation_capabilities_s {
|
||||
float turn_distance; /**< the optimal distance to a waypoint to switch to the next */
|
||||
float turn_distance; /**< the optimal distance to a waypoint to switch to the next */
|
||||
|
||||
/* Landing parameters: see fw_pos_control_l1/landingslope.h */
|
||||
float landing_horizontal_slope_displacement;
|
||||
float landing_slope_angle_rad;
|
||||
float landing_flare_length;
|
||||
/* Landing parameters: see fw_pos_control_l1/landingslope.h */
|
||||
float landing_horizontal_slope_displacement;
|
||||
float landing_slope_angle_rad;
|
||||
float landing_flare_length;
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -45,12 +45,11 @@
|
||||
|
||||
/**
|
||||
* Off-board control inputs.
|
||||
*
|
||||
*
|
||||
* Typically sent by a ground control station / joystick or by
|
||||
* some off-board controller via C or SIMULINK.
|
||||
*/
|
||||
enum OFFBOARD_CONTROL_MODE
|
||||
{
|
||||
enum OFFBOARD_CONTROL_MODE {
|
||||
OFFBOARD_CONTROL_MODE_DIRECT = 0,
|
||||
OFFBOARD_CONTROL_MODE_DIRECT_RATES = 1,
|
||||
OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE = 2,
|
||||
|
||||
@@ -57,6 +57,7 @@ struct optical_flow_s {
|
||||
|
||||
uint64_t timestamp; /**< in microseconds since system start */
|
||||
|
||||
uint64_t flow_timestamp; /**< timestamp from flow sensor */
|
||||
int16_t flow_raw_x; /**< flow in pixels in X direction, not rotation-compensated */
|
||||
int16_t flow_raw_y; /**< flow in pixels in Y direction, not rotation-compensated */
|
||||
float flow_comp_x_m; /**< speed over ground in meters, rotation-compensated */
|
||||
|
||||
@@ -54,24 +54,24 @@
|
||||
|
||||
enum SETPOINT_TYPE
|
||||
{
|
||||
SETPOINT_TYPE_NORMAL = 0, /**< normal setpoint */
|
||||
SETPOINT_TYPE_LOITER, /**< loiter setpoint */
|
||||
SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */
|
||||
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) */
|
||||
};
|
||||
|
||||
struct position_setpoint_s
|
||||
{
|
||||
bool valid; /**< true if setpoint is valid */
|
||||
bool valid; /**< true if setpoint is valid */
|
||||
enum SETPOINT_TYPE type; /**< setpoint type to adjust behavior of position controller */
|
||||
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 */
|
||||
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 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 */
|
||||
float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -85,7 +85,7 @@ struct position_setpoint_triplet_s
|
||||
struct position_setpoint_s current;
|
||||
struct position_setpoint_s next;
|
||||
|
||||
nav_state_t nav_state; /**< navigation state */
|
||||
nav_state_t nav_state; /**< navigation state */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -52,30 +52,29 @@
|
||||
*/
|
||||
#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[].
