static void uavoRelayTask(void *parameters)
{
UAVObjEvent ev;
// Loop forever
while (1) {
PIOS_Thread_Sleep(50);
// Wait for queue message
if (PIOS_Queue_Receive(queue, &ev, 2) == true) {
// Process event. This calls transmitData
UAVTalkSendObject(uavTalkCon, ev.obj, ev.instId, false, 0);
}
// Process incoming data in sufficient chunks that we keep up
uint8_t serial_data[8];
uint16_t bytes_to_process;
bytes_to_process = PIOS_COM_ReceiveBuffer(uavorelay_com_id, serial_data, sizeof(serial_data), 0);
do {
bytes_to_process = PIOS_COM_ReceiveBuffer(uavorelay_com_id, serial_data, sizeof(serial_data), 0);
for (uint8_t i = 0; i < bytes_to_process; i++)
UAVTalkProcessInputStream(uavTalkCon,serial_data[i]);
} while (bytes_to_process > 0);
}
}
/**
* @brief Gimbal output control task
*/
static void brushlessGimbalTask(void* parameters)
{
UAVObjEvent ev;
TIM2->CNT = 0;
TIM3->CNT = 0;
TIM15->CNT = 0;
TIM17->CNT = 0;
bool armed = false;
bool previous_armed = false;
while (1) {
PIOS_WDG_UpdateFlag(PIOS_WDG_ACTUATOR);
// Wait until the ActuatorDesired object is updated
PIOS_Queue_Receive(queue, &ev, 1);
previous_armed = armed;
armed |= PIOS_Thread_Systime() > 10000;
if (armed && !previous_armed) {
PIOS_Brushless_SetUpdateRate(60000);
}
if (!armed)
continue;
ActuatorDesiredData actuatorDesired;
ActuatorDesiredGet(&actuatorDesired);
// Set the rotation in electrical degrees per second. Note these
// will be divided by the number of physical poles to get real
// mechanical degrees per second
BrushlessGimbalSettingsData settings;
BrushlessGimbalSettingsGet(&settings);
PIOS_Brushless_SetScale(settings.PowerScale[0], settings.PowerScale[1], settings.PowerScale[2]);
PIOS_Brushless_SetMaxAcceleration(settings.SlewLimit[0], settings.SlewLimit[1], settings.SlewLimit[2]);
PIOS_Brushless_SetSpeed(0, actuatorDesired.Roll * settings.MaxDPS[BRUSHLESSGIMBALSETTINGS_MAXDPS_ROLL], 0.001f);
PIOS_Brushless_SetSpeed(1, actuatorDesired.Pitch * settings.MaxDPS[BRUSHLESSGIMBALSETTINGS_MAXDPS_PITCH], 0.001f);
// Use the gyros to set a damping term. This creates a phase offset of the integrated
// driving position to make the control pull against any momentum. Essentially the main
// output to the driver (above) is a velocity signal which the driver takes care of
// integrating to create a position. The current rate of roll creates a shift in that
// position (without changing the integrated position).
// This idea was taken from https://code.google.com/p/brushless-gimbal/
GyrosData gyros;
GyrosGet(&gyros);
PIOS_Brushless_SetPhaseLag(0, -gyros.x * settings.Damping[BRUSHLESSGIMBALSETTINGS_DAMPING_ROLL]);
PIOS_Brushless_SetPhaseLag(1, -gyros.y * settings.Damping[BRUSHLESSGIMBALSETTINGS_DAMPING_PITCH]);
}
}
/**
* Telemetry transmit task, regular priority
*
* Logic: We need to double buffer the DMA transfers. Pack the buffer until either
* 1) it is full (and then we should record the number of missed events then)
* 2) the current transaction is done (we should immediately schedule since we are slave)
* when done packing the buffer we should call PIOS_SPI_TransferBlock, change the active buffer
* and then take the semaphrore
*/
static void overoSyncTask(void *parameters)
{
UAVObjEvent ev;
// Kick off SPI transfers (once one is completed another will automatically transmit)
overosync->transaction_done = true;
overosync->sent_objects = 0;
overosync->failed_objects = 0;
overosync->received_objects = 0;
uint32_t lastUpdateTime = PIOS_Thread_Systime();
uint32_t updateTime;
fid = fopen("sim_log.opl", "w");
// Loop forever
while (1) {
// Wait for queue message
if (PIOS_Queue_Receive(queue, &ev, PIOS_QUEUE_TIMEOUT_MAX) == true) {
// Check it will fit before packetizing
if ((overosync->write_pointer + UAVObjGetNumBytes(ev.obj) + 12) >=
sizeof(overosync->transactions[overosync->loading_transaction_id].tx_buffer)) {
overosync->failed_objects ++;
} else {
// Process event. This calls transmitData
UAVTalkSendObject(uavTalkCon, ev.obj, ev.instId, false, 0);
}
updateTime = PIOS_Thread_Systime();
if(((uint32_t) (updateTime - lastUpdateTime)) > 1000) {
// Update stats. This will trigger a local send event too
OveroSyncStatsData syncStats;
syncStats.Send = overosync->sent_bytes;
syncStats.Received = 0;
syncStats.Connected = syncStats.Send > 500 ? OVEROSYNCSTATS_CONNECTED_TRUE : OVEROSYNCSTATS_CONNECTED_FALSE;
syncStats.DroppedUpdates = overosync->failed_objects;
OveroSyncStatsSet(&syncStats);
overosync->failed_objects = 0;
overosync->sent_bytes = 0;
lastUpdateTime = updateTime;
}
}
}
}
static void gimbalControlTask(void *parameters)
{
// Loop forever
while (1) {
struct pios_can_gimbal_message bgc_message;
// Wait for queue message
if (PIOS_Queue_Receive(queue, &bgc_message, 5) == true) {
