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LibrePilot/flight/modules/StateEstimation/stateestimation.c

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/**
******************************************************************************
* @addtogroup OpenPilotModules OpenPilot Modules
* @{
* @addtogroup State Estimation
* @brief Acquires sensor data and computes state estimate
* @{
*
* @file stateestimation.c
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2013.
* @brief Module to handle all comms to the AHRS on a periodic basis.
*
* @see The GNU Public License (GPL) Version 3
*
******************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#include "inc/stateestimation.h"
#include <callbackinfo.h>
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#include <gyrosensor.h>
#include <accelsensor.h>
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#include <magsensor.h>
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#include <barosensor.h>
#include <airspeedsensor.h>
#include <gpspositionsensor.h>
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#include <gpsvelocitysensor.h>
#include <homelocation.h>
#include <auxmagsensor.h>
#include <auxmagsettings.h>
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#include <gyrostate.h>
#include <accelstate.h>
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#include <magstate.h>
#include <airspeedstate.h>
#include <attitudestate.h>
#include <positionstate.h>
#include <velocitystate.h>
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#include "revosettings.h"
#include "flightstatus.h"
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#include "CoordinateConversions.h"
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// Private constants
#define STACK_SIZE_BYTES 256
#define CALLBACK_PRIORITY CALLBACK_PRIORITY_REGULAR
#define TASK_PRIORITY CALLBACK_TASK_FLIGHTCONTROL
#define TIMEOUT_MS 10
// Private filter init const
#define FILTER_INIT_FORCE -1
#define FILTER_INIT_IF_POSSIBLE -2
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// local macros, ONLY to be used in the middle of StateEstimationCb in section RUNSTATE_LOAD after the update of states updated!
#define FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(sensorname, shortname, a1, a2, a3) \
if (IS_SET(states.updated, SENSORUPDATES_##shortname)) { \
sensorname##Data s; \
sensorname##Get(&s); \
if (IS_REAL(s.a1) && IS_REAL(s.a2) && IS_REAL(s.a3)) { \
states.shortname[0] = s.a1; \
states.shortname[1] = s.a2; \
states.shortname[2] = s.a3; \
} \
else { \
UNSET_MASK(states.updated, SENSORUPDATES_##shortname); \
} \
}
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#define FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_1_DIMENSION_WITH_CUSTOM_EXTRA_CHECK(sensorname, shortname, a1, EXTRACHECK) \
if (IS_SET(states.updated, SENSORUPDATES_##shortname)) { \
sensorname##Data s; \
sensorname##Get(&s); \
if (IS_REAL(s.a1) && EXTRACHECK) { \
states.shortname[0] = s.a1; \
} \
else { \
UNSET_MASK(states.updated, SENSORUPDATES_##shortname); \
} \
}
#define FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_2_DIMENSION_WITH_CUSTOM_EXTRA_CHECK(sensorname, shortname, a1, a2, EXTRACHECK) \
if (IS_SET(states.updated, SENSORUPDATES_##shortname)) { \
sensorname##Data s; \
sensorname##Get(&s); \
if (IS_REAL(s.a1) && IS_REAL(s.a2) && EXTRACHECK) { \
states.shortname[0] = s.a1; \
states.shortname[1] = s.a2; \
} \
else { \
UNSET_MASK(states.updated, SENSORUPDATES_##shortname); \
} \
}
// local macros, ONLY to be used in the middle of StateEstimationCb in section RUNSTATE_SAVE before the check of alarms!