|
||||
*/
|
||||
enum RC_CHANNELS_FUNCTION
|
||||
{
|
||||
THROTTLE = 0,
|
||||
ROLL,
|
||||
PITCH,
|
||||
YAW,
|
||||
MODE,
|
||||
RETURN,
|
||||
ASSISTED,
|
||||
MISSION,
|
||||
OFFBOARD_MODE,
|
||||
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. */
|
||||
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. */
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -86,16 +85,17 @@ enum RC_CHANNELS_FUNCTION
|
||||
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 */
|
||||
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 */
|
||||
/*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 */
|
||||
}; /**< radio control channels. */
|
||||
|
||||
/**
|
||||
|
||||
@@ -77,34 +77,36 @@ struct sensor_combined_s {
|
||||
|
||||
/* NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes Change with consideration only */
|
||||
|
||||
uint64_t timestamp; /**< Timestamp in microseconds since boot */
|
||||
uint64_t timestamp; /**< Timestamp in microseconds since boot, from gyro */
|
||||
|
||||
int16_t gyro_raw[3]; /**< Raw sensor values of angular velocity */
|
||||
uint16_t gyro_counter; /**< Number of raw measurments taken */
|
||||
float gyro_rad_s[3]; /**< Angular velocity in radian per seconds */
|
||||
|
||||
|
||||
int16_t accelerometer_raw[3]; /**< Raw acceleration in NED body frame */
|
||||
uint32_t accelerometer_counter; /**< Number of raw acc measurements taken */
|
||||
float accelerometer_m_s2[3]; /**< Acceleration in NED body frame, in m/s^2 */
|
||||
int accelerometer_mode; /**< Accelerometer measurement mode */
|
||||
float accelerometer_range_m_s2; /**< Accelerometer measurement range in m/s^2 */
|
||||
uint64_t accelerometer_timestamp; /**< Accelerometer timestamp */
|
||||
|
||||
int16_t magnetometer_raw[3]; /**< Raw magnetic field in NED body frame */
|
||||
float magnetometer_ga[3]; /**< Magnetic field in NED body frame, in Gauss */
|
||||
int magnetometer_mode; /**< Magnetometer measurement mode */
|
||||
float magnetometer_range_ga; /**< ± measurement range in Gauss */
|
||||
float magnetometer_cuttoff_freq_hz; /**< Internal analog low pass frequency of sensor */
|
||||
uint32_t magnetometer_counter; /**< Number of raw mag measurements taken */
|
||||
|
||||
uint64_t magnetometer_timestamp; /**< Magnetometer timestamp */
|
||||
|
||||
float baro_pres_mbar; /**< Barometric pressure, already temp. comp. */
|
||||
float baro_alt_meter; /**< Altitude, already temp. comp. */
|
||||
float baro_temp_celcius; /**< Temperature in degrees celsius */
|
||||
float adc_voltage_v[4]; /**< ADC voltages of ADC Chan 10/11/12/13 or -1 */
|
||||
float adc_voltage_v[10]; /**< ADC voltages of ADC Chan 10/11/12/13 or -1 */
|
||||
unsigned adc_mapping[10]; /**< Channel indices of each of these values */
|
||||
float mcu_temp_celcius; /**< Internal temperature measurement of MCU */
|
||||
uint32_t baro_counter; /**< Number of raw baro measurements taken */
|
||||
uint64_t baro_timestamp; /**< Barometer timestamp */
|
||||
|
||||
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
|
||||
uint64_t differential_pressure_timestamp; /**< Last measurement timestamp */
|
||||
float differential_pressure_filtered_pa; /**< Low pass filtered airspeed sensor differential pressure reading */
|
||||
|
||||
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
|
||||
uint32_t differential_pressure_counter; /**< Number of raw differential pressure measurements taken */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -50,8 +50,7 @@
|
||||
#include <stdbool.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
enum SUBSYSTEM_TYPE
|
||||
{
|
||||
enum SUBSYSTEM_TYPE {
|
||||
SUBSYSTEM_TYPE_GYRO = 1,
|
||||
SUBSYSTEM_TYPE_ACC = 2,
|
||||
SUBSYSTEM_TYPE_MAG = 4,
|
||||
|
||||
@@ -0,0 +1,71 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 system_power.h
|
||||
*
|
||||
* Definition of the system_power voltage and power status uORB topic.
