/**
* Processes queue events
*/
static void processObjEvent(UAVObjEvent * ev)
{
UAVObjMetadata metadata;
UAVObjUpdateMode updateMode;
FlightTelemetryStatsData flightStats;
int32_t retries;
int32_t success;
if (ev->obj == 0) {
updateTelemetryStats();
} else if (ev->obj == GCSTelemetryStatsHandle()) {
gcsTelemetryStatsUpdated();
} else {
// Only process event if connected to GCS or if object FlightTelemetryStats is updated
FlightTelemetryStatsGet(&flightStats);
// Get object metadata
UAVObjGetMetadata(ev->obj, &metadata);
updateMode = UAVObjGetTelemetryUpdateMode(&metadata);
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED || ev->obj == FlightTelemetryStatsHandle()) {
// Act on event
retries = 0;
success = -1;
if (ev->event == EV_UPDATED || ev->event == EV_UPDATED_MANUAL || ((ev->event == EV_UPDATED_PERIODIC) && (updateMode != UPDATEMODE_THROTTLED))) {
// Send update to GCS (with retries)
while (retries < MAX_RETRIES && success == -1) {
success = UAVTalkSendObject(uavTalkCon, ev->obj, ev->instId, UAVObjGetTelemetryAcked(&metadata), REQ_TIMEOUT_MS); // call blocks until ack is received or timeout
++retries;
}
// Update stats
txRetries += (retries - 1);
if (success == -1) {
++txErrors;
}
} else if (ev->event == EV_UPDATE_REQ) {
// Request object update from GCS (with retries)
while (retries < MAX_RETRIES && success == -1) {
success = UAVTalkSendObjectRequest(uavTalkCon, ev->obj, ev->instId, REQ_TIMEOUT_MS); // call blocks until update is received or timeout
++retries;
}
// Update stats
txRetries += (retries - 1);
if (success == -1) {
++txErrors;
}
}
// If this is a metaobject then make necessary telemetry updates
if (UAVObjIsMetaobject(ev->obj)) {
updateObject(UAVObjGetLinkedObj(ev->obj), EV_NONE); // linked object will be the actual object the metadata are for
}
}
if((updateMode == UPDATEMODE_THROTTLED) && !UAVObjIsMetaobject(ev->obj)) {
// If this is UPDATEMODE_THROTTLED, the event mask changes on every event.
updateObject(ev->obj, ev->event);
}
}
}
/**
* Called each time the GCS telemetry stats object is updated.
* Trigger a flight telemetry stats update if a connection is not
* yet established.
*/
static void gcsTelemetryStatsUpdated()
{
FlightTelemetryStatsData flightStats;
GCSTelemetryStatsData gcsStats;
FlightTelemetryStatsGet(&flightStats);
GCSTelemetryStatsGet(&gcsStats);
if (flightStats.Status != FLIGHTTELEMETRYSTATS_STATUS_CONNECTED || gcsStats.Status != GCSTELEMETRYSTATS_STATUS_CONNECTED) {
updateTelemetryStats();
}
}
/**
* Processes queue events
*/
static void processObjEvent(UAVObjEvent * ev)
{
UAVObjMetadata metadata;
FlightTelemetryStatsData flightStats;
int32_t retries;
int32_t success;
if (ev->obj == 0) {
updateTelemetryStats();
} else if (ev->obj == GCSTelemetryStatsHandle()) {
gcsTelemetryStatsUpdated();
} else if (ev->obj == TelemetrySettingsHandle()) {
updateSettings();
} else {
// Only process event if connected to GCS or if object FlightTelemetryStats is updated
FlightTelemetryStatsGet(&flightStats);
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED || ev->obj == FlightTelemetryStatsHandle()) {
// Get object metadata
UAVObjGetMetadata(ev->obj, &metadata);
// Act on event
retries = 0;
success = -1;
if (ev->event == EV_UPDATED || ev->event == EV_UPDATED_MANUAL) {
// Send update to GCS (with retries)
while (retries < MAX_RETRIES && success == -1) {
success = UAVTalkSendObject(ev->obj, ev->instId, metadata.telemetryAcked, REQ_TIMEOUT_MS); // call blocks until ack is received or timeout
++retries;
}
// Update stats
txRetries += (retries - 1);
if (success == -1) {
++txErrors;
}
} else if (ev->event == EV_UPDATE_REQ) {
// Request object update from GCS (with retries)
while (retries < MAX_RETRIES && success == -1) {
success = UAVTalkSendObjectRequest(ev->obj, ev->instId, REQ_TIMEOUT_MS); // call blocks until update is received or timeout
++retries;
}
// Update stats
txRetries += (retries - 1);
if (success == -1) {
++txErrors;
}
}
// If this is a metaobject then make necessary telemetry updates
if (UAVObjIsMetaobject(ev->obj)) {
updateObject(UAVObjGetLinkedObj(ev->obj)); // linked object will be the actual object the metadata are for
}
}
}
}
/**
* Module task
*/
static void manualControlTask(void *parameters)
{
ManualControlSettingsData settings;
