/**
* Module thread, should not return.
*/
static void vtolPathFollowerTask(void *parameters)
{
SystemSettingsData systemSettings;
FlightStatusData flightStatus;
portTickType lastUpdateTime;
VtolPathFollowerSettingsConnectCallback(SettingsUpdatedCb);
PathDesiredConnectCallback(SettingsUpdatedCb);
VtolPathFollowerSettingsGet(&guidanceSettings);
PathDesiredGet(&pathDesired);
// Main task loop
lastUpdateTime = xTaskGetTickCount();
while (1) {
// Conditions when this runs:
// 1. Must have VTOL type airframe
// 2. Flight mode is PositionHold and PathDesired.Mode is Endpoint OR
// FlightMode is PathPlanner and PathDesired.Mode is Endpoint or Path
SystemSettingsGet(&systemSettings);
if ( (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_VTOL) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_QUADP) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_QUADX) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXA) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXAX) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_HEXACOAX) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTO) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOV) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOCOAXP) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_OCTOCOAXX) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_TRI) )
{
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_WARNING);
vTaskDelay(1000);
continue;
}
// Continue collecting data if not enough time
vTaskDelayUntil(&lastUpdateTime, MS2TICKS(guidanceSettings.UpdatePeriod));
// Convert the accels into the NED frame
updateNedAccel();
FlightStatusGet(&flightStatus);
// Check the combinations of flightmode and pathdesired mode
switch(flightStatus.FlightMode) {
/* This combination of RETURNTOHOME and HOLDPOSITION looks strange but
* is correct. RETURNTOHOME mode uses HOLDPOSITION with the position
* set to home */
case FLIGHTSTATUS_FLIGHTMODE_RETURNTOHOME:
if (pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateVtolDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
if (pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateVtolDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
case FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER:
if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT ||
pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateVtolDesiredAttitude();
} else if (pathDesired.Mode == PATHDESIRED_MODE_FLYVECTOR ||
pathDesired.Mode == PATHDESIRED_MODE_FLYCIRCLELEFT ||
pathDesired.Mode == PATHDESIRED_MODE_FLYCIRCLERIGHT) {
updatePathVelocity();
updateVtolDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
default:
for (uint32_t i = 0; i < VTOL_PID_NUM; i++)
pid_zero(&vtol_pids[i]);
// Track throttle before engaging this mode. Cheap system ident
StabilizationDesiredData stabDesired;
StabilizationDesiredGet(&stabDesired);
throttleOffset = stabDesired.Throttle;
break;
}
AlarmsClear(SYSTEMALARMS_ALARM_PATHFOLLOWER);
}
}
/**
* Module thread, should not return.
*/
static void groundPathFollowerTask(void *parameters)
{
SystemSettingsData systemSettings;
FlightStatusData flightStatus;
uint32_t lastUpdateTime;
GroundPathFollowerSettingsConnectCallback(SettingsUpdatedCb);
PathDesiredConnectCallback(SettingsUpdatedCb);
GroundPathFollowerSettingsGet(&guidanceSettings);
PathDesiredGet(&pathDesired);
// Main task loop
lastUpdateTime = PIOS_Thread_Systime();
while (1) {
// Conditions when this runs:
// 1. Must have GROUND type airframe
// 2. Flight mode is PositionHold and PathDesired.Mode is Endpoint OR
// FlightMode is PathPlanner and PathDesired.Mode is Endpoint or Path
SystemSettingsGet(&systemSettings);