|
||||
*/
|
||||
|
||||
#ifndef SYSTEM_POWER_H_
|
||||
#define SYSTEM_POWER_H_
|
||||
|
||||
#include "../uORB.h"
|
||||
#include <stdint.h>
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
|
||||
/**
|
||||
* voltage and power supply status
|
||||
*/
|
||||
struct system_power_s {
|
||||
uint64_t timestamp; /**< microseconds since system boot */
|
||||
float voltage5V_v; /**< peripheral 5V rail voltage */
|
||||
uint8_t usb_connected:1; /**< USB is connected when 1 */
|
||||
uint8_t brick_valid:1; /**< brick power is good when 1 */
|
||||
uint8_t servo_valid:1; /**< servo power is good when 1 */
|
||||
uint8_t periph_5V_OC:1; /**< peripheral overcurrent when 1 */
|
||||
uint8_t hipower_5V_OC:1; /**< hi power peripheral overcurrent when 1 */
|
||||
};
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(system_power);
|
||||
|
||||
#endif
|
||||
@@ -44,10 +44,10 @@
|
||||
#include "../uORB.h"
|
||||
|
||||
enum TELEMETRY_STATUS_RADIO_TYPE {
|
||||
TELEMETRY_STATUS_RADIO_TYPE_GENERIC = 0,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_WIRE
|
||||
TELEMETRY_STATUS_RADIO_TYPE_GENERIC = 0,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET,
|
||||
TELEMETRY_STATUS_RADIO_TYPE_WIRE
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -57,14 +57,14 @@ enum TELEMETRY_STATUS_RADIO_TYPE {
|
||||
|
||||
struct telemetry_status_s {
|
||||
uint64_t timestamp;
|
||||
enum TELEMETRY_STATUS_RADIO_TYPE type; /**< type of the radio hardware */
|
||||
uint8_t rssi; /**< local signal strength */
|
||||
uint8_t remote_rssi; /**< remote signal strength */
|
||||
uint16_t rxerrors; /**< receive errors */
|
||||
uint16_t fixed; /**< count of error corrected packets */
|
||||
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 */
|
||||
enum TELEMETRY_STATUS_RADIO_TYPE type; /**< type of the radio hardware */
|
||||
uint8_t rssi; /**< local signal strength */
|
||||
uint8_t remote_rssi; /**< remote signal strength */
|
||||
uint16_t rxerrors; /**< receive errors */
|
||||
uint16_t fixed; /**< count of error corrected packets */
|
||||
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 */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -76,7 +76,7 @@ struct vehicle_attitude_s {
|
||||
float rate_offsets[3]; /**< Offsets of the body angular rates from zero */
|
||||
float R[3][3]; /**< Rotation matrix body to world, (Tait-Bryan, NED) */
|
||||
float q[4]; /**< Quaternion (NED) */
|
||||
float g_comp[3]; /**< Compensated gravity vector */
|
||||
float g_comp[3]; /**< Compensated gravity vector */
|
||||
bool R_valid; /**< Rotation matrix valid */
|
||||
bool q_valid; /**< Quaternion valid */
|
||||
|
||||
|
||||
@@ -52,8 +52,7 @@
|
||||
/**
|
||||
* vehicle attitude setpoint.
|
||||
*/
|
||||
struct vehicle_attitude_setpoint_s
|
||||
{
|
||||
struct vehicle_attitude_setpoint_s {
|
||||
uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
|
||||
|
||||
float roll_body; /**< body angle in NED frame */
|
||||
|
||||
@@ -48,8 +48,7 @@
|
||||
* @{
|
||||
*/
|
||||
|
||||
struct vehicle_bodyframe_speed_setpoint_s
|
||||
{
|
||||
struct vehicle_bodyframe_speed_setpoint_s {
|
||||
uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
|
||||
|
||||
float vx; /**< in m/s */
|
||||
|
||||
@@ -51,43 +51,42 @@
|
||||
* Should contain all commands from MAVLink's VEHICLE_CMD ENUM,
|
||||
* but can contain additional ones.
|
||||
*/
|
||||
enum VEHICLE_CMD
|
||||
{
|
||||
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| */
|
||||
VEHICLE_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_NAV_LAND=21, /* Land at location |Empty| Empty| Empty| Desired yaw angle.| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
|
||||
VEHICLE_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
|
||||
VEHICLE_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */
|
||||
VEHICLE_CMD_CONDITION_DISTANCE=114, /* Delay mission state machine until within desired distance of next NAV point. |Distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_YAW=115, /* Reach a certain target angle. |target angle: [0-360], 0 is north| speed during yaw change:[deg per second]| direction: negative: counter clockwise, positive: clockwise [-1,1]| relative offset or absolute angle: [ 1,0]| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_LAST=159, /* NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_MODE=176, /* Set system mode. |Mode, as defined by ENUM MAV_MODE| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_JUMP=177, /* Jump to the desired command in the mission list. Repeat this action only the specified number of times |Sequence number| Repeat count| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_CHANGE_SPEED=178, /* Change speed and/or throttle set points. |Speed type (0=Airspeed, 1=Ground Speed)| Speed (m/s, -1 indicates no change)| Throttle ( Percent, -1 indicates no change)| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_HOME=179, /* Changes the home