CameraDesiredData cameraDesired;
CameraDesiredGet(&cameraDesired);
cameraDesired.Declination = bgc_message.setpoint_pitch;
cameraDesired.Bearing = bgc_message.setpoint_yaw;
cameraDesired.Roll = bgc_message.fc_roll;
cameraDesired.Pitch = bgc_message.fc_pitch;
cameraDesired.Yaw = bgc_message.fc_yaw;
CameraDesiredSet(&cameraDesired);
}
}
}
static void loggingTask(void *parameters)
{
UAVObjEvent ev;
bool armed = false;
uint32_t now = PIOS_Thread_Systime();
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
bool write_open = false;
bool read_open = false;
int32_t read_sector = 0;
uint8_t read_data[LOGGINGSTATS_FILESECTOR_NUMELEM];
#endif
// Get settings automatically for now on
LoggingSettingsConnectCopy(&settings);
LoggingStatsGet(&loggingData);
loggingData.BytesLogged = 0;
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
if (destination_spi_flash)
{
loggingData.MinFileId = PIOS_STREAMFS_MinFileId(streamfs_id);
loggingData.MaxFileId = PIOS_STREAMFS_MaxFileId(streamfs_id);
}
#endif
if (settings.LogBehavior == LOGGINGSETTINGS_LOGBEHAVIOR_LOGONSTART) {
loggingData.Operation = LOGGINGSTATS_OPERATION_INITIALIZING;
} else {
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
}
LoggingStatsSet(&loggingData);
// Loop forever
while (1)
{
LoggingStatsGet(&loggingData);
// Check for change in armed state if logging on armed
if (settings.LogBehavior == LOGGINGSETTINGS_LOGBEHAVIOR_LOGONARM) {
FlightStatusData flightStatus;
FlightStatusGet(&flightStatus);
if (flightStatus.Armed == FLIGHTSTATUS_ARMED_ARMED && !armed) {
// Start logging because just armed
loggingData.Operation = LOGGINGSTATS_OPERATION_INITIALIZING;
armed = true;
LoggingStatsSet(&loggingData);
} else if (flightStatus.Armed == FLIGHTSTATUS_ARMED_DISARMED && armed) {
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
armed = false;
LoggingStatsSet(&loggingData);
}
}
switch (loggingData.Operation) {
case LOGGINGSTATS_OPERATION_FORMAT:
// Format the file system
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
if (destination_spi_flash){
if (read_open || write_open) {
PIOS_STREAMFS_Close(streamfs_id);
read_open = false;
write_open = false;
}
PIOS_STREAMFS_Format(streamfs_id);
loggingData.MinFileId = PIOS_STREAMFS_MinFileId(streamfs_id);
loggingData.MaxFileId = PIOS_STREAMFS_MaxFileId(streamfs_id);
}
#endif /* defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC) */
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
LoggingStatsSet(&loggingData);
break;
case LOGGINGSTATS_OPERATION_INITIALIZING:
// Unregister all objects
UAVObjIterate(&unregister_object);
// Register objects to be logged
switch (settings.Profile) {
case LOGGINGSETTINGS_PROFILE_DEFAULT:
register_default_profile();
break;
case LOGGINGSETTINGS_PROFILE_CUSTOM:
UAVObjIterate(®ister_object);
break;
}
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
if (destination_spi_flash){
// Close the file if it is open for reading
if (read_open) {
PIOS_STREAMFS_Close(streamfs_id);
read_open = false;
}
// Open the file if it is not open for writing
if (!write_open) {
if (PIOS_STREAMFS_OpenWrite(streamfs_id) != 0) {
loggingData.Operation = LOGGINGSTATS_OPERATION_ERROR;
continue;
} else {
write_open = true;
}
loggingData.MinFileId = PIOS_STREAMFS_MinFileId(streamfs_id);
loggingData.MaxFileId = PIOS_STREAMFS_MaxFileId(streamfs_id);
LoggingStatsSet(&loggingData);
}
}
else {
read_open = false;
write_open = true;
}
#endif /* defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC) */
// Write information at start of the log file
writeHeader();
// Log settings
if (settings.LogSettingsOnStart == LOGGINGSETTINGS_LOGSETTINGSONSTART_TRUE){
UAVObjIterate(&logSettings);
}
// Empty the queue
while(PIOS_Queue_Receive(logging_queue, &ev, 0))
LoggingStatsBytesLoggedSet(&written_bytes);
loggingData.Operation = LOGGINGSTATS_OPERATION_LOGGING;
LoggingStatsSet(&loggingData);
break;
case LOGGINGSTATS_OPERATION_LOGGING:
{
// Sleep between writing
PIOS_Thread_Sleep_Until(&now, LOGGING_PERIOD_MS);
// Log the objects registred to the shared queue
for (int i=0; i<LOGGING_QUEUE_SIZE; i++) {
if (PIOS_Queue_Receive(logging_queue, &ev, 0) == true) {
UAVTalkSendObjectTimestamped(uavTalkCon, ev.obj, ev.instId, false, 0);
}
else {
break;
}
}
LoggingStatsBytesLoggedSet(&written_bytes);
now = PIOS_Thread_Systime();
}
break;
case LOGGINGSTATS_OPERATION_DOWNLOAD:
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
if (destination_spi_flash) {
if (!read_open) {
// Start reading
if (PIOS_STREAMFS_OpenRead(streamfs_id, loggingData.FileRequest) != 0) {
loggingData.Operation = LOGGINGSTATS_OPERATION_ERROR;
} else {
read_open = true;
read_sector = -1;
}
}
if (read_open && read_sector == loggingData.FileSectorNum) {
// Request received for same sector. Reupdate.