if ( (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_GROUNDVEHICLECAR) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_GROUNDVEHICLEDIFFERENTIAL) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_GROUNDVEHICLEMOTORCYCLE) )
{
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_WARNING);
PIOS_Thread_Sleep(1000);
continue;
}
// Continue collecting data if not enough time
PIOS_Thread_Sleep_Until(&lastUpdateTime, guidanceSettings.UpdatePeriod);
// Convert the accels into the NED frame
updateNedAccel();
FlightStatusGet(&flightStatus);
// Check the combinations of flightmode and pathdesired mode
switch(flightStatus.FlightMode) {
/* This combination of RETURNTOHOME and HOLDPOSITION looks strange but
* is correct. RETURNTOHOME mode uses HOLDPOSITION with the position
* set to home */
case FLIGHTSTATUS_FLIGHTMODE_RETURNTOHOME:
if (pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateGroundDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
if (pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateGroundDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
case FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER:
if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT ||
pathDesired.Mode == PATHDESIRED_MODE_HOLDPOSITION) {
updateEndpointVelocity();
updateGroundDesiredAttitude();
} else if (pathDesired.Mode == PATHDESIRED_MODE_FLYVECTOR ||
pathDesired.Mode == PATHDESIRED_MODE_FLYCIRCLELEFT ||
pathDesired.Mode == PATHDESIRED_MODE_FLYCIRCLERIGHT) {
updatePathVelocity();
updateGroundDesiredAttitude();
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_ERROR);
}
break;
default:
// Be cleaner and get rid of global variables
northVelIntegral = 0;
eastVelIntegral = 0;
northPosIntegral = 0;
eastPosIntegral = 0;
// Track throttle before engaging this mode. Cheap system ident
StabilizationDesiredData stabDesired;
StabilizationDesiredGet(&stabDesired);
throttleOffset = stabDesired.Throttle;
break;
}
AlarmsClear(SYSTEMALARMS_ALARM_PATHFOLLOWER);
}
}
/**
* Module thread, should not return.
*/
static void pathfollowerTask(void *parameters)
{
SystemSettingsData systemSettings;
FlightStatusData flightStatus;
uint32_t lastUpdateTime;
AirspeedActualConnectCallback(airspeedActualUpdatedCb);
FixedWingPathFollowerSettingsConnectCallback(SettingsUpdatedCb);
FixedWingAirspeedsConnectCallback(SettingsUpdatedCb);
PathDesiredConnectCallback(SettingsUpdatedCb);
// Force update of all the settings
SettingsUpdatedCb(NULL);
FixedWingPathFollowerSettingsGet(&fixedwingpathfollowerSettings);
path_desired_updated = false;
PathDesiredGet(&pathDesired);
PathDesiredConnectCallback(pathDesiredUpdated);
// Main task loop
lastUpdateTime = PIOS_Thread_Systime();
while (1) {
// Conditions when this runs:
// 1. Must have FixedWing type airframe
// 2. Flight mode is PositionHold and PathDesired.Mode is Endpoint OR
// FlightMode is PathPlanner and PathDesired.Mode is Endpoint or Path
SystemSettingsGet(&systemSettings);
if ( (systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_FIXEDWING) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_FIXEDWINGELEVON) &&
(systemSettings.AirframeType != SYSTEMSETTINGS_AIRFRAMETYPE_FIXEDWINGVTAIL) )
{
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_CRITICAL);
PIOS_Thread_Sleep(1000);
continue;
}
// Continue collecting data if not enough time
PIOS_Thread_Sleep_Until(&lastUpdateTime, fixedwingpathfollowerSettings.UpdatePeriod);
static uint8_t last_flight_mode;
FlightStatusGet(&flightStatus);
PathStatusGet(&pathStatus);
PositionActualData positionActual;
static enum {FW_FOLLOWER_IDLE, FW_FOLLOWER_RUNNING, FW_FOLLOWER_ERR} state = FW_FOLLOWER_IDLE;
// Check whether an update to the path desired occured and we should
// process it. This makes sure that the follower alarm state is
// updated.