#define EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_3_DIMENSIONS(statename, shortname, a1, a2, a3) \
if (IS_SET(states.updated, SENSORUPDATES_##shortname)) { \
statename##Data s; \
statename##Get(&s); \
s.a1 = states.shortname[0]; \
s.a2 = states.shortname[1]; \
s.a3 = states.shortname[2]; \
statename##Set(&s); \
}
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#define EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_2_DIMENSIONS(statename, shortname, a1, a2) \
if (IS_SET(states.updated, SENSORUPDATES_##shortname)) { \
statename##Data s; \
statename##Get(&s); \
s.a1 = states.shortname[0]; \
s.a2 = states.shortname[1]; \
statename##Set(&s); \
}
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// Private types
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struct filterPipelineStruct;
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typedef const struct filterPipelineStruct {
const stateFilter *filter;
const struct filterPipelineStruct *next;
} filterPipeline;
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// Private variables
static DelayedCallbackInfo *stateEstimationCallback;
static volatile RevoSettingsData revoSettings;
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static volatile sensorUpdates updatedSensors;
static volatile int32_t fusionAlgorithm = -1;
static const filterPipeline *filterChain = NULL;
// different filters available to state estimation
static stateFilter magFilter;
static stateFilter baroFilter;
static stateFilter baroiFilter;
static stateFilter velocityFilter;
static stateFilter altitudeFilter;
static stateFilter airFilter;
static stateFilter stationaryFilter;
static stateFilter llaFilter;
static stateFilter cfFilter;
static stateFilter cfmFilter;
static stateFilter ekf13iFilter;
static stateFilter ekf13Filter;
// this is a hack to provide a computational shortcut for faster gyro state progression
static float gyroRaw[3];
static float gyroDelta[3];
// preconfigured filter chains selectable via revoSettings.FusionAlgorithm
static const filterPipeline *cfQueue = &(filterPipeline) {
.filter = &airFilter,
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.next = &(filterPipeline) {
.filter = &baroiFilter,
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.next = &(filterPipeline) {
.filter = &altitudeFilter,
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.next = &(filterPipeline) {
.filter = &cfFilter,
.next = NULL,
}
}
}
};
static const filterPipeline *cfmiQueue = &(filterPipeline) {
.filter = &magFilter,
.next = &(filterPipeline) {
.filter = &airFilter,
.next = &(filterPipeline) {
.filter = &baroiFilter,
.next = &(filterPipeline) {
.filter = &altitudeFilter,
.next = &(filterPipeline) {
.filter = &cfmFilter,
.next = NULL,
}
}
}
}
};
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static const filterPipeline *cfmQueue = &(filterPipeline) {
.filter = &magFilter,
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.next = &(filterPipeline) {
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.filter = &airFilter,
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.next = &(filterPipeline) {
.filter = &llaFilter,
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.next = &(filterPipeline) {
.filter = &baroFilter,
.next = &(filterPipeline) {
.filter = &altitudeFilter,
.next = &(filterPipeline) {
.filter = &cfmFilter,
.next = NULL,
}
}
}
}
}
};
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static const filterPipeline *ekf13iQueue = &(filterPipeline) {
.filter = &magFilter,
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.next = &(filterPipeline) {
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.filter = &airFilter,
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.next = &(filterPipeline) {
.filter = &baroiFilter,
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.next = &(filterPipeline) {
.filter = &stationaryFilter,
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.next = &(filterPipeline) {
.filter = &ekf13iFilter,
.next = &(filterPipeline) {
.filter = &velocityFilter,
.next = NULL,
}
}
}
}
}
};
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static const filterPipeline *ekf13Queue = &(filterPipeline) {
.filter = &magFilter,
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.next = &(filterPipeline) {
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.filter = &airFilter,
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.next = &(filterPipeline) {
.filter = &llaFilter,
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.next = &(filterPipeline) {
.filter = &baroFilter,
.next = &(filterPipeline) {
.filter = &ekf13Filter,
.next = &(filterPipeline) {
.filter = &velocityFilter,