memcpy(loggingData.FileSector, read_data, LOGGINGSTATS_FILESECTOR_NUMELEM);
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
} else if (read_open && (read_sector + 1) == loggingData.FileSectorNum) {
int32_t bytes_read = PIOS_COM_ReceiveBuffer(logging_com_id, read_data, LOGGINGSTATS_FILESECTOR_NUMELEM, 1);
if (bytes_read < 0 || bytes_read > LOGGINGSTATS_FILESECTOR_NUMELEM) {
// close on error
loggingData.Operation = LOGGINGSTATS_OPERATION_ERROR;
PIOS_STREAMFS_Close(streamfs_id);
read_open = false;
} else if (bytes_read < LOGGINGSTATS_FILESECTOR_NUMELEM) {
// Check it has really run out of bytes by reading again
int32_t bytes_read2 = PIOS_COM_ReceiveBuffer(logging_com_id, &read_data[bytes_read], LOGGINGSTATS_FILESECTOR_NUMELEM - bytes_read, 1);
memcpy(loggingData.FileSector, read_data, LOGGINGSTATS_FILESECTOR_NUMELEM);
if ((bytes_read + bytes_read2) < LOGGINGSTATS_FILESECTOR_NUMELEM) {
// indicate end of file
loggingData.Operation = LOGGINGSTATS_OPERATION_COMPLETE;
PIOS_STREAMFS_Close(streamfs_id);
read_open = false;
} else {
// Indicate sent
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
}
} else {
// Indicate sent
loggingData.Operation = LOGGINGSTATS_OPERATION_IDLE;
memcpy(loggingData.FileSector, read_data, LOGGINGSTATS_FILESECTOR_NUMELEM);
}
read_sector = loggingData.FileSectorNum;
}
LoggingStatsSet(&loggingData);
}
#endif /* defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC) */
// fall-through to default case
default:
// Makes sure that we are not hogging the processor
PIOS_Thread_Sleep(10);
#if defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC)
if (destination_spi_flash) {
// Close the file if necessary
if (write_open) {
PIOS_STREAMFS_Close(streamfs_id);
loggingData.MinFileId = PIOS_STREAMFS_MinFileId(streamfs_id);
loggingData.MaxFileId = PIOS_STREAMFS_MaxFileId(streamfs_id);
LoggingStatsSet(&loggingData);
write_open = false;
}
}
#endif /* defined(PIOS_INCLUDE_FLASH) && defined(PIOS_INCLUDE_FLASH_JEDEC) */
}
}
}
/**
* System task, periodically executes every SYSTEM_UPDATE_PERIOD_MS
*/
static void systemTask(void *parameters)
{
/* create all modules thread */
MODULE_TASKCREATE_ALL;
if (PIOS_heap_malloc_failed_p()) {
/* We failed to malloc during task creation,
* system behaviour is undefined. Reset and let
* the BootFault code recover for us.
*/
PIOS_SYS_Reset();
}
#if defined(PIOS_INCLUDE_IAP)
/* Record a successful boot */
PIOS_IAP_WriteBootCount(0);
#endif
// Initialize vars
idleCounter = 0;
idleCounterClear = 0;
// Listen for SettingPersistance object updates, connect a callback function
ObjectPersistenceConnectQueue(objectPersistenceQueue);
#if (defined(COPTERCONTROL) || defined(REVOLUTION) || defined(SIM_OSX)) && ! (defined(SIM_POSIX))
// Run this initially to make sure the configuration is checked
configuration_check();
// Whenever the configuration changes, make sure it is safe to fly
if (StabilizationSettingsHandle())
StabilizationSettingsConnectCallback(configurationUpdatedCb);
if (SystemSettingsHandle())
SystemSettingsConnectCallback(configurationUpdatedCb);
if (ManualControlSettingsHandle())
ManualControlSettingsConnectCallback(configurationUpdatedCb);
if (FlightStatusHandle())
FlightStatusConnectCallback(configurationUpdatedCb);
#endif
#if (defined(REVOLUTION) || defined(SIM_OSX)) && ! (defined(SIM_POSIX))
if (StateEstimationHandle())
StateEstimationConnectCallback(configurationUpdatedCb);
#endif
// Main system loop
while (1) {
// Update the system statistics
updateStats();
// Update the system alarms
updateSystemAlarms();
#if defined(WDG_STATS_DIAGNOSTICS)
updateWDGstats();
#endif
#if defined(DIAG_TASKS)
// Update the task status object
TaskMonitorUpdateAll();
#endif
// Flash the heartbeat LED
#if defined(PIOS_LED_HEARTBEAT)
PIOS_LED_Toggle(PIOS_LED_HEARTBEAT);
DEBUG_MSG("+ 0x%08x\r\n", 0xDEADBEEF);
#endif /* PIOS_LED_HEARTBEAT */
// Turn on the error LED if an alarm is set
if (indicateError()) {
#if defined (PIOS_LED_ALARM)
PIOS_LED_On(PIOS_LED_ALARM);
#endif /* PIOS_LED_ALARM */
} else {
#if defined (PIOS_LED_ALARM)
PIOS_LED_Off(PIOS_LED_ALARM);
#endif /* PIOS_LED_ALARM */
}
FlightStatusData flightStatus;
FlightStatusGet(&flightStatus);
UAVObjEvent ev;
int delayTime = flightStatus.Armed == FLIGHTSTATUS_ARMED_ARMED ?
SYSTEM_UPDATE_PERIOD_MS / (LED_BLINK_RATE_HZ * 2) :
SYSTEM_UPDATE_PERIOD_MS;
if (PIOS_Queue_Receive(objectPersistenceQueue, &ev, delayTime) == true) {
// If object persistence is updated call the callback
objectUpdatedCb(&ev);
}
}
}
/**
* Module thread, should not return.
*/
static void altitudeHoldTask(void *parameters)
{
bool engaged = false;
AltitudeHoldDesiredData altitudeHoldDesired;
StabilizationDesiredData stabilizationDesired;
AltitudeHoldSettingsData altitudeHoldSettings;
UAVObjEvent ev;
struct pid velocity_pid;
// Listen for object updates.