ManualControlCommandData cmd;
portTickType lastSysTime;
float flightMode = 0;
uint8_t disconnected_count = 0;
uint8_t connected_count = 0;
enum { CONNECTED, DISCONNECTED } connection_state = DISCONNECTED;
// Make sure unarmed on power up
ManualControlCommandGet(&cmd);
cmd.Armed = MANUALCONTROLCOMMAND_ARMED_FALSE;
ManualControlCommandSet(&cmd);
armState = ARM_STATE_DISARMED;
// Main task loop
lastSysTime = xTaskGetTickCount();
while (1) {
float scaledChannel[MANUALCONTROLCOMMAND_CHANNEL_NUMELEM];
// Wait until next update
vTaskDelayUntil(&lastSysTime, UPDATE_PERIOD_MS / portTICK_RATE_MS);
PIOS_WDG_UpdateFlag(PIOS_WDG_MANUAL);
// Read settings
ManualControlSettingsGet(&settings);
if (ManualControlCommandReadOnly(&cmd)) {
FlightTelemetryStatsData flightTelemStats;
FlightTelemetryStatsGet(&flightTelemStats);
if(flightTelemStats.Status != FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
/* trying to fly via GCS and lost connection. fall back to transmitter */
UAVObjMetadata metadata;
UAVObjGetMetadata(&cmd, &metadata);
metadata.access = ACCESS_READWRITE;
UAVObjSetMetadata(&cmd, &metadata);
}
}
if (!ManualControlCommandReadOnly(&cmd)) {
// Check settings, if error raise alarm
if (settings.Roll >= MANUALCONTROLSETTINGS_ROLL_NONE ||
settings.Pitch >= MANUALCONTROLSETTINGS_PITCH_NONE ||
settings.Yaw >= MANUALCONTROLSETTINGS_YAW_NONE ||
settings.Throttle >= MANUALCONTROLSETTINGS_THROTTLE_NONE ||
settings.FlightMode >= MANUALCONTROLSETTINGS_FLIGHTMODE_NONE) {
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_CRITICAL);
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
ManualControlCommandSet(&cmd);
continue;
}
// Read channel values in us
// TODO: settings.InputMode is currently ignored because PIOS will not allow runtime
// selection of PWM and PPM. The configuration is currently done at compile time in
// the pios_config.h file.
for (int n = 0; n < MANUALCONTROLCOMMAND_CHANNEL_NUMELEM; ++n) {
#if defined(PIOS_INCLUDE_PWM)
cmd.Channel[n] = PIOS_PWM_Get(n);
#elif defined(PIOS_INCLUDE_PPM)
cmd.Channel[n] = PIOS_PPM_Get(n);
#elif defined(PIOS_INCLUDE_SPEKTRUM)
cmd.Channel[n] = PIOS_SPEKTRUM_Get(n);
#endif
scaledChannel[n] = scaleChannel(cmd.Channel[n], settings.ChannelMax[n], settings.ChannelMin[n], settings.ChannelNeutral[n], 0);
}
// Scale channels to -1 -> +1 range
cmd.Roll = scaledChannel[settings.Roll];
cmd.Pitch = scaledChannel[settings.Pitch];
cmd.Yaw = scaledChannel[settings.Yaw];
cmd.Throttle = scaledChannel[settings.Throttle];
flightMode = scaledChannel[settings.FlightMode];
if (settings.Accessory1 != MANUALCONTROLSETTINGS_ACCESSORY1_NONE)
cmd.Accessory1 = scaledChannel[settings.Accessory1];
else
cmd.Accessory1 = 0;
if (settings.Accessory2 != MANUALCONTROLSETTINGS_ACCESSORY2_NONE)
cmd.Accessory2 = scaledChannel[settings.Accessory2];
else
cmd.Accessory2 = 0;
if (settings.Accessory3 != MANUALCONTROLSETTINGS_ACCESSORY3_NONE)
cmd.Accessory3 = scaledChannel[settings.Accessory3];
else
cmd.Accessory3 = 0;
// Note here the code is ass
if (flightMode < -FLIGHT_MODE_LIMIT)
cmd.FlightMode = settings.FlightModePosition[0];
else if (flightMode > FLIGHT_MODE_LIMIT)
cmd.FlightMode = settings.FlightModePosition[2];
else
cmd.FlightMode = settings.FlightModePosition[1];
// Update the ManualControlCommand object
ManualControlCommandSet(&cmd);
// This seems silly to set then get, but the reason is if the GCS is
// the control input, the set command will be blocked by the read only
// setting and the get command will pull the right values from telemetry
} else
ManualControlCommandGet(&cmd); /* Under GCS control */
// Implement hysteresis loop on connection status
// Must check both Max and Min in case they reversed
if (!ManualControlCommandReadOnly(&cmd) &&
cmd.Channel[settings.Throttle] < settings.ChannelMax[settings.Throttle] - CONNECTION_OFFSET &&
cmd.Channel[settings.Throttle] < settings.ChannelMin[settings.Throttle] - CONNECTION_OFFSET) {
if (disconnected_count++ > 10) {
connection_state = DISCONNECTED;
connected_count = 0;
disconnected_count = 0;
} else
disconnected_count++;
} else {
if (connected_count++ > 10) {
connection_state = CONNECTED;
connected_count = 0;
disconnected_count = 0;
} else
connected_count++;
}
if (connection_state == DISCONNECTED) {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