.next = NULL,
}
}
}
}
}
};
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// Private functions
static void settingsUpdatedCb(UAVObjEvent *objEv);
static void sensorUpdatedCb(UAVObjEvent *objEv);
static void criticalConfigUpdatedCb(UAVObjEvent *objEv);
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static void StateEstimationCb(void);
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static inline int32_t maxint32_t(int32_t a, int32_t b)
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{
if (a > b) {
return a;
}
return b;
}
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/**
* Initialise the module. Called before the start function
* \returns 0 on success or -1 if initialisation failed
*/
int32_t StateEstimationInitialize(void)
{
RevoSettingsInitialize();
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GyroSensorInitialize();
MagSensorInitialize();
AuxMagSensorInitialize();
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BaroSensorInitialize();
AirspeedSensorInitialize();
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GPSVelocitySensorInitialize();
GPSPositionSensorInitialize();
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HomeLocationInitialize();
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GyroStateInitialize();
AccelStateInitialize();
MagStateInitialize();
AirspeedStateInitialize();
PositionStateInitialize();
VelocityStateInitialize();
AuxMagSettingsInitialize();
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RevoSettingsConnectCallback(&settingsUpdatedCb);
HomeLocationConnectCallback(&criticalConfigUpdatedCb);
AuxMagSettingsConnectCallback(&criticalConfigUpdatedCb);
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GyroSensorConnectCallback(&sensorUpdatedCb);
AccelSensorConnectCallback(&sensorUpdatedCb);
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MagSensorConnectCallback(&sensorUpdatedCb);
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BaroSensorConnectCallback(&sensorUpdatedCb);
AirspeedSensorConnectCallback(&sensorUpdatedCb);
AuxMagSensorConnectCallback(&sensorUpdatedCb);
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GPSVelocitySensorConnectCallback(&sensorUpdatedCb);
GPSPositionSensorConnectCallback(&sensorUpdatedCb);
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uint32_t stack_required = STACK_SIZE_BYTES;
// Initialize Filters
stack_required = maxint32_t(stack_required, filterMagInitialize(&magFilter));
stack_required = maxint32_t(stack_required, filterBaroiInitialize(&baroiFilter));
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stack_required = maxint32_t(stack_required, filterBaroInitialize(&baroFilter));
stack_required = maxint32_t(stack_required, filterVelocityInitialize(&velocityFilter));
stack_required = maxint32_t(stack_required, filterAltitudeInitialize(&altitudeFilter));
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stack_required = maxint32_t(stack_required, filterAirInitialize(&airFilter));
stack_required = maxint32_t(stack_required, filterStationaryInitialize(&stationaryFilter));
stack_required = maxint32_t(stack_required, filterLLAInitialize(&llaFilter));
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stack_required = maxint32_t(stack_required, filterCFInitialize(&cfFilter));
stack_required = maxint32_t(stack_required, filterCFMInitialize(&cfmFilter));
stack_required = maxint32_t(stack_required, filterEKF13iInitialize(&ekf13iFilter));
stack_required = maxint32_t(stack_required, filterEKF13Initialize(&ekf13Filter));
stateEstimationCallback = PIOS_CALLBACKSCHEDULER_Create(&StateEstimationCb, CALLBACK_PRIORITY, TASK_PRIORITY, CALLBACKINFO_RUNNING_STATEESTIMATION, stack_required);
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return 0;
}
/**
* Start the task. Expects all objects to be initialized by this point.
* \returns 0 on success or -1 if initialisation failed
*/
int32_t StateEstimationStart(void)
{
RevoSettingsConnectCallback(&settingsUpdatedCb);
// Force settings update to make sure rotation loaded
settingsUpdatedCb(NULL);
return 0;
}
MODULE_INITCALL(StateEstimationInitialize, StateEstimationStart);
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/**
* Module callback
*/
static void StateEstimationCb(void)
{
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static filterResult alarm = FILTERRESULT_OK;
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static filterResult lastAlarm = FILTERRESULT_UNINITIALISED;
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static uint16_t alarmcounter = 0;
static const filterPipeline *current;
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static stateEstimation states;