bool process_path_desired_update =
(last_flight_mode == FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER ||
last_flight_mode == FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER) &&
path_desired_updated;
path_desired_updated = false;
// Process most of these when the flight mode changes
// except when in path following mode in which case
// each iteration must make sure this has the latest
// PathDesired
if (flightStatus.FlightMode != last_flight_mode ||
process_path_desired_update) {
last_flight_mode = flightStatus.FlightMode;
switch(flightStatus.FlightMode) {
case FLIGHTSTATUS_FLIGHTMODE_RETURNTOHOME:
state = FW_FOLLOWER_RUNNING;
PositionActualGet(&positionActual);
pathDesired.Mode = PATHDESIRED_MODE_CIRCLEPOSITIONRIGHT;
pathDesired.Start[0] = positionActual.North;
pathDesired.Start[1] = positionActual.East;
pathDesired.Start[2] = positionActual.Down;
pathDesired.End[0] = 0;
pathDesired.End[1] = 0;
pathDesired.End[2] = -30.0f;
pathDesired.ModeParameters = fixedwingpathfollowerSettings.OrbitRadius;
pathDesired.StartingVelocity = fixedWingAirspeeds.CruiseSpeed;
pathDesired.EndingVelocity = fixedWingAirspeeds.CruiseSpeed;
PathDesiredSet(&pathDesired);
break;
case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
state = FW_FOLLOWER_RUNNING;
PositionActualGet(&positionActual);
pathDesired.Mode = PATHDESIRED_MODE_CIRCLEPOSITIONRIGHT;
pathDesired.Start[0] = positionActual.North;
pathDesired.Start[1] = positionActual.East;
pathDesired.Start[2] = positionActual.Down;
pathDesired.End[0] = positionActual.North;
pathDesired.End[1] = positionActual.East;
pathDesired.End[2] = positionActual.Down;
pathDesired.ModeParameters = fixedwingpathfollowerSettings.OrbitRadius;
pathDesired.StartingVelocity = fixedWingAirspeeds.CruiseSpeed;
pathDesired.EndingVelocity = fixedWingAirspeeds.CruiseSpeed;
PathDesiredSet(&pathDesired);
break;
case FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER:
case FLIGHTSTATUS_FLIGHTMODE_TABLETCONTROL:
state = FW_FOLLOWER_RUNNING;
PathDesiredGet(&pathDesired);
switch(pathDesired.Mode) {
case PATHDESIRED_MODE_ENDPOINT:
case PATHDESIRED_MODE_VECTOR:
case PATHDESIRED_MODE_CIRCLERIGHT:
case PATHDESIRED_MODE_CIRCLELEFT:
break;
default:
state = FW_FOLLOWER_ERR;
pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
PathStatusSet(&pathStatus);
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_CRITICAL);
break;
}
break;
default:
state = FW_FOLLOWER_IDLE;
break;
}
}
switch(state) {
case FW_FOLLOWER_RUNNING:
{
updatePathVelocity();
uint8_t result = updateFixedDesiredAttitude();
if (result) {
AlarmsClear(SYSTEMALARMS_ALARM_PATHFOLLOWER);
} else {
AlarmsSet(SYSTEMALARMS_ALARM_PATHFOLLOWER,SYSTEMALARMS_ALARM_WARNING);
}
PathStatusSet(&pathStatus);
break;
}
case FW_FOLLOWER_IDLE:
// Be cleaner and get rid of global variables
northVelIntegral = 0;
eastVelIntegral = 0;
downVelIntegral = 0;
bearingIntegral = 0;
speedIntegral = 0;
accelIntegral = 0;
powerIntegral = 0;
airspeedErrorInt = 0;
AlarmsClear(SYSTEMALARMS_ALARM_PATHFOLLOWER);
break;
case FW_FOLLOWER_ERR:
default:
// Leave alarms set above
break;
}
}
}
/**
* fixed wing autopilot:
* straight forward:
* 1. update path velocity for limited motion crafts
* 2. update attitude according to default fixed wing pathfollower algorithm
*/
uint8_t FixedWingFlyController::updateAutoPilotFixedWing()
{
updatePathVelocity(fixedWingSettings->CourseFeedForward, true);
return updateFixedDesiredAttitude();
}