cmd.Throttle = -1; // Shut down engine with no control
cmd.Roll = 0;
cmd.Yaw = 0;
cmd.Pitch = 0;
//cmd.FlightMode = MANUALCONTROLCOMMAND_FLIGHTMODE_AUTO; // don't do until AUTO implemented and functioning
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_WARNING);
ManualControlCommandSet(&cmd);
} else {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_TRUE;
AlarmsClear(SYSTEMALARMS_ALARM_MANUALCONTROL);
ManualControlCommandSet(&cmd);
}
//
// Arming and Disarming mechanism
//
// Look for state changes and write in newArmState
uint8_t newCmdArmed = cmd.Armed; // By default, keep the arming state the same
if (settings.Arming == MANUALCONTROLSETTINGS_ARMING_ALWAYSDISARMED) {
// In this configuration we always disarm
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_FALSE;
} else {
// In all other cases, we will not change the arm state when disconnected
if (connection_state == CONNECTED)
{
if (settings.Arming == MANUALCONTROLSETTINGS_ARMING_ALWAYSARMED) {
// In this configuration, we go into armed state as soon as the throttle is low, never disarm
if (cmd.Throttle < 0) {
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_TRUE;
}
} else {
// When the configuration is not "Always armed" and no "Always disarmed",
// the state will not be changed when the throttle is not low
if (cmd.Throttle < 0) {
static portTickType armedDisarmStart;
float armingInputLevel = 0;
// Calc channel see assumptions7
switch ( (settings.Arming-MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 ) {
case ARMING_CHANNEL_ROLL: armingInputLevel = cmd.Roll; break;
case ARMING_CHANNEL_PITCH: armingInputLevel = cmd.Pitch; break;
case ARMING_CHANNEL_YAW: armingInputLevel = cmd.Yaw; break;
}
bool manualArm = false;
bool manualDisarm = false;
if (connection_state == CONNECTED) {
// Should use RC input only if RX is connected
if (armingInputLevel <= -0.90)
manualArm = true;
else if (armingInputLevel >= +0.90)
manualDisarm = true;
}
// Swap arm-disarming see assumptions8
if ((settings.Arming-MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2) {
bool temp = manualArm;
manualArm = manualDisarm;
manualDisarm = temp;
}
switch(armState) {
case ARM_STATE_DISARMED:
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_FALSE;
if (manualArm)
{
if (okToArm()) // only allow arming if it's OK too
{
armedDisarmStart = lastSysTime;
armState = ARM_STATE_ARMING_MANUAL;
}
}
break;
case ARM_STATE_ARMING_MANUAL:
if (manualArm) {
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > ARMED_TIME_MS)
armState = ARM_STATE_ARMED;
}
else
armState = ARM_STATE_DISARMED;
break;
case ARM_STATE_ARMED:
// When we get here, the throttle is low,
// we go immediately to disarming due to timeout, also when the disarming mechanism is not enabled
armedDisarmStart = lastSysTime;
armState = ARM_STATE_DISARMING_TIMEOUT;
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_TRUE;
break;
case ARM_STATE_DISARMING_TIMEOUT:
// We get here when armed while throttle low, even when the arming timeout is not enabled
if (settings.ArmedTimeout != 0)
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > settings.ArmedTimeout)
armState = ARM_STATE_DISARMED;
// Switch to disarming due to manual control when needed
if (manualDisarm) {
armedDisarmStart = lastSysTime;
armState = ARM_STATE_DISARMING_MANUAL;
}
break;
case ARM_STATE_DISARMING_MANUAL:
if (manualDisarm) {
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > ARMED_TIME_MS)
armState = ARM_STATE_DISARMED;
}
else
armState = ARM_STATE_ARMED;
break;
} // End Switch
} else {
// The throttle is not low, in case we where arming or disarming, abort
switch(armState) {
case ARM_STATE_DISARMING_MANUAL:
case ARM_STATE_DISARMING_TIMEOUT:
armState = ARM_STATE_ARMED;
break;
case ARM_STATE_ARMING_MANUAL:
armState = ARM_STATE_DISARMED;
break;
default:
// Nothing needs to be done in the other states
break;
}
}
}
}
}
// Update cmd object when needed
if (newCmdArmed != cmd.Armed) {
cmd.Armed = newCmdArmed;
ManualControlCommandSet(&cmd);
}
//
// End of arming/disarming
//
// Depending on the mode update the Stabilization or Actuator objects
switch(PARSE_FLIGHT_MODE(cmd.FlightMode)) {
case FLIGHTMODE_UNDEFINED:
// This reflects a bug in the code architecture!