location either to the current location or a specified location. |Use current (1=use current location, 0=use specified location)| Empty| Empty| Empty| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_DO_SET_PARAMETER=180, /* Set a system parameter. Caution! Use of this command requires knowledge of the numeric enumeration value of the parameter. |Parameter number| Parameter value| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_RELAY=181, /* Set a relay to a condition. |Relay number| Setting (1=on, 0=off, others possible depending on system hardware)| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_REPEAT_RELAY=182, /* Cycle a relay on and off for a desired number of cyles with a desired period. |Relay number| Cycle count| Cycle time (seconds, decimal)| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_SERVO=183, /* Set a servo to a desired PWM value. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */
|
||||
VEHICLE_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_OVERRIDE_GOTO=252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */
|
||||
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, /* | */
|
||||
enum VEHICLE_CMD {
|
||||
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| */
|
||||
VEHICLE_CMD_NAV_LOITER_TIME = 19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_RETURN_TO_LAUNCH = 20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_NAV_LAND = 21, /* Land at location |Empty| Empty| Empty| Desired yaw angle.| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_TAKEOFF = 22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_NAV_ROI = 80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
|
||||
VEHICLE_CMD_NAV_PATHPLANNING = 81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
|
||||
VEHICLE_CMD_NAV_LAST = 95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_DELAY = 112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_CHANGE_ALT = 113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */
|
||||
VEHICLE_CMD_CONDITION_DISTANCE = 114, /* Delay mission state machine until within desired distance of next NAV point. |Distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_YAW = 115, /* Reach a certain target angle. |target angle: [0-360], 0 is north| speed during yaw change:[deg per second]| direction: negative: counter clockwise, positive: clockwise [-1,1]| relative offset or absolute angle: [ 1,0]| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_CONDITION_LAST = 159, /* NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_MODE = 176, /* Set system mode. |Mode, as defined by ENUM MAV_MODE| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_JUMP = 177, /* Jump to the desired command in the mission list. Repeat this action only the specified number of times |Sequence number| Repeat count| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_CHANGE_SPEED = 178, /* Change speed and/or throttle set points. |Speed type (0=Airspeed, 1=Ground Speed)| Speed (m/s, -1 indicates no change)| Throttle ( Percent, -1 indicates no change)| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_HOME = 179, /* Changes the home location either to the current location or a specified location. |Use current (1=use current location, 0=use specified location)| Empty| Empty| Empty| Latitude| Longitude| Altitude| */
|
||||
VEHICLE_CMD_DO_SET_PARAMETER = 180, /* Set a system parameter. Caution! Use of this command requires knowledge of the numeric enumeration value of the parameter. |Parameter number| Parameter value| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_RELAY = 181, /* Set a relay to a condition. |Relay number| Setting (1=on, 0=off, others possible depending on system hardware)| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_REPEAT_RELAY = 182, /* Cycle a relay on and off for a desired number of cyles with a desired period. |Relay number| Cycle count| Cycle time (seconds, decimal)| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_SET_SERVO = 183, /* Set a servo to a desired PWM value. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_REPEAT_SERVO = 184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_CONTROL_VIDEO = 200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_DO_LAST = 240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_CALIBRATION = 241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS = 242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */
|
||||
VEHICLE_CMD_PREFLIGHT_STORAGE = 245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN = 246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */
|
||||
VEHICLE_CMD_OVERRIDE_GOTO = 252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */
|
||||
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, /* | */
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -96,14 +95,13 @@ enum VEHICLE_CMD
|
||||
* Should contain all of MAVLink's VEHICLE_CMD_RESULT values
|
||||
* but can contain additional ones.