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static uint32_t last_time;
static uint16_t bootDelay = 64;
// after system startup, first few sensor readings might be messed up, delay until everything has settled
if (bootDelay) {
bootDelay--;
PIOS_CALLBACKSCHEDULER_Schedule(stateEstimationCallback, TIMEOUT_MS, CALLBACK_UPDATEMODE_SOONER);
return;
}
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alarm = FILTERRESULT_OK;
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// set alarm to warning if called through timeout
if (updatedSensors == 0) {
if (PIOS_DELAY_DiffuS(last_time) > 1000 * TIMEOUT_MS) {
alarm = FILTERRESULT_WARNING;
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}
} else {
last_time = PIOS_DELAY_GetRaw();
}
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// check if a new filter chain should be initialized
if (fusionAlgorithm != revoSettings.FusionAlgorithm) {
FlightStatusData fs;
FlightStatusGet(&fs);
if (fs.Armed == FLIGHTSTATUS_ARMED_DISARMED || fusionAlgorithm == FILTER_INIT_FORCE) {
const filterPipeline *newFilterChain;
switch ((RevoSettingsFusionAlgorithmOptions)revoSettings.FusionAlgorithm) {
case REVOSETTINGS_FUSIONALGORITHM_BASICCOMPLEMENTARY:
newFilterChain = cfQueue;
break;
case REVOSETTINGS_FUSIONALGORITHM_COMPLEMENTARYMAG:
newFilterChain = cfmiQueue;
break;
case REVOSETTINGS_FUSIONALGORITHM_COMPLEMENTARYMAGGPSOUTDOOR:
newFilterChain = cfmQueue;
break;
case REVOSETTINGS_FUSIONALGORITHM_INS13INDOOR:
newFilterChain = ekf13iQueue;
break;
case REVOSETTINGS_FUSIONALGORITHM_GPSNAVIGATIONINS13:
newFilterChain = ekf13Queue;
break;
default:
newFilterChain = NULL;
}
// initialize filters in chain
current = newFilterChain;
bool error = 0;
while (current != NULL) {
int32_t result = current->filter->init((stateFilter *)current->filter);
if (result != 0) {
error = 1;
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break;
}
current = current->next;
}
if (error) {
AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_ERROR);
return;
} else {
// set new fusion algortithm
filterChain = newFilterChain;
fusionAlgorithm = revoSettings.FusionAlgorithm;
}
}
}
// read updated sensor UAVObjects and set initial state
states.updated = updatedSensors;
updatedSensors = 0;
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// fetch sensors, check values, and load into state struct
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(GyroSensor, gyro, x, y, z);
if (IS_SET(states.updated, SENSORUPDATES_gyro)) {
gyroRaw[0] = states.gyro[0];
gyroRaw[1] = states.gyro[1];
gyroRaw[2] = states.gyro[2];
}
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(AccelSensor, accel, x, y, z);
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(MagSensor, boardMag, x, y, z);
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(AuxMagSensor, auxMag, x, y, z);
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_3_DIMENSIONS(GPSVelocitySensor, vel, North, East, Down);
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_1_DIMENSION_WITH_CUSTOM_EXTRA_CHECK(BaroSensor, baro, Altitude, true);
FETCH_SENSOR_FROM_UAVOBJECT_CHECK_AND_LOAD_TO_STATE_2_DIMENSION_WITH_CUSTOM_EXTRA_CHECK(AirspeedSensor, airspeed, CalibratedAirspeed, TrueAirspeed, s.SensorConnected == AIRSPEEDSENSOR_SENSORCONNECTED_TRUE);
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// GPS position data (LLA) is not fetched here since it does not contain floats. The filter must do all checks itself
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// at this point sensor state is stored in "states" with some rudimentary filtering applied
// apply all filters in the current filter chain
current = filterChain;
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// we are not done, re-dispatch self execution
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while (current) {
filterResult result = current->filter->filter((stateFilter *)current->filter, &states);
if (result > alarm) {
alarm = result;
}
current = current->next;
}
// the final output of filters is saved in state variables
// EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_3_DIMENSIONS(GyroState, gyro, x, y, z) // replaced by performance shortcut
if (IS_SET(states.updated, SENSORUPDATES_gyro)) {
gyroDelta[0] = states.gyro[0] - gyroRaw[0];
gyroDelta[1] = states.gyro[1] - gyroRaw[1];
gyroDelta[2] = states.gyro[2] - gyroRaw[2];
}
EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_3_DIMENSIONS(AccelState, accel, x, y, z);
if (IS_SET(states.updated, SENSORUPDATES_mag)) {
MagStateData s;
MagStateGet(&s);
s.x = states.mag[0];
s.y = states.mag[1];
s.z = states.mag[2];
switch (states.magStatus) {
case MAGSTATUS_OK:
s.Source = MAGSTATE_SOURCE_ONBOARD;
break;
case MAGSTATUS_AUX:
