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OP-1217 change the way modules are enabled/disabled based on flightstatus
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1898d0ad35
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@ -181,52 +181,50 @@ static void pathfollowerTask(__attribute__((unused)) void *parameters)
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uint8_t result;
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// Check the combinations of flightmode and pathdesired mode
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switch (flightStatus.FlightMode) {
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case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
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case FLIGHTSTATUS_FLIGHTMODE_RETURNTOBASE:
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updatePathVelocity();
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result = updateFixedDesiredAttitude();
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if (result) {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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if (flightStatus.ControlChain.PathFollower == FLIGHTSTATUS_CONTROLCHAIN_TRUE) {
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if (flightStatus.ControlChain.PathPlanner == FLIGHTSTATUS_CONTROLCHAIN_FALSE) {
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updatePathVelocity();
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result = updateFixedDesiredAttitude();
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if (result) {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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}
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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}
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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}
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break;
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case FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER:
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pathStatus.UID = pathDesired.UID;
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pathStatus.Status = PATHSTATUS_STATUS_INPROGRESS;
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switch (pathDesired.Mode) {
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case PATHDESIRED_MODE_FLYENDPOINT:
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case PATHDESIRED_MODE_FLYVECTOR:
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case PATHDESIRED_MODE_FLYCIRCLERIGHT:
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case PATHDESIRED_MODE_FLYCIRCLELEFT:
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updatePathVelocity();
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result = updateFixedDesiredAttitude();
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if (result) {
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pathStatus.UID = pathDesired.UID;
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pathStatus.Status = PATHSTATUS_STATUS_INPROGRESS;
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switch (pathDesired.Mode) {
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case PATHDESIRED_MODE_FLYENDPOINT:
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case PATHDESIRED_MODE_FLYVECTOR:
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case PATHDESIRED_MODE_FLYCIRCLERIGHT:
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case PATHDESIRED_MODE_FLYCIRCLELEFT:
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updatePathVelocity();
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result = updateFixedDesiredAttitude();
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if (result) {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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} else {
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pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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}
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break;
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case PATHDESIRED_MODE_FIXEDATTITUDE:
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updateFixedAttitude(pathDesired.ModeParameters);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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} else {
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break;
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case PATHDESIRED_MODE_DISARMALARM:
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_CRITICAL);
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break;
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default:
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pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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break;
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}
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break;
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case PATHDESIRED_MODE_FIXEDATTITUDE:
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updateFixedAttitude(pathDesired.ModeParameters);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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break;
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case PATHDESIRED_MODE_DISARMALARM:
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_CRITICAL);
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break;
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default:
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pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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break;
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}
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break;
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default:
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} else {
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// Be cleaner and get rid of global variables
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northVelIntegral = 0;
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eastVelIntegral = 0;
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@ -234,8 +232,6 @@ static void pathfollowerTask(__attribute__((unused)) void *parameters)
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courseIntegral = 0;
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speedIntegral = 0;
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powerIntegral = 0;
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break;
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}
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PathStatusSet(&pathStatus);
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}
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@ -138,7 +138,7 @@ static void pathPlannerTask()
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FlightStatusData flightStatus;
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FlightStatusGet(&flightStatus);
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if (flightStatus.FlightMode != FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER) {
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if (flightStatus.ControlChain.PathPlanner != FLIGHTSTATUS_CONTROLCHAIN_TRUE) {
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pathplanner_active = false;
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if (!validPathPlan) {
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// unverified path plans are only a warning while we are not in pathplanner mode
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@ -50,7 +50,6 @@
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#include "flightstatus.h"
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#include "manualcontrolsettings.h"
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#include "flightmodesettings.h"
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#include "manualcontrol.h" // Just to get a macro
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#include "taskinfo.h"
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// Math libraries
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@ -669,7 +668,7 @@ static void stabilizationTask(__attribute__((unused)) void *parameters)
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}
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}
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if (PARSE_FLIGHT_MODE(flightStatus.FlightMode) != FLIGHTMODE_MANUAL) {
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if (flightStatus.ControlChain.Stabilization == FLIGHTSTATUS_CONTROLCHAIN_TRUE) {
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ActuatorDesiredSet(&actuatorDesired);
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} else {
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// Force all axes to reinitialize when engaged
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@ -206,55 +206,53 @@ static void vtolPathFollowerTask(__attribute__((unused)) void *parameters)