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_CRITICAL);
break;
case FLIGHTMODE_MANUAL:
updateActuatorDesired(&cmd);
break;
case FLIGHTMODE_STABILIZED:
updateStabilizationDesired(&cmd, &settings);
break;
case FLIGHTMODE_GUIDANCE:
// TODO: Implement
break;
}
}
}
/**
* Module task
*/
static void manualControlTask(void *parameters)
{
ManualControlSettingsData settings;
StabilizationSettingsData stabSettings;
ManualControlCommandData cmd;
ActuatorDesiredData actuator;
AttitudeDesiredData attitude;
RateDesiredData rate;
portTickType lastSysTime;
float flightMode;
uint8_t disconnected_count = 0;
uint8_t connected_count = 0;
enum { CONNECTED, DISCONNECTED } connection_state = DISCONNECTED;
// Make sure unarmed on power up
ManualControlCommandGet(&cmd);
cmd.Armed = MANUALCONTROLCOMMAND_ARMED_FALSE;
ManualControlCommandSet(&cmd);
armState = ARM_STATE_DISARMED;
// Main task loop
lastSysTime = xTaskGetTickCount();
while (1) {
float scaledChannel[MANUALCONTROLCOMMAND_CHANNEL_NUMELEM];
// Wait until next update
vTaskDelayUntil(&lastSysTime, UPDATE_PERIOD_MS / portTICK_RATE_MS);
PIOS_WDG_UpdateFlag(PIOS_WDG_MANUAL);
// Read settings
ManualControlSettingsGet(&settings);
StabilizationSettingsGet(&stabSettings);
if (ManualControlCommandReadOnly(&cmd)) {
FlightTelemetryStatsData flightTelemStats;
FlightTelemetryStatsGet(&flightTelemStats);
if(flightTelemStats.Status != FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
/* trying to fly via GCS and lost connection. fall back to transmitter */
UAVObjMetadata metadata;
UAVObjGetMetadata(&cmd, &metadata);
metadata.access = ACCESS_READWRITE;
UAVObjSetMetadata(&cmd, &metadata);
}
}
if (!ManualControlCommandReadOnly(&cmd)) {
// Check settings, if error raise alarm
if (settings.Roll >= MANUALCONTROLSETTINGS_ROLL_NONE ||
settings.Pitch >= MANUALCONTROLSETTINGS_PITCH_NONE ||
settings.Yaw >= MANUALCONTROLSETTINGS_YAW_NONE ||
settings.Throttle >= MANUALCONTROLSETTINGS_THROTTLE_NONE ||
settings.FlightMode >= MANUALCONTROLSETTINGS_FLIGHTMODE_NONE) {
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_CRITICAL);
cmd.FlightMode = MANUALCONTROLCOMMAND_FLIGHTMODE_AUTO;
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
ManualControlCommandSet(&cmd);
continue;
}
// Read channel values in us
// TODO: settings.InputMode is currently ignored because PIOS will not allow runtime
// selection of PWM and PPM. The configuration is currently done at compile time in
// the pios_config.h file.