|
||||
*/
|
||||
enum VEHICLE_CMD_RESULT
|
||||
{
|
||||
VEHICLE_CMD_RESULT_ACCEPTED=0, /* Command ACCEPTED and EXECUTED | */
|
||||
VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED=1, /* Command TEMPORARY REJECTED/DENIED | */
|
||||
VEHICLE_CMD_RESULT_DENIED=2, /* Command PERMANENTLY DENIED | */
|
||||
VEHICLE_CMD_RESULT_UNSUPPORTED=3, /* Command UNKNOWN/UNSUPPORTED | */
|
||||
VEHICLE_CMD_RESULT_FAILED=4, /* Command executed, but failed | */
|
||||
VEHICLE_CMD_RESULT_ENUM_END=5, /* | */
|
||||
enum VEHICLE_CMD_RESULT {
|
||||
VEHICLE_CMD_RESULT_ACCEPTED = 0, /* Command ACCEPTED and EXECUTED | */
|
||||
VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED = 1, /* Command TEMPORARY REJECTED/DENIED | */
|
||||
VEHICLE_CMD_RESULT_DENIED = 2, /* Command PERMANENTLY DENIED | */
|
||||
VEHICLE_CMD_RESULT_UNSUPPORTED = 3, /* Command UNKNOWN/UNSUPPORTED | */
|
||||
VEHICLE_CMD_RESULT_FAILED = 4, /* Command executed, but failed | */
|
||||
VEHICLE_CMD_RESULT_ENUM_END = 5, /* | */
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -111,8 +109,7 @@ enum VEHICLE_CMD_RESULT
|
||||
* @{
|
||||
*/
|
||||
|
||||
struct vehicle_command_s
|
||||
{
|
||||
struct vehicle_command_s {
|
||||
float param1; /**< Parameter 1, as defined by MAVLink VEHICLE_CMD enum. */
|
||||
float param2; /**< Parameter 2, as defined by MAVLink VEHICLE_CMD enum. */
|
||||
float param3; /**< Parameter 3, as defined by MAVLink VEHICLE_CMD enum. */
|
||||
|
||||
@@ -47,8 +47,7 @@
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
struct vehicle_control_debug_s
|
||||
{
|
||||
struct vehicle_control_debug_s {
|
||||
uint64_t timestamp; /**< in microseconds since system start */
|
||||
|
||||
float roll_p; /**< roll P control part */
|
||||
@@ -77,9 +76,9 @@ struct vehicle_control_debug_s
|
||||
|
||||
}; /**< vehicle_control_debug */
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(vehicle_control_debug);
|
||||
|
||||
@@ -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
|
||||
@@ -38,8 +34,13 @@
|
||||
/**
|
||||
* @file vehicle_control_mode.h
|
||||
* Definition of the vehicle_control_mode uORB topic.
|
||||
*
|
||||
*
|
||||
* All control apps should depend their actions based on the flags set here.
|
||||
*
|
||||
* @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>
|
||||
*/
|
||||
|
||||
#ifndef VEHICLE_CONTROL_MODE
|
||||
@@ -61,8 +62,7 @@
|
||||
* Encodes the complete system state and is set by the commander app.
|
||||
*/
|
||||
|
||||
struct vehicle_control_mode_s
|
||||
{
|
||||
struct vehicle_control_mode_s {
|
||||
uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
|
||||
|
||||
bool flag_armed;
|
||||
|
||||
@@ -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>
|
||||
* 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_global_position.h
|
||||
* Definition of the global fused WGS84 position uORB topic.
|
||||
*
|
||||
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||
* @author Julian Oes <joes@student.ethz.ch>
|
||||
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||
*/
|
||||
|
||||
#ifndef VEHICLE_GLOBAL_POSITION_T_H_
|
||||
@@ -59,13 +60,9 @@
|
||||
* estimator, which will take more sources of information into account than just GPS,
|
||||
* e.g. control inputs of the vehicle in a Kalman-filter implementation.
|
||||
*/
|
||||
struct vehicle_global_position_s
|
||||
{
|
||||
struct vehicle_global_position_s {
|
||||
uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */
|
||||
|
||||
bool global_valid; /**< true if position satisfies validity criteria of estimator */
|
||||
bool baro_valid; /**< true if baro_alt is valid (vel_d is also valid in this case) */
|
||||
|
||||
uint64_t time_gps_usec; /**< GPS timestamp in microseconds */
|
||||
double lat; /**< Latitude in degrees */
|
||||
double lon; /**< Longitude in degrees */
|
||||
@@ -74,8 +71,8 @@ struct vehicle_global_position_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 baro_alt; /**< Barometric altitude (not raw baro but fused with accelerometer) */
|
||||
float eph;
|
||||
float epv;
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -47,8 +47,7 @@
|
||||
* @{
|
||||
*/
|
||||
|
||||
struct vehicle_global_velocity_setpoint_s
|
||||
{
|
||||
struct vehicle_global_velocity_setpoint_s {
|
||||
float vx; /**< in m/s NED */
|
||||
float vy; /**< in m/s NED */
|
||||
float vz; /**< in m/s NED */
|
||||
|
||||
@@ -53,13 +53,12 @@
|
||||
/**
|
||||
* GPS position in WGS84 coordinates.