AltitudeHoldDesiredConnectQueue(queue);
AltitudeHoldSettingsConnectQueue(queue);
FlightStatusConnectQueue(queue);
AltitudeHoldSettingsGet(&altitudeHoldSettings);
pid_configure(&velocity_pid, altitudeHoldSettings.VelocityKp,
altitudeHoldSettings.VelocityKi, 0.0f, 1.0f);
AlarmsSet(SYSTEMALARMS_ALARM_ALTITUDEHOLD, SYSTEMALARMS_ALARM_OK);
// Main task loop
const uint32_t dt_ms = 5;
const float dt_s = dt_ms * 0.001f;
uint32_t timeout = dt_ms;
while (1) {
if (PIOS_Queue_Receive(queue, &ev, timeout) != true) {
} else if (ev.obj == FlightStatusHandle()) {
uint8_t flight_mode;
FlightStatusFlightModeGet(&flight_mode);
if (flight_mode == FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD && !engaged) {
// Copy the current throttle as a starting point for integral
StabilizationDesiredThrottleGet(&velocity_pid.iAccumulator);
velocity_pid.iAccumulator *= 1000.0f; // pid library scales up accumulator by 1000
engaged = true;
} else if (flight_mode != FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD)
engaged = false;
// Run loop at 20 Hz when engaged otherwise just slowly wait for it to be engaged
timeout = engaged ? dt_ms : 100;
} else if (ev.obj == AltitudeHoldDesiredHandle()) {
AltitudeHoldDesiredGet(&altitudeHoldDesired);
} else if (ev.obj == AltitudeHoldSettingsHandle()) {
AltitudeHoldSettingsGet(&altitudeHoldSettings);
pid_configure(&velocity_pid, altitudeHoldSettings.VelocityKp,
altitudeHoldSettings.VelocityKi, 0.0f, 1.0f);
}
bool landing = altitudeHoldDesired.Land == ALTITUDEHOLDDESIRED_LAND_TRUE;
// For landing mode allow throttle to go negative to allow the integrals
// to stop winding up
const float min_throttle = landing ? -0.1f : 0.0f;
// When engaged compute altitude controller output
if (engaged) {
float position_z, velocity_z, altitude_error;
PositionActualDownGet(&position_z);
VelocityActualDownGet(&velocity_z);
position_z = -position_z; // Use positive up convention
velocity_z = -velocity_z; // Use positive up convention
// Compute the altitude error
altitude_error = altitudeHoldDesired.Altitude - position_z;
// Velocity desired is from the outer controller plus the set point
float velocity_desired = altitude_error * altitudeHoldSettings.PositionKp + altitudeHoldDesired.ClimbRate;
float throttle_desired = pid_apply_antiwindup(&velocity_pid,
velocity_desired - velocity_z,
min_throttle, 1.0f, // positive limits since this is throttle
dt_s);
if (altitudeHoldSettings.AttitudeComp > 0) {
// Throttle desired is at this point the mount desired in the up direction, we can
// account for the attitude if desired
AttitudeActualData attitudeActual;
AttitudeActualGet(&attitudeActual);
// Project a unit vector pointing up into the body frame and
// get the z component
float fraction = attitudeActual.q1 * attitudeActual.q1 -
attitudeActual.q2 * attitudeActual.q2 -
attitudeActual.q3 * attitudeActual.q3 +
attitudeActual.q4 * attitudeActual.q4;
// Add ability to scale up the amount of compensation to achieve
// level forward flight
fraction = powf(fraction, (float) altitudeHoldSettings.AttitudeComp / 100.0f);
// Dividing by the fraction remaining in the vertical projection will
// attempt to compensate for tilt. This acts like the thrust is linear
// with the output which isn't really true. If the fraction is starting
// to go negative we are inverted and should shut off throttle
throttle_desired = (fraction > 0.1f) ? (throttle_desired / fraction) : 0.0f;
}
StabilizationDesiredGet(&stabilizationDesired);
stabilizationDesired.Throttle = bound_min_max(throttle_desired, min_throttle, 1.0f);
if (landing) {
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_ROLL] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_PITCH] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_YAW] = STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK;
stabilizationDesired.Roll = 0;
stabilizationDesired.Pitch = 0;
stabilizationDesired.Yaw = 0;
} else {
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_ROLL] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_PITCH] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_YAW] = STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK;
stabilizationDesired.Roll = altitudeHoldDesired.Roll;
stabilizationDesired.Pitch = altitudeHoldDesired.Pitch;
stabilizationDesired.Yaw = altitudeHoldDesired.Yaw;
}
StabilizationDesiredSet(&stabilizationDesired);
}
}
}
/**
* Module task
*/
static void stabilizationTask(void* parameters)
{
UAVObjEvent ev;
uint32_t timeval = PIOS_DELAY_GetRaw();
ActuatorDesiredData actuatorDesired;
StabilizationDesiredData stabDesired;
RateDesiredData rateDesired;
AttitudeActualData attitudeActual;
GyrosData gyrosData;
FlightStatusData flightStatus;
float *stabDesiredAxis = &stabDesired.Roll;
float *actuatorDesiredAxis = &actuatorDesired.Roll;
float *rateDesiredAxis = &rateDesired.Roll;
float horizonRateFraction = 0.0f;
// Force refresh of all settings immediately before entering main task loop
SettingsUpdatedCb((UAVObjEvent *) NULL);
// Settings for system identification
uint32_t iteration = 0;
const uint32_t SYSTEM_IDENT_PERIOD = 75;
uint32_t system_ident_timeval = PIOS_DELAY_GetRaw();
float dT_filtered = 0;
// Main task loop
zero_pids();
while(1) {
iteration++;
PIOS_WDG_UpdateFlag(PIOS_WDG_STABILIZATION);
// Wait until the AttitudeRaw object is updated, if a timeout then go to failsafe
if (PIOS_Queue_Receive(queue, &ev, FAILSAFE_TIMEOUT_MS) != true)
{
AlarmsSet(SYSTEMALARMS_ALARM_STABILIZATION,SYSTEMALARMS_ALARM_WARNING);
continue;
}
calculate_pids();
float dT = PIOS_DELAY_DiffuS(timeval) * 1.0e-6f;
timeval = PIOS_DELAY_GetRaw();
// exponential moving averaging (EMA) of dT to reduce jitter; ~200points
// to have more or less equivalent noise reduction to a normal N point moving averaging: alpha = 2 / (N + 1)
// run it only at the beginning for the first samples, to reduce CPU load, and the value should converge to a constant value
if (iteration < 100) {
dT_filtered = dT;
} else if (iteration < 2000) {
dT_filtered = 0.01f * dT + (1.0f - 0.01f) * dT_filtered;
} else if (iteration == 2000) {
gyro_filter_updated = true;
}
if (gyro_filter_updated) {
if (settings.GyroCutoff < 1.0f) {
gyro_alpha = 0;
} else {
gyro_alpha = expf(-2.0f * (float)(M_PI) *
settings.GyroCutoff * dT_filtered);
}
// Compute time constant for vbar decay term
if (settings.VbarTau < 0.001f) {
vbar_decay = 0;
} else {
vbar_decay = expf(-dT_filtered / settings.VbarTau);
}
gyro_filter_updated = false;
}
FlightStatusGet(&flightStatus);
StabilizationDesiredGet(&stabDesired);
AttitudeActualGet(&attitudeActual);
GyrosGet(&gyrosData);
ActuatorDesiredGet(&actuatorDesired);
#if defined(RATEDESIRED_DIAGNOSTICS)
RateDesiredGet(&rateDesired);
#endif
struct TrimmedAttitudeSetpoint {
float Roll;
float Pitch;
float Yaw;
} trimmedAttitudeSetpoint;
// Mux in level trim values, and saturate the trimmed attitude setpoint.