for (int n = 0; n < MANUALCONTROLCOMMAND_CHANNEL_NUMELEM; ++n) {
#if defined(PIOS_INCLUDE_PWM)
cmd.Channel[n] = PIOS_PWM_Get(n);
#elif defined(PIOS_INCLUDE_PPM)
cmd.Channel[n] = PIOS_PPM_Get(n);
#elif defined(PIOS_INCLUDE_SPEKTRUM)
cmd.Channel[n] = PIOS_SPEKTRUM_Get(n);
#endif
scaledChannel[n] = scaleChannel(cmd.Channel[n], settings.ChannelMax[n], settings.ChannelMin[n], settings.ChannelNeutral[n]);
}
// Scale channels to -1 -> +1 range
cmd.Roll = scaledChannel[settings.Roll];
cmd.Pitch = scaledChannel[settings.Pitch];
cmd.Yaw = scaledChannel[settings.Yaw];
cmd.Throttle = scaledChannel[settings.Throttle];
flightMode = scaledChannel[settings.FlightMode];
if (settings.Accessory1 != MANUALCONTROLSETTINGS_ACCESSORY1_NONE)
cmd.Accessory1 = scaledChannel[settings.Accessory1];
else
cmd.Accessory1 = 0;
if (settings.Accessory2 != MANUALCONTROLSETTINGS_ACCESSORY2_NONE)
cmd.Accessory2 = scaledChannel[settings.Accessory2];
else
cmd.Accessory2 = 0;
if (settings.Accessory3 != MANUALCONTROLSETTINGS_ACCESSORY3_NONE)
cmd.Accessory3 = scaledChannel[settings.Accessory3];
else
cmd.Accessory3 = 0;
if (flightMode < -FLIGHT_MODE_LIMIT) {
// Position 1
for(int i = 0; i < 3; i++) {
cmd.StabilizationSettings[i] = settings.Pos1StabilizationSettings[i]; // See assumptions1
}
cmd.FlightMode = settings.Pos1FlightMode; // See assumptions2
} else if (flightMode > FLIGHT_MODE_LIMIT) {
// Position 3
for(int i = 0; i < 3; i++) {
cmd.StabilizationSettings[i] = settings.Pos3StabilizationSettings[i]; // See assumptions5
}
cmd.FlightMode = settings.Pos3FlightMode; // See assumptions6
} else {
// Position 2
for(int i = 0; i < 3; i++) {
cmd.StabilizationSettings[i] = settings.Pos2StabilizationSettings[i]; // See assumptions3
}
cmd.FlightMode = settings.Pos2FlightMode; // See assumptions4
}
// Update the ManualControlCommand object
ManualControlCommandSet(&cmd);
// This seems silly to set then get, but the reason is if the GCS is
// the control input, the set command will be blocked by the read only
// setting and the get command will pull the right values from telemetry
} else
ManualControlCommandGet(&cmd); /* Under GCS control */
// Implement hysteresis loop on connection status
// Must check both Max and Min in case they reversed
if (!ManualControlCommandReadOnly(&cmd) &&
cmd.Channel[settings.Throttle] < settings.ChannelMax[settings.Throttle] - CONNECTION_OFFSET &&
cmd.Channel[settings.Throttle] < settings.ChannelMin[settings.Throttle] - CONNECTION_OFFSET) {
if (disconnected_count++ > 10) {
connection_state = DISCONNECTED;
connected_count = 0;
disconnected_count = 0;
} else
disconnected_count++;
} else {
if (connected_count++ > 10) {
connection_state = CONNECTED;
connected_count = 0;
disconnected_count = 0;
} else
connected_count++;
}
if (connection_state == DISCONNECTED) {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
cmd.Throttle = -1; // Shut down engine with no control
cmd.Roll = 0;
cmd.Yaw = 0;
cmd.Pitch = 0;
//cmd.FlightMode = MANUALCONTROLCOMMAND_FLIGHTMODE_AUTO; // don't do until AUTO implemented and functioning
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_WARNING);
ManualControlCommandSet(&cmd);
} else {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_TRUE;
AlarmsClear(SYSTEMALARMS_ALARM_MANUALCONTROL);
ManualControlCommandSet(&cmd);
}
// Arming and Disarming mechanism
if (cmd.Throttle < 0) {
// Throttle is low, in this condition the arming state could change
uint8_t newCmdArmed = cmd.Armed;
static portTickType armedDisarmStart;
// Look for state changes and write in newArmState
if (settings.Arming == MANUALCONTROLSETTINGS_ARMING_NONE) {
// No channel assigned to arming -> arm immediately when throttle is low
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_TRUE;
} else {
float armStickLevel;
uint8_t channel = settings.Arming/2; // 0=Channel1, 1=Channel1_Rev, 2=Channel2, ....