|
||||
*/
|
||||
struct vehicle_gps_position_s
|
||||
{
|
||||
struct vehicle_gps_position_s {
|
||||
uint64_t timestamp_position; /**< Timestamp for position information */
|
||||
int32_t lat; /**< Latitude in 1E-7 degrees */
|
||||
int32_t lon; /**< Longitude in 1E-7 degrees */
|
||||
int32_t alt; /**< Altitude in 1E-3 meters (millimeters) above MSL */
|
||||
|
||||
|
||||
uint64_t timestamp_variance;
|
||||
float s_variance_m_s; /**< speed accuracy estimate m/s */
|
||||
float p_variance_m; /**< position accuracy estimate m */
|
||||
|
||||
@@ -1,7 +1,6 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||
* Author: @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
|
||||
@@ -35,6 +34,9 @@
|
||||
/**
|
||||
* @file vehicle_local_position.h
|
||||
* Definition of the local fused NED position uORB topic.
|
||||
*
|
||||
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||
* @author Anton Babushkin <anton.babushkin@me.com>
|
||||
*/
|
||||
|
||||
#ifndef TOPIC_VEHICLE_LOCAL_POSITION_H_
|
||||
@@ -52,8 +54,7 @@
|
||||
/**
|
||||
* Fused local position in NED.
|
||||
*/
|
||||
struct vehicle_local_position_s
|
||||
{
|
||||
struct vehicle_local_position_s {
|
||||
uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */
|
||||
bool xy_valid; /**< true if x and y are valid */
|
||||
bool z_valid; /**< true if z is valid */
|
||||
@@ -73,8 +74,8 @@ struct vehicle_local_position_s
|
||||
bool xy_global; /**< true if position (x, y) is valid and has valid global reference (ref_lat, ref_lon) */
|
||||
bool z_global; /**< true if z is valid and has valid global reference (ref_alt) */
|
||||
uint64_t ref_timestamp; /**< Time when reference position was set */
|
||||
int32_t ref_lat; /**< Reference point latitude in 1E7 degrees */
|
||||
int32_t ref_lon; /**< Reference point longitude in 1E7 degrees */
|
||||
double ref_lat; /**< Reference point latitude in degrees */
|
||||
double ref_lon; /**< Reference point longitude in degrees */
|
||||
float ref_alt; /**< Reference altitude AMSL in meters, MUST be set to current (not at reference point!) ground level */
|
||||
bool landed; /**< true if vehicle is landed */
|
||||
/* Distance to surface */
|
||||
|
||||
@@ -49,8 +49,7 @@
|
||||
* @{
|
||||
*/
|
||||
|
||||
struct vehicle_local_position_setpoint_s
|
||||
{
|
||||
struct vehicle_local_position_setpoint_s {
|
||||
float x; /**< in meters NED */
|
||||
float y; /**< in meters NED */
|
||||
float z; /**< in meters NED */
|
||||
|
||||
@@ -47,8 +47,7 @@
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
struct vehicle_rates_setpoint_s
|
||||
{
|
||||
struct vehicle_rates_setpoint_s {
|
||||
uint64_t timestamp; /**< in microseconds since system start */
|
||||
|
||||
float roll; /**< body angular rates in NED frame */
|
||||
@@ -58,9 +57,9 @@ struct vehicle_rates_setpoint_s
|
||||
|
||||
}; /**< vehicle_rates_setpoint */
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(vehicle_rates_setpoint);
|
||||
|
||||
@@ -63,13 +63,15 @@
|
||||
/* main state machine */
|
||||
typedef enum {
|
||||
MAIN_STATE_MANUAL = 0,
|
||||
MAIN_STATE_ACRO,
|
||||
MAIN_STATE_SEATBELT,
|
||||
MAIN_STATE_EASY,
|
||||
MAIN_STATE_ALTCTL,
|
||||
MAIN_STATE_POSCTL,
|
||||
MAIN_STATE_AUTO,
|
||||
MAIN_STATE_ACRO,
|
||||
MAIN_STATE_MAX
|
||||
} main_state_t;
|
||||
|
||||
// If you change the order, add or remove arming_state_t states make sure to update the arrays
|
||||
// in state_machine_helper.cpp as well.