trimmedAttitudeSetpoint.Roll = bound_min_max(
stabDesired.Roll + trimAngles.Roll,
-settings.RollMax + trimAngles.Roll,
settings.RollMax + trimAngles.Roll);
trimmedAttitudeSetpoint.Pitch = bound_min_max(
stabDesired.Pitch + trimAngles.Pitch,
-settings.PitchMax + trimAngles.Pitch,
settings.PitchMax + trimAngles.Pitch);
trimmedAttitudeSetpoint.Yaw = stabDesired.Yaw;
// For horizon mode we need to compute the desire attitude from an unscaled value and apply the
// trim offset. Also track the stick with the most deflection to choose rate blending.
horizonRateFraction = 0.0f;
if (stabDesired.StabilizationMode[ROLL] == STABILIZATIONDESIRED_STABILIZATIONMODE_HORIZON) {
trimmedAttitudeSetpoint.Roll = bound_min_max(
stabDesired.Roll * settings.RollMax + trimAngles.Roll,
-settings.RollMax + trimAngles.Roll,
settings.RollMax + trimAngles.Roll);
horizonRateFraction = fabsf(stabDesired.Roll);
}
if (stabDesired.StabilizationMode[PITCH] == STABILIZATIONDESIRED_STABILIZATIONMODE_HORIZON) {
trimmedAttitudeSetpoint.Pitch = bound_min_max(
stabDesired.Pitch * settings.PitchMax + trimAngles.Pitch,
-settings.PitchMax + trimAngles.Pitch,
settings.PitchMax + trimAngles.Pitch);
horizonRateFraction = MAX(horizonRateFraction, fabsf(stabDesired.Pitch));
}
if (stabDesired.StabilizationMode[YAW] == STABILIZATIONDESIRED_STABILIZATIONMODE_HORIZON) {
trimmedAttitudeSetpoint.Yaw = stabDesired.Yaw * settings.YawMax;
horizonRateFraction = MAX(horizonRateFraction, fabsf(stabDesired.Yaw));
}
// For weak leveling mode the attitude setpoint is the trim value (drifts back towards "0")
if (stabDesired.StabilizationMode[ROLL] == STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) {
trimmedAttitudeSetpoint.Roll = trimAngles.Roll;
}
if (stabDesired.StabilizationMode[PITCH] == STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) {
trimmedAttitudeSetpoint.Pitch = trimAngles.Pitch;
}
if (stabDesired.StabilizationMode[YAW] == STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) {
trimmedAttitudeSetpoint.Yaw = 0;
}
// Note we divide by the maximum limit here so the fraction ranges from 0 to 1 depending on
// how much is requested.
horizonRateFraction = bound_sym(horizonRateFraction, HORIZON_MODE_MAX_BLEND) / HORIZON_MODE_MAX_BLEND;
// Calculate the errors in each axis. The local error is used in the following modes:
// ATTITUDE, HORIZON, WEAKLEVELING
float local_attitude_error[3];
local_attitude_error[0] = trimmedAttitudeSetpoint.Roll - attitudeActual.Roll;
local_attitude_error[1] = trimmedAttitudeSetpoint.Pitch - attitudeActual.Pitch;
local_attitude_error[2] = trimmedAttitudeSetpoint.Yaw - attitudeActual.Yaw;
// Wrap yaw error to [-180,180]
local_attitude_error[2] = circular_modulus_deg(local_attitude_error[2]);
static float gyro_filtered[3];
gyro_filtered[0] = gyro_filtered[0] * gyro_alpha + gyrosData.x * (1 - gyro_alpha);
gyro_filtered[1] = gyro_filtered[1] * gyro_alpha + gyrosData.y * (1 - gyro_alpha);
gyro_filtered[2] = gyro_filtered[2] * gyro_alpha + gyrosData.z * (1 - gyro_alpha);
// A flag to track which stabilization mode each axis is in
static uint8_t previous_mode[MAX_AXES] = {255,255,255};
bool error = false;
//Run the selected stabilization algorithm on each axis:
for(uint8_t i=0; i< MAX_AXES; i++)
{
// Check whether this axis mode needs to be reinitialized
bool reinit = (stabDesired.StabilizationMode[i] != previous_mode[i]);
// The unscaled input (-1,1)
float *raw_input = &stabDesired.Roll;
previous_mode[i] = stabDesired.StabilizationMode[i];
// Apply the selected control law
switch(stabDesired.StabilizationMode[i])
{
case STABILIZATIONDESIRED_STABILIZATIONMODE_RATE:
if(reinit)
pids[PID_GROUP_RATE + i].iAccumulator = 0;
// Store to rate desired variable for storing to UAVO
rateDesiredAxis[i] = bound_sym(stabDesiredAxis[i], settings.ManualRate[i]);
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_ACROPLUS:
// this implementation is based on the Openpilot/Librepilot Acro+ flightmode
// and our existing rate & MWRate flightmodes
if(reinit)
pids[PID_GROUP_RATE + i].iAccumulator = 0;
// The factor for gyro suppression / mixing raw stick input into the output; scaled by raw stick input
float factor = fabsf(raw_input[i]) * settings.AcroInsanityFactor / 100;
// Store to rate desired variable for storing to UAVO
rateDesiredAxis[i] = bound_sym(raw_input[i] * settings.ManualRate[i], settings.ManualRate[i]);
