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LibrePilot/flight/Modules/Sensors/sensors.c
James Cotton f8e59443b8 If the BMA180 isn't read when an IRQ fires (because the flash chip has claimed
the bus) then it won't fire another interrupt until read.  For now this is
dealt with in the sensor loop by forcing a read when the fifo is empty.
2012-01-21 10:13:46 -06:00

434 lines
13 KiB
C

/**
******************************************************************************
* @addtogroup OpenPilotModules OpenPilot Modules
* @{
* @addtogroup Sensors
* @brief Acquires sensor data
* Specifically updates the the @ref Gyros, @ref Accels, and @ref Magnetometer objects
* @{
*
* @file sensors.c
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
* @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
*/
/**
* Input objects: None, takes sensor data via pios
* Output objects: @ref Gyros @ref Accels @ref Magnetometer
*
* The module executes in its own thread.
*
* UAVObjects are automatically generated by the UAVObjectGenerator from
* the object definition XML file.
*
* Modules have no API, all communication to other modules is done through UAVObjects.
* However modules may use the API exposed by shared libraries.
* See the OpenPilot wiki for more details.
* http://www.openpilot.org/OpenPilot_Application_Architecture
*
*/
#include "pios.h"
#include "attitude.h"
#include "magnetometer.h"
#include "accels.h"
#include "gyros.h"
#include "gyrosbias.h"
#include "attitudeactual.h"
#include "attitudesettings.h"
#include "revocalibration.h"
#include "flightstatus.h"
#include "gpsposition.h"
#include "baroaltitude.h"
#include "CoordinateConversions.h"
// Private constants
#define STACK_SIZE_BYTES 1540
#define TASK_PRIORITY (tskIDLE_PRIORITY+3)
#define SENSOR_PERIOD 2
#define F_PI 3.14159265358979323846f
#define PI_MOD(x) (fmod(x + F_PI, F_PI * 2) - F_PI)
// Private types
// Private variables
static xTaskHandle sensorsTaskHandle;
static bool gps_updated = false;
static bool baro_updated = false;
// Private functions
static void SensorsTask(void *parameters);
static void settingsUpdatedCb(UAVObjEvent * objEv);
static void sensorsUpdatedCb(UAVObjEvent * objEv);
// These values are initialized by settings but can be updated by the attitude algorithm
static bool bias_correct_gyro = true;
static float mag_bias[3] = {0,0,0};
static float mag_scale[3] = {0,0,0};
static float accel_bias[3] = {0,0,0};
static float accel_scale[3] = {0,0,0};
/**
* API for sensor fusion algorithms:
* Configure(xQueueHandle gyro, xQueueHandle accel, xQueueHandle mag, xQueueHandle baro)
* Stores all the queues the algorithm will pull data from
* FinalizeSensors() -- before saving the sensors modifies them based on internal state (gyro bias)
* Update() -- queries queues and updates the attitude estiamte
*/
/**
* Initialise the module. Called before the start function
* \returns 0 on success or -1 if initialisation failed
*/
int32_t SensorsInitialize(void)
{
GyrosInitialize();
GyrosBiasInitialize();
AccelsInitialize();
MagnetometerInitialize();
RevoCalibrationInitialize();
RevoCalibrationConnectCallback(&settingsUpdatedCb);
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 SensorsStart(void)
{
// Start main task
xTaskCreate(SensorsTask, (signed char *)"Sensors", STACK_SIZE_BYTES/4, NULL, TASK_PRIORITY, &sensorsTaskHandle);
TaskMonitorAdd(TASKINFO_RUNNING_SENSORS, sensorsTaskHandle);
PIOS_WDG_RegisterFlag(PIOS_WDG_SENSORS);
return 0;
}
MODULE_INITCALL(SensorsInitialize, SensorsStart)
int32_t accel_test;
int32_t gyro_test;
int32_t mag_test;
//int32_t pressure_test;
/**
* The sensor task. This polls the gyros at 500 Hz and pumps that data to
* stabilization and to the attitude loop
*
* This function has a lot of if/defs right now to allow these configurations:
* 1. BMA180 accel and MPU6000 gyro
* 2. MPU6000 gyro and accel
* 3. BMA180 accel and L3GD20 gyro
*/
static void SensorsTask(void *parameters)
{
uint8_t init = 0;
portTickType lastSysTime;