|
||||
typedef enum {
|
||||
ARMING_STATE_INIT = 0,
|
||||
ARMING_STATE_STANDBY,
|
||||
@@ -94,35 +96,6 @@ typedef enum {
|
||||
FAILSAFE_STATE_MAX
|
||||
} failsafe_state_t;
|
||||
|
||||
typedef enum {
|
||||
MODE_SWITCH_MANUAL = 0,
|
||||
MODE_SWITCH_ASSISTED,
|
||||
MODE_SWITCH_AUTO
|
||||
} mode_switch_pos_t;
|
||||
|
||||
typedef enum {
|
||||
ASSISTED_SWITCH_SEATBELT = 0,
|
||||
ASSISTED_SWITCH_EASY
|
||||
} assisted_switch_pos_t;
|
||||
|
||||
typedef enum {
|
||||
RETURN_SWITCH_NONE = 0,
|
||||
RETURN_SWITCH_NORMAL,
|
||||
RETURN_SWITCH_RETURN
|
||||
} return_switch_pos_t;
|
||||
|
||||
typedef enum {
|
||||
MISSION_SWITCH_NONE = 0,
|
||||
MISSION_SWITCH_LOITER,
|
||||
MISSION_SWITCH_MISSION
|
||||
} mission_switch_pos_t;
|
||||
|
||||
typedef enum {
|
||||
ACRO_SWITCH_NONE = 0,
|
||||
ACRO_SWITCH_NORMAL,
|
||||
ACRO_SWITCH_ACRO
|
||||
} acro_switch_pos_t;
|
||||
|
||||
enum VEHICLE_MODE_FLAG {
|
||||
VEHICLE_MODE_FLAG_SAFETY_ARMED = 128,
|
||||
VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED = 64,
|
||||
@@ -138,31 +111,31 @@ enum VEHICLE_MODE_FLAG {
|
||||
* Should match 1:1 MAVLink's MAV_TYPE ENUM
|
||||
*/
|
||||
enum VEHICLE_TYPE {
|
||||
VEHICLE_TYPE_GENERIC=0, /* Generic micro air vehicle. | */
|
||||
VEHICLE_TYPE_FIXED_WING=1, /* Fixed wing aircraft. | */
|
||||
VEHICLE_TYPE_QUADROTOR=2, /* Quadrotor | */
|
||||
VEHICLE_TYPE_COAXIAL=3, /* Coaxial helicopter | */
|
||||
VEHICLE_TYPE_HELICOPTER=4, /* Normal helicopter with tail rotor. | */
|
||||
VEHICLE_TYPE_ANTENNA_TRACKER=5, /* Ground installation | */
|
||||
VEHICLE_TYPE_GCS=6, /* Operator control unit / ground control station | */
|
||||
VEHICLE_TYPE_AIRSHIP=7, /* Airship, controlled | */
|
||||
VEHICLE_TYPE_FREE_BALLOON=8, /* Free balloon, uncontrolled | */
|
||||
VEHICLE_TYPE_ROCKET=9, /* Rocket | */
|
||||
VEHICLE_TYPE_GROUND_ROVER=10, /* Ground rover | */
|
||||
VEHICLE_TYPE_SURFACE_BOAT=11, /* Surface vessel, boat, ship | */
|
||||
VEHICLE_TYPE_SUBMARINE=12, /* Submarine | */
|
||||
VEHICLE_TYPE_HEXAROTOR=13, /* Hexarotor | */
|
||||
VEHICLE_TYPE_OCTOROTOR=14, /* Octorotor | */
|
||||
VEHICLE_TYPE_TRICOPTER=15, /* Octorotor | */
|
||||
VEHICLE_TYPE_FLAPPING_WING=16, /* Flapping wing | */
|
||||
VEHICLE_TYPE_KITE=17, /* Kite | */
|
||||
VEHICLE_TYPE_ENUM_END=18, /* | */
|
||||
VEHICLE_TYPE_GENERIC = 0, /* Generic micro air vehicle. | */
|
||||
VEHICLE_TYPE_FIXED_WING = 1, /* Fixed wing aircraft. | */
|
||||
VEHICLE_TYPE_QUADROTOR = 2, /* Quadrotor | */
|
||||
VEHICLE_TYPE_COAXIAL = 3, /* Coaxial helicopter | */
|
||||
VEHICLE_TYPE_HELICOPTER = 4, /* Normal helicopter with tail rotor. | */
|
||||
VEHICLE_TYPE_ANTENNA_TRACKER = 5, /* Ground installation | */
|
||||
VEHICLE_TYPE_GCS = 6, /* Operator control unit / ground control station | */
|
||||