// Zero integral for aggressive maneuvers, like it is done for MWRate
if ((i < 2 && fabsf(gyro_filtered[i]) > 150.0f) ||
(i == 0 && fabsf(raw_input[i]) > 0.2f)) {
pids[PID_GROUP_RATE + i].iAccumulator = 0;
pids[PID_GROUP_RATE + i].i = 0;
}
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = factor * raw_input[i] + (1.0f - factor) * actuatorDesiredAxis[i];
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i], 1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE:
if(reinit) {
pids[PID_GROUP_ATT + i].iAccumulator = 0;
pids[PID_GROUP_RATE + i].iAccumulator = 0;
}
// Compute the outer loop
rateDesiredAxis[i] = pid_apply(&pids[PID_GROUP_ATT + i], local_attitude_error[i], dT);
rateDesiredAxis[i] = bound_sym(rateDesiredAxis[i], settings.MaximumRate[i]);
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_VIRTUALBAR:
// Store for debugging output
rateDesiredAxis[i] = stabDesiredAxis[i];
// Run a virtual flybar stabilization algorithm on this axis
stabilization_virtual_flybar(gyro_filtered[i], rateDesiredAxis[i], &actuatorDesiredAxis[i], dT, reinit, i, &pids[PID_GROUP_VBAR + i], &settings);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING:
{
if (reinit)
pids[PID_GROUP_RATE + i].iAccumulator = 0;
float weak_leveling = local_attitude_error[i] * weak_leveling_kp;
weak_leveling = bound_sym(weak_leveling, weak_leveling_max);
// Compute desired rate as input biased towards leveling
rateDesiredAxis[i] = stabDesiredAxis[i] + weak_leveling;
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
}
case STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK:
if (reinit)
pids[PID_GROUP_RATE + i].iAccumulator = 0;
if (fabsf(stabDesiredAxis[i]) > max_axislock_rate) {
// While getting strong commands act like rate mode
rateDesiredAxis[i] = bound_sym(stabDesiredAxis[i], settings.ManualRate[i]);
// Reset accumulator
axis_lock_accum[i] = 0;
} else {
// For weaker commands or no command simply lock (almost) on no gyro change
axis_lock_accum[i] += (stabDesiredAxis[i] - gyro_filtered[i]) * dT;
axis_lock_accum[i] = bound_sym(axis_lock_accum[i], max_axis_lock);
// Compute the inner loop
float tmpRateDesired = pid_apply(&pids[PID_GROUP_ATT + i], axis_lock_accum[i], dT);
rateDesiredAxis[i] = bound_sym(tmpRateDesired, settings.MaximumRate[i]);
}
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_HORIZON:
if(reinit) {
pids[PID_GROUP_RATE + i].iAccumulator = 0;
}
// Do not allow outer loop integral to wind up in this mode since the controller
// is often disengaged.
pids[PID_GROUP_ATT + i].iAccumulator = 0;
// Compute the outer loop for the attitude control
float rateDesiredAttitude = pid_apply(&pids[PID_GROUP_ATT + i], local_attitude_error[i], dT);
// Compute the desire rate for a rate control
float rateDesiredRate = raw_input[i] * settings.ManualRate[i];
// Blend from one rate to another. The maximum of all stick positions is used for the
// amount so that when one axis goes completely to rate the other one does too. This
// prevents doing flips while one axis tries to stay in attitude mode.
rateDesiredAxis[i] = rateDesiredAttitude * (1.0f-horizonRateFraction) + rateDesiredRate * horizonRateFraction;
rateDesiredAxis[i] = bound_sym(rateDesiredAxis[i], settings.ManualRate[i]);
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_MWRATE:
{
if(reinit) {
pids[PID_GROUP_MWR + i].iAccumulator = 0;
}
/*
Conversion from MultiWii PID settings to our units.
Kp = Kp_mw * 4 / 80 / 500
Kd = Kd_mw * looptime * 1e-6 * 4 * 3 / 32 / 500
Ki = Ki_mw * 4 / 125 / 64 / (looptime * 1e-6) / 500
These values will just be approximate and should help
you get started.
*/
// The unscaled input (-1,1) - note in MW this is from (-500,500)
float *raw_input = &stabDesired.Roll;
// dynamic PIDs are scaled both by throttle and stick position
float scale = (i == 0 || i == 1) ? mwrate_settings.RollPitchRate : mwrate_settings.YawRate;
float pid_scale = (100.0f - scale * fabsf(raw_input[i])) / 100.0f;
float dynP8 = pids[PID_GROUP_MWR + i].p * pid_scale;
float dynD8 = pids[PID_GROUP_MWR + i].d * pid_scale;
// these terms are used by the integral loop this proportional term is scaled by throttle (this is different than MW
// that does not apply scale
float cfgP8 = pids[PID_GROUP_MWR + i].p;
float cfgI8 = pids[PID_GROUP_MWR + i].i;
// Dynamically adjust PID settings
struct pid mw_pid;
mw_pid.p = 0; // use zero Kp here because of strange setpoint. applied later.