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PathDesiredGet(&pathDesired);
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// Check the combinations of flightmode and pathdesired mode
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switch (flightStatus.FlightMode) {
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case FLIGHTSTATUS_FLIGHTMODE_LAND:
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case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
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case FLIGHTSTATUS_FLIGHTMODE_RETURNTOBASE:
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updateEndpointVelocity();
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updateVtolDesiredAttitude(false);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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if (flightStatus.ControlChain.PathFollower == FLIGHTSTATUS_CONTROLCHAIN_TRUE) {
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if (flightStatus.ControlChain.PathPlanner == FLIGHTSTATUS_CONTROLCHAIN_FALSE) {
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if (flightStatus.FlightMode == FLIGHTSTATUS_FLIGHTMODE_POI) {
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updateEndpointVelocity();
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updateVtolDesiredAttitude(true);
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updatePOIBearing();
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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}
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} else {
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updateEndpointVelocity();
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updateVtolDesiredAttitude(false);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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}
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}
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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pathStatus.UID = pathDesired.UID;
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pathStatus.Status = PATHSTATUS_STATUS_INPROGRESS;
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switch (pathDesired.Mode) {
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// TODO: Make updateVtolDesiredAttitude and velocity report success and update PATHSTATUS_STATUS accordingly
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case PATHDESIRED_MODE_FLYENDPOINT:
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case PATHDESIRED_MODE_FLYVECTOR:
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case PATHDESIRED_MODE_FLYCIRCLERIGHT:
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case PATHDESIRED_MODE_FLYCIRCLELEFT:
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updatePathVelocity();
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updateVtolDesiredAttitude(false);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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break;
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case PATHDESIRED_MODE_FIXEDATTITUDE:
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updateFixedAttitude(pathDesired.ModeParameters);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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break;
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case PATHDESIRED_MODE_DISARMALARM:
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_CRITICAL);
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break;
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default:
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pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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break;
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}
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PathStatusSet(&pathStatus);
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}
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break;
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case FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER:
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pathStatus.UID = pathDesired.UID;
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pathStatus.Status = PATHSTATUS_STATUS_INPROGRESS;
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switch (pathDesired.Mode) {
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// TODO: Make updateVtolDesiredAttitude and velocity report success and update PATHSTATUS_STATUS accordingly
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case PATHDESIRED_MODE_FLYENDPOINT:
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case PATHDESIRED_MODE_FLYVECTOR:
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case PATHDESIRED_MODE_FLYCIRCLERIGHT:
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case PATHDESIRED_MODE_FLYCIRCLELEFT:
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updatePathVelocity();
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updateVtolDesiredAttitude(false);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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break;
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case PATHDESIRED_MODE_FIXEDATTITUDE:
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updateFixedAttitude(pathDesired.ModeParameters);
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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break;
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case PATHDESIRED_MODE_DISARMALARM:
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_CRITICAL);
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break;
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default:
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pathStatus.Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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break;
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}
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PathStatusSet(&pathStatus);
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break;
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case FLIGHTSTATUS_FLIGHTMODE_POI:
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if (pathDesired.Mode == PATHDESIRED_MODE_FLYENDPOINT) {
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updateEndpointVelocity();
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updateVtolDesiredAttitude(true);
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updatePOIBearing();
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} else {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_ERROR);
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}
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break;
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default:
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} else {
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// Be cleaner and get rid of global variables
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northVelIntegral = 0;
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eastVelIntegral = 0;
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@ -267,8 +265,6 @@ static void vtolPathFollowerTask(__attribute__((unused)) void *parameters)
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StabilizationDesiredData stabDesired;
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StabilizationDesiredGet(&stabDesired);
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thrustOffset = stabDesired.Thrust;
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break;
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}
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AlarmsClear(SYSTEMALARMS_ALARM_GUIDANCE);
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@ -6,6 +6,14 @@
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<!-- Note these enumerated values should be the same as ManualControlSettings -->
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<field name="FlightMode" units="" type="enum" elements="1" options="Manual,Stabilized1,Stabilized2,Stabilized3,Autotune,AltitudeHold,AltitudeVario,VelocityControl,PositionHold,ReturnToBase,Land,PathPlanner,POI"/>
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<field name="ControlChain" units="bool" type="enum" options="false,true">
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<elementnames>
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<elementname>Stabilization</elementname>
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<elementname>PathFollower</elementname>
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<elementname>PathPlanner</elementname>
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</elementnames>
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</field>
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<access gcs="readwrite" flight="readwrite"/>
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<telemetrygcs acked="false" updatemode="manual" period="0"/>
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<telemetryflight acked="false" updatemode="onchange" period="5000"/>
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