s.Source = MAGSTATE_SOURCE_AUX;
break;
default:
s.Source = MAGSTATE_SOURCE_INVALID;
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}
MagStateSet(&s);
}
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EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_3_DIMENSIONS(PositionState, pos, North, East, Down);
EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_3_DIMENSIONS(VelocityState, vel, North, East, Down);
EXPORT_STATE_TO_UAVOBJECT_IF_UPDATED_2_DIMENSIONS(AirspeedState, airspeed, CalibratedAirspeed, TrueAirspeed);
// attitude nees manual conversion from quaternion to euler
if (IS_SET(states.updated, SENSORUPDATES_attitude)) { \
AttitudeStateData s;
AttitudeStateGet(&s);
s.q1 = states.attitude[0];
s.q2 = states.attitude[1];
s.q3 = states.attitude[2];
s.q4 = states.attitude[3];
Quaternion2RPY(&s.q1, &s.Roll);
AttitudeStateSet(&s);
}
// throttle alarms, raise alarm flags immediately
// but require system to run for a while before decreasing
// to prevent alarm flapping
if (alarm >= lastAlarm) {
lastAlarm = alarm;
alarmcounter = 0;
} else {
if (alarmcounter < 100) {
alarmcounter++;
} else {
lastAlarm = alarm;
alarmcounter = 0;
}
}
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// clear alarms if everything is alright, then schedule callback execution after timeout
if (lastAlarm == FILTERRESULT_WARNING) {
AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_WARNING);
} else if (lastAlarm == FILTERRESULT_CRITICAL) {
AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_CRITICAL);
} else if (lastAlarm >= FILTERRESULT_ERROR) {
AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_ERROR);
} else {
AlarmsClear(SYSTEMALARMS_ALARM_ATTITUDE);
}
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if (updatedSensors) {
PIOS_CALLBACKSCHEDULER_Dispatch(stateEstimationCallback);
} else {
PIOS_CALLBACKSCHEDULER_Schedule(stateEstimationCallback, TIMEOUT_MS, CALLBACK_UPDATEMODE_SOONER);
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}
}
/**
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* Callback for eventdispatcher when RevoSettings has been updated
*/
static void settingsUpdatedCb(__attribute__((unused)) UAVObjEvent *ev)
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{
RevoSettingsGet((RevoSettingsData *)&revoSettings);
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}
/**
* Callback for eventdispatcher when HomeLocation or other critical configs (auxmagsettings, ...) has been updated
*/
static void criticalConfigUpdatedCb(__attribute__((unused)) UAVObjEvent *ev)
{
// Ask for a filter init (necessary for LLA filter)
// Only possible if disarmed
fusionAlgorithm = FILTER_INIT_IF_POSSIBLE;
}
/**
* Callback for eventdispatcher when any sensor UAVObject has been updated
* updates the list of "recently updated UAVObjects" and dispatches the state estimator callback
*/
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static void sensorUpdatedCb(UAVObjEvent *ev)
{
if (!ev) {
return;
}
if (ev->obj == GyroSensorHandle()) {
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updatedSensors |= SENSORUPDATES_gyro;
// shortcut - update GyroState right away
GyroSensorData s;
GyroStateData t;
GyroSensorGet(&s);
t.x = s.x + gyroDelta[0];
t.y = s.y + gyroDelta[1];
t.z = s.z + gyroDelta[2];
GyroStateSet(&t);
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}
if (ev->obj == AccelSensorHandle()) {
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updatedSensors |= SENSORUPDATES_accel;
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}
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if (ev->obj == MagSensorHandle()) {
updatedSensors |= SENSORUPDATES_boardMag;
}
if (ev->obj == AuxMagSensorHandle()) {
updatedSensors |= SENSORUPDATES_auxMag;
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}
if (ev->obj == GPSPositionSensorHandle()) {
updatedSensors |= SENSORUPDATES_lla;
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}
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if (ev->obj == GPSVelocitySensorHandle()) {
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updatedSensors |= SENSORUPDATES_vel;
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}
if (ev->obj == BaroSensorHandle()) {
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updatedSensors |= SENSORUPDATES_baro;
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}
if (ev->obj == AirspeedSensorHandle()) {
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updatedSensors |= SENSORUPDATES_airspeed;
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}
PIOS_CALLBACKSCHEDULER_Dispatch(stateEstimationCallback);
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}
/**
* @}
* @}
*/