mw_pid.d = dynD8;
mw_pid.i = cfgI8;
mw_pid.iLim = pids[PID_GROUP_MWR + i].iLim;
mw_pid.iAccumulator = pids[PID_GROUP_MWR + i].iAccumulator;
mw_pid.lastErr = pids[PID_GROUP_MWR + i].lastErr;
mw_pid.lastDer = pids[PID_GROUP_MWR + i].lastDer;
// Zero integral for aggressive maneuvers
if ((i < 2 && fabsf(gyro_filtered[i]) > 150.0f) ||
(i == 0 && fabsf(raw_input[i]) > 0.2f)) {
mw_pid.iAccumulator = 0;
mw_pid.i = 0;
}
// Apply controller as if we want zero change, then add stick input afterwards
actuatorDesiredAxis[i] = pid_apply_setpoint(&mw_pid, raw_input[i] / cfgP8, gyro_filtered[i], dT);
actuatorDesiredAxis[i] += raw_input[i]; // apply input
actuatorDesiredAxis[i] -= dynP8 * gyro_filtered[i]; // apply Kp term
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
// Store PID accumulators for next cycle
pids[PID_GROUP_MWR + i].iAccumulator = mw_pid.iAccumulator;
pids[PID_GROUP_MWR + i].lastErr = mw_pid.lastErr;
pids[PID_GROUP_MWR + i].lastDer = mw_pid.lastDer;
}
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_SYSTEMIDENT:
if(reinit) {
pids[PID_GROUP_ATT + i].iAccumulator = 0;
pids[PID_GROUP_RATE + i].iAccumulator = 0;
}
static uint32_t ident_iteration = 0;
static float ident_offsets[3] = {0};
if (PIOS_DELAY_DiffuS(system_ident_timeval) / 1000.0f > SYSTEM_IDENT_PERIOD && SystemIdentHandle()) {
ident_iteration++;
system_ident_timeval = PIOS_DELAY_GetRaw();
SystemIdentData systemIdent;
SystemIdentGet(&systemIdent);
const float SCALE_BIAS = 7.1f;
float roll_scale = expf(SCALE_BIAS - systemIdent.Beta[SYSTEMIDENT_BETA_ROLL]);
float pitch_scale = expf(SCALE_BIAS - systemIdent.Beta[SYSTEMIDENT_BETA_PITCH]);
float yaw_scale = expf(SCALE_BIAS - systemIdent.Beta[SYSTEMIDENT_BETA_YAW]);
if (roll_scale > 0.25f)
roll_scale = 0.25f;
if (pitch_scale > 0.25f)
pitch_scale = 0.25f;
if (yaw_scale > 0.25f)
yaw_scale = 0.2f;
switch(ident_iteration & 0x07) {
case 0:
ident_offsets[0] = 0;
ident_offsets[1] = 0;
ident_offsets[2] = yaw_scale;
break;
case 1:
ident_offsets[0] = roll_scale;
ident_offsets[1] = 0;
ident_offsets[2] = 0;
break;
case 2:
ident_offsets[0] = 0;
ident_offsets[1] = 0;
ident_offsets[2] = -yaw_scale;
break;
case 3:
ident_offsets[0] = -roll_scale;
ident_offsets[1] = 0;
ident_offsets[2] = 0;
break;
case 4:
ident_offsets[0] = 0;
ident_offsets[1] = 0;
ident_offsets[2] = yaw_scale;
break;
case 5:
ident_offsets[0] = 0;
ident_offsets[1] = pitch_scale;
ident_offsets[2] = 0;
break;
case 6:
ident_offsets[0] = 0;
ident_offsets[1] = 0;
ident_offsets[2] = -yaw_scale;
break;
case 7:
ident_offsets[0] = 0;
ident_offsets[1] = -pitch_scale;
ident_offsets[2] = 0;
break;
}
}
if (i == ROLL || i == PITCH) {
// Compute the outer loop
rateDesiredAxis[i] = pid_apply(&pids[PID_GROUP_ATT + i], local_attitude_error[i], dT);
rateDesiredAxis[i] = bound_sym(rateDesiredAxis[i], settings.MaximumRate[i]);
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] += ident_offsets[i];
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
} else {
// Get the desired rate. yaw is always in rate mode in system ident.
rateDesiredAxis[i] = bound_sym(stabDesiredAxis[i], settings.ManualRate[i]);
// Compute the inner loop only for yaw
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] += ident_offsets[i];
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
}
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_COORDINATEDFLIGHT:
switch (i) {
case YAW:
if (reinit) {
pids[PID_COORDINATED_FLIGHT_YAW].iAccumulator = 0;
pids[PID_RATE_YAW].iAccumulator = 0;
axis_lock_accum[YAW] = 0;
}
//If we are not in roll attitude mode, trigger an error
if (stabDesired.StabilizationMode[ROLL] != STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE)
{
error = true;
break ;
}
if (fabsf(stabDesired.Yaw) < COORDINATED_FLIGHT_MAX_YAW_THRESHOLD) { //If yaw is within the deadband...
if (fabsf(stabDesired.Roll) > COORDINATED_FLIGHT_MIN_ROLL_THRESHOLD) { // We're requesting more roll than the threshold
float accelsDataY;
AccelsyGet(&accelsDataY);
//Reset integral if we have changed roll to opposite direction from rudder. This implies that we have changed desired turning direction.
if ((stabDesired.Roll > 0 && actuatorDesiredAxis[YAW] < 0) ||
(stabDesired.Roll < 0 && actuatorDesiredAxis[YAW] > 0)){
pids[PID_COORDINATED_FLIGHT_YAW].iAccumulator = 0;
}
// Coordinate flight can simply be seen as ensuring that there is no lateral acceleration in the
// body frame. As such, we use the (noisy) accelerometer data as our measurement. Ideally, at
// some point in the future we will estimate acceleration and then we can use the estimated value
// instead of the measured value.
float errorSlip = -accelsDataY;
float command = pid_apply(&pids[PID_COORDINATED_FLIGHT_YAW], errorSlip, dT);
actuatorDesiredAxis[YAW] = bound_sym(command ,1.0);
// Reset axis-lock integrals
pids[PID_RATE_YAW].iAccumulator = 0;
axis_lock_accum[YAW] = 0;
} else if (fabsf(stabDesired.Roll) <= COORDINATED_FLIGHT_MIN_ROLL_THRESHOLD) { // We're requesting less roll than the threshold
// Axis lock on no gyro change
axis_lock_accum[YAW] += (0 - gyro_filtered[YAW]) * dT;
rateDesiredAxis[YAW] = pid_apply(&pids[PID_ATT_YAW], axis_lock_accum[YAW], dT);
rateDesiredAxis[YAW] = bound_sym(rateDesiredAxis[YAW], settings.MaximumRate[YAW]);
actuatorDesiredAxis[YAW] = pid_apply_setpoint(&pids[PID_RATE_YAW], rateDesiredAxis[YAW], gyro_filtered[YAW], dT);
actuatorDesiredAxis[YAW] = bound_sym(actuatorDesiredAxis[YAW],1.0f);
// Reset coordinated-flight integral
pids[PID_COORDINATED_FLIGHT_YAW].iAccumulator = 0;
}
} else { //... yaw is outside the deadband. Pass the manual input directly to the actuator.
actuatorDesiredAxis[YAW] = bound_sym(stabDesiredAxis[YAW], 1.0);
// Reset all integrals
pids[PID_COORDINATED_FLIGHT_YAW].iAccumulator = 0;
pids[PID_RATE_YAW].iAccumulator = 0;
axis_lock_accum[YAW] = 0;
}
break;
case ROLL:
case PITCH:
default:
//Coordinated Flight has no effect in these modes. Trigger a configuration error.