bool reverse = (settings.Arming%2)==1;
bool manualArm = false;
bool manualDisarm = false;
if (connection_state == CONNECTED) {
// Should use RC input only if RX is connected
armStickLevel = scaledChannel[channel];
if (reverse)
armStickLevel =-armStickLevel;
if (armStickLevel <= -0.90)
manualArm = true;
else if (armStickLevel >= +0.90)
manualDisarm = true;
}
switch(armState) {
case ARM_STATE_DISARMED:
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_FALSE;
if (manualArm) {
armedDisarmStart = lastSysTime;
armState = ARM_STATE_ARMING_MANUAL;
}
break;
case ARM_STATE_ARMING_MANUAL:
if (manualArm) {
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > ARMED_TIME_MS)
armState = ARM_STATE_ARMED;
}
else
armState = ARM_STATE_DISARMED;
break;
case ARM_STATE_ARMED:
// When we get here, the throttle is low,
// we go immediately to disarming due to timeout, also when the disarming mechanism is not enabled
armedDisarmStart = lastSysTime;
armState = ARM_STATE_DISARMING_TIMEOUT;
newCmdArmed = MANUALCONTROLCOMMAND_ARMED_TRUE;
break;
case ARM_STATE_DISARMING_TIMEOUT:
// We get here when armed while throttle low, even when the arming timeout is not enabled
if (settings.ArmedTimeout != 0)
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > settings.ArmedTimeout)
armState = ARM_STATE_DISARMED;
// Switch to disarming due to manual control when needed
if (manualDisarm) {
armedDisarmStart = lastSysTime;
armState = ARM_STATE_DISARMING_MANUAL;
}
break;
case ARM_STATE_DISARMING_MANUAL:
if (manualDisarm) {
if (timeDifferenceMs(armedDisarmStart, lastSysTime) > ARMED_TIME_MS)
armState = ARM_STATE_DISARMED;
}
else
armState = ARM_STATE_ARMED;
break;
}
}
// Update cmd object when needed
if (newCmdArmed != cmd.Armed) {
cmd.Armed = newCmdArmed;
ManualControlCommandSet(&cmd);
}
} else {
// The throttle is not low, in case we where arming or disarming, abort
switch(armState) {
case ARM_STATE_DISARMING_MANUAL:
case ARM_STATE_DISARMING_TIMEOUT:
armState = ARM_STATE_ARMED;
break;
case ARM_STATE_ARMING_MANUAL:
armState = ARM_STATE_DISARMED;
break;
default:
// Nothing needs to be done in the other states
break;
}
}
// End of arming/disarming
// Depending on the mode update the Stabilization or Actuator objects
if (cmd.FlightMode == MANUALCONTROLCOMMAND_FLIGHTMODE_MANUAL) {
actuator.Roll = cmd.Roll;
actuator.Pitch = cmd.Pitch;
actuator.Yaw = cmd.Yaw;
actuator.Throttle = cmd.Throttle;
ActuatorDesiredSet(&actuator);
} else if (cmd.FlightMode == MANUALCONTROLCOMMAND_FLIGHTMODE_STABILIZED) {
attitude.Roll = cmd.Roll * stabSettings.RollMax;
attitude.Pitch = cmd.Pitch * stabSettings.PitchMax;
attitude.Yaw = fmod(cmd.Yaw * 180.0, 360);
attitude.Throttle = (cmd.Throttle < 0) ? -1 : cmd.Throttle;
rate.Roll = cmd.Roll * stabSettings.ManualRate[STABILIZATIONSETTINGS_MANUALRATE_ROLL];
rate.Pitch = cmd.Pitch * stabSettings.ManualRate[STABILIZATIONSETTINGS_MANUALRATE_PITCH];
rate.Yaw = cmd.Yaw * stabSettings.ManualRate[STABILIZATIONSETTINGS_MANUALRATE_YAW];
AttitudeDesiredSet(&attitude);
RateDesiredSet(&rate);
}
}
}
/**
* @brief Process inputs and arming
*
* This will always process the arming signals as for now the transmitter
* is always in charge. When a transmitter is not detected control will
* fall back to the failsafe module. If the flight mode is in tablet
* control position then control will be ceeded to that module.
*/
int32_t transmitter_control_update()
{
lastSysTime = PIOS_Thread_Systime();
float scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_NUMELEM];
bool validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_NUMELEM];
if (settings_updated) {
settings_updated = false;
ManualControlSettingsGet(&settings);
}
/* Update channel activity monitor */
uint8_t arm_status;
FlightStatusArmedGet(&arm_status);
if (arm_status == FLIGHTSTATUS_ARMED_DISARMED) {
if (updateRcvrActivity(&activity_fsm)) {
/* Reset the aging timer because activity was detected */
lastActivityTime = lastSysTime;
}
}
if (timeDifferenceMs(lastActivityTime, lastSysTime) > 5000) {
resetRcvrActivity(&activity_fsm);
lastActivityTime = lastSysTime;
}
if (ManualControlCommandReadOnly()) {
FlightTelemetryStatsData flightTelemStats;
FlightTelemetryStatsGet(&flightTelemStats);
if(flightTelemStats.Status != FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
/* trying to fly via GCS and lost connection. fall back to transmitter */
UAVObjMetadata metadata;
ManualControlCommandGetMetadata(&metadata);
UAVObjSetAccess(&metadata, ACCESS_READWRITE);
ManualControlCommandSetMetadata(&metadata);
}
// Don't process anything else when GCS is overriding the objects
return 0;
}
if (settings.RssiType != MANUALCONTROLSETTINGS_RSSITYPE_NONE) {
int32_t value = 0;
extern uintptr_t pios_rcvr_group_map[];