VEHICLE_TYPE_AIRSHIP = 7, /* Airship, controlled | */
|
||||
VEHICLE_TYPE_FREE_BALLOON = 8, /* Free balloon, uncontrolled | */
|
||||
VEHICLE_TYPE_ROCKET = 9, /* Rocket | */
|
||||
VEHICLE_TYPE_GROUND_ROVER = 10, /* Ground rover | */
|
||||
VEHICLE_TYPE_SURFACE_BOAT = 11, /* Surface vessel, boat, ship | */
|
||||
VEHICLE_TYPE_SUBMARINE = 12, /* Submarine | */
|
||||
VEHICLE_TYPE_HEXAROTOR = 13, /* Hexarotor | */
|
||||
VEHICLE_TYPE_OCTOROTOR = 14, /* Octorotor | */
|
||||
VEHICLE_TYPE_TRICOPTER = 15, /* Octorotor | */
|
||||
VEHICLE_TYPE_FLAPPING_WING = 16, /* Flapping wing | */
|
||||
VEHICLE_TYPE_KITE = 17, /* Kite | */
|
||||
VEHICLE_TYPE_ENUM_END = 18, /* | */
|
||||
};
|
||||
|
||||
enum VEHICLE_BATTERY_WARNING {
|
||||
VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */
|
||||
VEHICLE_BATTERY_WARNING_LOW, /**< warning of low voltage */
|
||||
VEHICLE_BATTERY_WARNING_CRITICAL /**< alerting of critical voltage */
|
||||
VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */
|
||||
VEHICLE_BATTERY_WARNING_LOW, /**< warning of low voltage */
|
||||
VEHICLE_BATTERY_WARNING_CRITICAL /**< alerting of critical voltage */
|
||||
};
|
||||
|
||||
/**
|
||||
@@ -175,8 +148,7 @@ enum VEHICLE_BATTERY_WARNING {
|
||||
*
|
||||
* Encodes the complete system state and is set by the commander app.
|
||||
*/
|
||||
struct vehicle_status_s
|
||||
{
|
||||
struct vehicle_status_s {
|
||||
/* use of a counter and timestamp recommended (but not necessary) */
|
||||
|
||||
uint16_t counter; /**< incremented by the writing thread everytime new data is stored */
|
||||
@@ -195,12 +167,6 @@ struct vehicle_status_s
|
||||
|
||||
bool is_rotary_wing;
|
||||
|
||||
mode_switch_pos_t mode_switch;
|
||||
return_switch_pos_t return_switch;
|
||||
assisted_switch_pos_t assisted_switch;
|
||||
mission_switch_pos_t mission_switch;
|
||||
acro_switch_pos_t acro_switch;
|
||||
|
||||
bool condition_battery_voltage_valid;
|
||||
bool condition_system_in_air_restore; /**< true if we can restore in mid air */
|
||||
bool condition_system_sensors_initialized;
|
||||
@@ -227,7 +193,7 @@ struct vehicle_status_s
|
||||
uint32_t onboard_control_sensors_present;
|
||||
uint32_t onboard_control_sensors_enabled;
|
||||
uint32_t onboard_control_sensors_health;
|
||||
|
||||
|
||||
float load; /**< processor load from 0 to 1 */
|
||||
float battery_voltage;
|
||||
float battery_current;
|
||||
|
||||
@@ -52,8 +52,7 @@
|
||||
/**
|
||||
* Fused local position in NED.
|
||||
*/
|
||||
struct vehicle_vicon_position_s
|
||||
{
|
||||
struct vehicle_vicon_position_s {
|
||||
uint64_t timestamp; /**< time of this estimate, in microseconds since system start */
|
||||
bool valid; /**< true if position satisfies validity criteria of estimator */
|
||||
|
||||
|
||||
Reference in New Issue
Block a user