uint32_t accel_samples;
uint32_t gyro_samples;
int32_t accel_accum[3] = {0, 0, 0};
int32_t gyro_accum[3] = {0,0,0};
float gyro_scaling;
float accel_scaling;
AlarmsClear(SYSTEMALARMS_ALARM_SENSORS);
UAVObjEvent ev;
settingsUpdatedCb(&ev);
accel_test = PIOS_BMA180_Test();
#if defined(PIOS_INCLUDE_MPU6000)
gyro_test = PIOS_MPU6000_Test();
#elif defined(PIOS_INCLUDE_L3GD20)
gyro_test = PIOS_L3GD20_Test();
#endif
mag_test = PIOS_HMC5883_Test();
if(accel_test < 0 || gyro_test < 0 || mag_test < 0) {
AlarmsSet(SYSTEMALARMS_ALARM_SENSORS, SYSTEMALARMS_ALARM_CRITICAL);
while(1) {
PIOS_WDG_UpdateFlag(PIOS_WDG_SENSORS);
vTaskDelay(10);
}
}
// If debugging connect callback
if(pios_com_aux_id != 0) {
BaroAltitudeConnectCallback(&sensorsUpdatedCb);
GPSPositionConnectCallback(&sensorsUpdatedCb);
}
// Main task loop
lastSysTime = xTaskGetTickCount();
bool error = false;
while (1) {
// TODO: add timeouts to the sensor reads and set an error if the fail
if (error) {
PIOS_WDG_UpdateFlag(PIOS_WDG_SENSORS);
lastSysTime = xTaskGetTickCount();
vTaskDelayUntil(&lastSysTime, SENSOR_PERIOD / portTICK_RATE_MS);
AlarmsSet(SYSTEMALARMS_ALARM_SENSORS, SYSTEMALARMS_ALARM_CRITICAL);
error = false;
} else {
AlarmsClear(SYSTEMALARMS_ALARM_SENSORS);
}
int32_t read_good;
int32_t count;
for (int i = 0; i < 3; i++) {
accel_accum[i] = 0;
gyro_accum[i] = 0;
}
accel_samples = 0;
gyro_samples = 0;
// Make sure we get one sample
#if !defined(PIOS_MPU6000_ACCEL)
struct pios_bma180_data accel;
count = 0;
while((read_good = PIOS_BMA180_ReadFifo(&accel)) != 0 && !error)
error = ((xTaskGetTickCount() - lastSysTime) > SENSOR_PERIOD) ? true : error;
if (error) {
// Unfortunately if the BMA180 ever misses getting read, then it will not
// trigger more interrupts. In this case we must force a read to kickstarts
// it.
struct pios_bma180_data data;
PIOS_BMA180_ReadAccels(&data);
continue;
}
while(read_good == 0) {
count++;
accel_accum[0] += accel.x;
accel_accum[1] += accel.y;
accel_accum[2] += accel.z;
read_good = PIOS_BMA180_ReadFifo(&accel);
}
accel_samples = count;
accel_scaling = PIOS_BMA180_GetScale();
#endif
// Using MPU6000 gyro and possibly accel
#if defined(PIOS_INCLUDE_MPU6000)
struct pios_mpu6000_data gyro;
count = 0;
while((read_good = PIOS_MPU6000_ReadFifo(&gyro)) != 0 && !error)
error = ((xTaskGetTickCount() - lastSysTime) > SENSOR_PERIOD) ? true : error;
if (error)
continue;
while(read_good == 0) {
count++;
gyro_accum[0] += gyro.gyro_x;
gyro_accum[1] += gyro.gyro_y;
gyro_accum[2] += gyro.gyro_z;
#if defined(PIOS_MPU6000_ACCEL)
accel_accum[0] += gyro.accel_x;
accel_accum[1] += gyro.accel_y;
accel_accum[2] += gyro.accel_z;
#endif
read_good = PIOS_MPU6000_ReadFifo(&gyro);
}
gyro_samples = count;
gyro_scaling = PIOS_MPU6000_GetScale();
#if defined(PIOS_MPU6000_ACCEL)
accel_samples = count;
accel_scaling = PIOS_MPU6000_GetAccelScale();
#endif
// Using L3DG20 gyro
#elif defined(PIOS_INCLUDE_L3GD20)
struct pios_l3gd20_data gyro;
count = 0;
while((read_good = PIOS_L3GD20_ReadFifo(&gyro)) != 0 && !error)
error = ((xTaskGetTickCount() - lastSysTime) > SENSOR_PERIOD) ? true : error;
if (error)
continue;
while(read_good == 0) {
count++;
gyro_accum[0] += gyro.gyro_x;
gyro_accum[1] += gyro.gyro_y;
gyro_accum[2] += gyro.gyro_z;
read_good = PIOS_L3GD20_ReadFifo(&gyro);
}
gyro_samples = count;
gyro_scaling = PIOS_L3GD20_GetScale();
#else
//#error No gyro defined
struct gyro_data {float x; float y; float z; float temperature;} gyro;
gyro_scaling = 0;
gyro_samples = 1;
#endif
float accels[3] = {(float) accel_accum[1] / accel_samples, (float) accel_accum[0] / accel_samples, -(float) accel_accum[2] / accel_samples};
// Not the swaping of channel orders
#if defined(PIOS_MPU6000_ACCEL)
accel_scaling = PIOS_MPU6000_GetAccelScale();
#else
accel_scaling = PIOS_BMA180_GetScale();
#endif
AccelsData accelsData; // Skip get as we set all the fields
accelsData.x = accels[0] * accel_scaling * accel_scale[0] - accel_bias[0];