switch (settings.RssiType) {
case MANUALCONTROLSETTINGS_RSSITYPE_PWM:
value = PIOS_RCVR_Read(pios_rcvr_group_map[MANUALCONTROLSETTINGS_CHANNELGROUPS_PWM], settings.RssiChannelNumber);
break;
case MANUALCONTROLSETTINGS_RSSITYPE_PPM:
value = PIOS_RCVR_Read(pios_rcvr_group_map[MANUALCONTROLSETTINGS_CHANNELGROUPS_PPM], settings.RssiChannelNumber);
break;
case MANUALCONTROLSETTINGS_RSSITYPE_ADC:
#if defined(PIOS_INCLUDE_ADC)
value = PIOS_ADC_GetChannelRaw(settings.RssiChannelNumber);
#endif
break;
case MANUALCONTROLSETTINGS_RSSITYPE_OPENLRS:
#if defined(PIOS_INCLUDE_OPENLRS_RCVR)
value = PIOS_OpenLRS_RSSI_Get();
#endif /* PIOS_INCLUDE_OPENLRS_RCVR */
break;
case MANUALCONTROLSETTINGS_RSSITYPE_FRSKYPWM:
#if defined(PIOS_INCLUDE_FRSKY_RSSI)
value = PIOS_FrSkyRssi_Get();
#endif /* PIOS_INCLUDE_FRSKY_RSSI */
break;
case MANUALCONTROLSETTINGS_RSSITYPE_SBUS:
#if defined(PIOS_INCLUDE_SBUS)
value = PIOS_RCVR_Read(pios_rcvr_group_map[MANUALCONTROLSETTINGS_CHANNELGROUPS_SBUS], settings.RssiChannelNumber);
#endif /* PIOS_INCLUDE_SBUS */
break;
}
if(value < 0)
value = 0;
if (settings.RssiMax == settings.RssiMin)
cmd.Rssi = 0;
else
cmd.Rssi = ((float)(value - settings.RssiMin)/((float)settings.RssiMax-settings.RssiMin)) * 100;
cmd.RawRssi = value;
}
bool valid_input_detected = true;
// Read channel values in us
for (uint8_t n = 0;
n < MANUALCONTROLSETTINGS_CHANNELGROUPS_NUMELEM && n < MANUALCONTROLCOMMAND_CHANNEL_NUMELEM;
++n) {
extern uintptr_t pios_rcvr_group_map[];
if (settings.ChannelGroups[n] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE) {
cmd.Channel[n] = PIOS_RCVR_INVALID;
validChannel[n] = false;
} else {
cmd.Channel[n] = PIOS_RCVR_Read(pios_rcvr_group_map[settings.ChannelGroups[n]],
settings.ChannelNumber[n]);
}
// If a channel has timed out this is not valid data and we shouldn't update anything
// until we decide to go to failsafe
if(cmd.Channel[n] == (uint16_t) PIOS_RCVR_TIMEOUT) {
valid_input_detected = false;
validChannel[n] = false;
} else {
scaledChannel[n] = scaleChannel(n, cmd.Channel[n]);
validChannel[n] = validInputRange(n, cmd.Channel[n], CONNECTION_OFFSET);
}
}
// Check settings, if error raise alarm
if (settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_ROLL] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE ||
settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_PITCH] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE ||
settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_YAW] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE ||
settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_THROTTLE] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE ||
// Check all channel mappings are valid
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ROLL] == (uint16_t) PIOS_RCVR_INVALID ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_PITCH] == (uint16_t) PIOS_RCVR_INVALID ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_YAW] == (uint16_t) PIOS_RCVR_INVALID ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_THROTTLE] == (uint16_t) PIOS_RCVR_INVALID ||
// Check the driver exists
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ROLL] == (uint16_t) PIOS_RCVR_NODRIVER ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_PITCH] == (uint16_t) PIOS_RCVR_NODRIVER ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_YAW] == (uint16_t) PIOS_RCVR_NODRIVER ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_THROTTLE] == (uint16_t) PIOS_RCVR_NODRIVER ||
// Check the FlightModeNumber is valid
settings.FlightModeNumber < 1 || settings.FlightModeNumber > MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_NUMELEM ||
// If we've got more than one possible valid FlightMode, we require a configured FlightMode channel
((settings.FlightModeNumber > 1) && (settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE)) ||
// Whenever FlightMode channel is configured, it needs to be valid regardless of FlightModeNumber settings
((settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE] < MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE) && (
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE] == (uint16_t) PIOS_RCVR_INVALID ||
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE] == (uint16_t) PIOS_RCVR_NODRIVER ))) {
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_SETTINGS);
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
ManualControlCommandSet(&cmd);
// Need to do this here since we don't process armed status. Since this shouldn't happen in flight (changed config)
// immediately disarm
pending_control_event = CONTROL_EVENTS_DISARM;
return -1;
}
// the block above validates the input configuration. this simply checks that the range is valid if flight mode is configured.