error = true;
break;
}
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_POI:
// The sanity check enforces this is only selectable for Yaw
// for a gimbal you can select pitch too.
if(reinit) {
pids[PID_GROUP_ATT + i].iAccumulator = 0;
pids[PID_GROUP_RATE + i].iAccumulator = 0;
}
float error;
float angle;
if (CameraDesiredHandle()) {
switch(i) {
case PITCH:
CameraDesiredDeclinationGet(&angle);
error = circular_modulus_deg(angle - attitudeActual.Pitch);
break;
case ROLL:
{
uint8_t roll_fraction = 0;
#ifdef GIMBAL
if (BrushlessGimbalSettingsHandle()) {
BrushlessGimbalSettingsRollFractionGet(&roll_fraction);
}
#endif /* GIMBAL */
// For ROLL POI mode we track the FC roll angle (scaled) to
// allow keeping some motion
CameraDesiredRollGet(&angle);
angle *= roll_fraction / 100.0f;
error = circular_modulus_deg(angle - attitudeActual.Roll);
}
break;
case YAW:
CameraDesiredBearingGet(&angle);
error = circular_modulus_deg(angle - attitudeActual.Yaw);
break;
default:
error = true;
}
} else
error = true;
// Compute the outer loop
rateDesiredAxis[i] = pid_apply(&pids[PID_GROUP_ATT + i], error, dT);
rateDesiredAxis[i] = bound_sym(rateDesiredAxis[i], settings.PoiMaximumRate[i]);
// Compute the inner loop
actuatorDesiredAxis[i] = pid_apply_setpoint(&pids[PID_GROUP_RATE + i], rateDesiredAxis[i], gyro_filtered[i], dT);
actuatorDesiredAxis[i] = bound_sym(actuatorDesiredAxis[i],1.0f);
break;
case STABILIZATIONDESIRED_STABILIZATIONMODE_NONE:
actuatorDesiredAxis[i] = bound_sym(stabDesiredAxis[i],1.0f);
break;
default:
error = true;
break;
}
}
if (settings.VbarPiroComp == STABILIZATIONSETTINGS_VBARPIROCOMP_TRUE)
stabilization_virtual_flybar_pirocomp(gyro_filtered[2], dT);
#if defined(RATEDESIRED_DIAGNOSTICS)
RateDesiredSet(&rateDesired);
#endif
// Save dT
actuatorDesired.UpdateTime = dT * 1000;
actuatorDesired.Throttle = stabDesired.Throttle;
if(flightStatus.FlightMode != FLIGHTSTATUS_FLIGHTMODE_MANUAL) {
ActuatorDesiredSet(&actuatorDesired);
} else {
// Force all axes to reinitialize when engaged
for(uint8_t i=0; i< MAX_AXES; i++)
previous_mode[i] = 255;
}
if(flightStatus.Armed != FLIGHTSTATUS_ARMED_ARMED ||
(lowThrottleZeroIntegral && stabDesired.Throttle < 0))
{
// Force all axes to reinitialize when engaged
for(uint8_t i=0; i< MAX_AXES; i++)
previous_mode[i] = 255;
}
// Clear or set alarms. Done like this to prevent toggling each cycle
// and hammering system alarms
if (error)
AlarmsSet(SYSTEMALARMS_ALARM_STABILIZATION,SYSTEMALARMS_ALARM_ERROR);
else
AlarmsClear(SYSTEMALARMS_ALARM_STABILIZATION);
}
}
/**
* Telemetry transmit task, regular priority
*
* Logic: We need to double buffer the DMA transfers. Pack the buffer until either
* 1) it is full (and then we should record the number of missed events then)
* 2) the current transaction is done (we should immediately schedule since we are slave)
* when done packing the buffer we should call PIOS_SPI_TransferBlock, change the active buffer
* and then take the semaphrore
*/
static void overoSyncTask(void *parameters)
{
UAVObjEvent ev;
// Kick off SPI transfers (once one is completed another will automatically transmit)
overosync->sent_objects = 0;
overosync->failed_objects = 0;
overosync->received_objects = 0;
uint32_t lastUpdateTime = PIOS_Thread_Systime();
uint32_t updateTime;
bool initialized = false;
uint8_t last_connected = OVEROSYNCSTATS_CONNECTED_FALSE;
// Loop forever
while (1) {
// Wait for queue message
if (PIOS_Queue_Receive(queue, &ev, PIOS_QUEUE_TIMEOUT_MAX) == true) {
// For the first seconds do not send updates to allow the
// overo to boot. Then enable it and act normally.
if (!initialized && PIOS_Thread_Systime() < 5000) {
continue;
} else if (!initialized) {
initialized = true;
PIOS_OVERO_Enable(pios_overo_id);
}
// Process event. This calls transmitData
UAVTalkSendObjectTimestamped(uavTalkCon, ev.obj, ev.instId, false, 0);
updateTime = PIOS_Thread_Systime();
if(((uint32_t) (updateTime - lastUpdateTime)) > 1000) {
// Update stats. This will trigger a local send event too
OveroSyncStatsData syncStats;
syncStats.Send = overosync->sent_bytes;
syncStats.Connected = syncStats.Send > 500 ? OVEROSYNCSTATS_CONNECTED_TRUE : OVEROSYNCSTATS_CONNECTED_FALSE;
syncStats.DroppedUpdates = overosync->failed_objects;
syncStats.Packets = PIOS_OVERO_GetPacketCount(pios_overo_id);
OveroSyncStatsSet(&syncStats);
overosync->failed_objects = 0;
overosync->sent_bytes = 0;
lastUpdateTime = updateTime;
// When first connected, send all the settings. Right now this
// will fail since all the settings will overfill the buffer and
if (last_connected == OVEROSYNCSTATS_CONNECTED_FALSE &&
syncStats.Connected == OVEROSYNCSTATS_CONNECTED_TRUE) {
UAVObjIterate(&send_settings);
}
// Because the previous code only happens on connection and the
// remote logging program doesn't send the settings to the log
// when arming starts we send all settings every thirty seconds
static uint32_t second_count = 0;
if (second_count ++ > 30) {
UAVObjIterate(&send_settings);
second_count = 0;
}
last_connected = syncStats.Connected;
}
// TODO: Check the receive buffer
}
}
}