accelsData.y = accels[1] * accel_scaling * accel_scale[1] - accel_bias[1];
accelsData.z = accels[2] * accel_scaling * accel_scale[2] - accel_bias[2];
accelsData.temperature = 25.0f + ((float) accel.temperature - 2.0f) / 2.0f;
AccelsSet(&accelsData);
float gyros[3] = {(float) gyro_accum[1] / gyro_samples, (float) gyro_accum[0] / gyro_samples, -(float) gyro_accum[2] / gyro_samples};
GyrosData gyrosData; // Skip get as we set all the fields
gyrosData.x = gyros[0] * gyro_scaling;
gyrosData.y = gyros[1] * gyro_scaling;
gyrosData.z = gyros[2] * gyro_scaling;
#if defined(PIOS_INCLUDE_MPU6000)
gyrosData.temperature = 35.0f + ((float) gyro.temperature + 512.0f) / 340.0f;
#else
gyrosData.temperature = gyro.temperature;
#endif
if (bias_correct_gyro) {
// Apply bias correction to the gyros
GyrosBiasData gyrosBias;
GyrosBiasGet(&gyrosBias);
gyrosData.x += gyrosBias.x;
gyrosData.y += gyrosBias.y;
gyrosData.z += gyrosBias.z;
}
GyrosSet(&gyrosData);
// Because most crafts wont get enough information from gravity to zero yaw gyro, we try
// and make it average zero (weakly)
MagnetometerData mag;
bool mag_updated = false;
if (PIOS_HMC5883_NewDataAvailable()) {
mag_updated = true;
int16_t values[3];
PIOS_HMC5883_ReadMag(values);
mag.x = values[1] * mag_scale[0] - mag_bias[0];
mag.y = values[0] * mag_scale[1] - mag_bias[1];
mag.z = -values[2] * mag_scale[2] - mag_bias[2];
MagnetometerSet(&mag);
}
// For debugging purposes here we can output all of the sensors. Do it as a single transaction
// so the message isn't split if anything else is writing to it
if(pios_com_aux_id != 0) {
uint32_t message_size = 3;
uint8_t message[200] = {0xff, (lastSysTime & 0xff00) >> 8, lastSysTime & 0x00ff};
// Add accel data
memcpy(&message[message_size], &accelsData.x, sizeof(accelsData.x) * 3);
message_size += sizeof(accelsData.x) * 3;
// Add gyro data with temp
memcpy(&message[message_size], &gyrosData, sizeof(gyrosData));
message_size += sizeof(gyrosData);
if(mag_updated) { // Add mag data
message[message_size] = 0x01; // Indicate mag data here
message_size++;
memcpy(&message[message_size], &mag, sizeof(mag));
message_size += sizeof(mag);
}
if(gps_updated) { // Add GPS data
gps_updated = false;
GPSPositionData gps;
GPSPositionGet(&gps);
message[message_size] = 0x02; // Indicate gps data here
message_size++;
memcpy(&message[message_size], &gps, sizeof(gps));
message_size += sizeof(gps);
}
if(baro_updated) { // Add baro data
baro_updated = false;
BaroAltitudeData baro;
BaroAltitudeGet(&baro);
message[message_size] = 0x03; // Indicate mag data here
message_size++;
memcpy(&message[message_size], &baro, sizeof(baro));
message_size += sizeof(baro);
}
PIOS_COM_SendBufferNonBlocking(pios_com_aux_id, message, message_size);
}
PIOS_WDG_UpdateFlag(PIOS_WDG_SENSORS);
vTaskDelayUntil(&lastSysTime, SENSOR_PERIOD / portTICK_RATE_MS);
}
}
/**
* Indicate that these sensors have been updated
*/
static void sensorsUpdatedCb(UAVObjEvent * objEv)
{
if(objEv->obj == GPSPositionHandle())
gps_updated = true;
if(objEv->obj == BaroAltitudeHandle())
baro_updated = true;
}
/**
* Locally cache some variables from the AtttitudeSettings object
*/
static void settingsUpdatedCb(UAVObjEvent * objEv) {
RevoCalibrationData cal;
RevoCalibrationGet(&cal);
mag_bias[0] = cal.mag_bias[REVOCALIBRATION_MAG_BIAS_X];
mag_bias[1] = cal.mag_bias[REVOCALIBRATION_MAG_BIAS_Y];
mag_bias[2] = cal.mag_bias[REVOCALIBRATION_MAG_BIAS_Z];
mag_scale[0] = cal.mag_scale[REVOCALIBRATION_MAG_SCALE_X];
mag_scale[1] = cal.mag_scale[REVOCALIBRATION_MAG_SCALE_Y];
mag_scale[2] = cal.mag_scale[REVOCALIBRATION_MAG_SCALE_Z];
accel_bias[0] = cal.accel_bias[REVOCALIBRATION_ACCEL_BIAS_X];
accel_bias[1] = cal.accel_bias[REVOCALIBRATION_ACCEL_BIAS_Y];
accel_bias[2] = cal.accel_bias[REVOCALIBRATION_ACCEL_BIAS_Z];
accel_scale[0] = cal.accel_scale[REVOCALIBRATION_ACCEL_SCALE_X];
accel_scale[1] = cal.accel_scale[REVOCALIBRATION_ACCEL_SCALE_Y];
accel_scale[2] = cal.accel_scale[REVOCALIBRATION_ACCEL_SCALE_Z];
}
/**
* @}
* @}
*/