bool flightmode_valid_input = settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE] >= MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE ||
validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE];
// because arming is optional we must determine if it is needed before checking it is valid
bool arming_valid_input = (settings.Arming < MANUALCONTROLSETTINGS_ARMING_SWITCH) ||
validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ARMING];
// decide if we have valid manual input or not
valid_input_detected &= validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_THROTTLE] &&
validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ROLL] &&
validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_YAW] &&
validChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_PITCH] &&
flightmode_valid_input &&
arming_valid_input;
// Implement hysteresis loop on connection status
if (valid_input_detected && (++connected_count > 10)) {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_TRUE;
connected_count = 0;
disconnected_count = 0;
} else if (!valid_input_detected && (++disconnected_count > 10)) {
cmd.Connected = MANUALCONTROLCOMMAND_CONNECTED_FALSE;
connected_count = 0;
disconnected_count = 0;
}
if (cmd.Connected == MANUALCONTROLCOMMAND_CONNECTED_FALSE) {
// These values are not used but just put ManualControlCommand in a sane state. When
// Connected is false, then the failsafe submodule will be in control.
cmd.Throttle = -1;
cmd.Roll = 0;
cmd.Yaw = 0;
cmd.Pitch = 0;
cmd.Collective = 0;
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_NORX);
} else if (valid_input_detected) {
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_NONE);
// Scale channels to -1 -> +1 range
cmd.Roll = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ROLL];
cmd.Pitch = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_PITCH];
cmd.Yaw = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_YAW];
cmd.Throttle = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_THROTTLE];
cmd.ArmSwitch = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ARMING] > 0 ?
MANUALCONTROLCOMMAND_ARMSWITCH_ARMED : MANUALCONTROLCOMMAND_ARMSWITCH_DISARMED;
flight_mode_value = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_FLIGHTMODE];
// Apply deadband for Roll/Pitch/Yaw stick inputs
if (settings.Deadband) {
applyDeadband(&cmd.Roll, settings.Deadband);
applyDeadband(&cmd.Pitch, settings.Deadband);
applyDeadband(&cmd.Yaw, settings.Deadband);
}
if(cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_COLLECTIVE] != (uint16_t) PIOS_RCVR_INVALID &&
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_COLLECTIVE] != (uint16_t) PIOS_RCVR_NODRIVER &&
cmd.Channel[MANUALCONTROLSETTINGS_CHANNELGROUPS_COLLECTIVE] != (uint16_t) PIOS_RCVR_TIMEOUT) {
cmd.Collective = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_COLLECTIVE];
}
AccessoryDesiredData accessory;
// Set Accessory 0
if (settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY0] !=
MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE) {
accessory.AccessoryVal = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY0];
if(AccessoryDesiredInstSet(0, &accessory) != 0) //These are allocated later and that allocation might fail
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_ACCESSORY);
}
// Set Accessory 1
if (settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY1] !=
MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE) {
accessory.AccessoryVal = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY1];
if(AccessoryDesiredInstSet(1, &accessory) != 0) //These are allocated later and that allocation might fail
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_ACCESSORY);
}
// Set Accessory 2
if (settings.ChannelGroups[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY2] !=
MANUALCONTROLSETTINGS_CHANNELGROUPS_NONE) {
accessory.AccessoryVal = scaledChannel[MANUALCONTROLSETTINGS_CHANNELGROUPS_ACCESSORY2];
if(AccessoryDesiredInstSet(2, &accessory) != 0) //These are allocated later and that allocation might fail
set_manual_control_error(SYSTEMALARMS_MANUALCONTROL_ACCESSORY);
}
}
// Process arming outside conditional so system will disarm when disconnected. Notice this
// is processed in the _update method instead of _select method so the state system is always
// evalulated, even if not detected.
process_transmitter_events(&cmd, &settings, valid_input_detected);
// Update cmd object
ManualControlCommandSet(&cmd);
return 0;
}
/**
* Update telemetry statistics and handle connection handshake
*/
static void updateTelemetryStats()
{
UAVTalkStats utalkStats;
FlightTelemetryStatsData flightStats;
GCSTelemetryStatsData gcsStats;
uint8_t forceUpdate;
uint8_t connectionTimeout;
uint32_t timeNow;
// Get stats
UAVTalkGetStats(&utalkStats);
UAVTalkResetStats();
// Get object data
FlightTelemetryStatsGet(&flightStats);
GCSTelemetryStatsGet(&gcsStats);
// Update stats object
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
flightStats.RxDataRate = (float)utalkStats.rxBytes / ((float)STATS_UPDATE_PERIOD_MS / 1000.0);
flightStats.TxDataRate = (float)utalkStats.txBytes / ((float)STATS_UPDATE_PERIOD_MS / 1000.0);
flightStats.RxFailures += utalkStats.rxErrors;
flightStats.TxFailures += txErrors;
flightStats.TxRetries += txRetries;
txErrors = 0;
txRetries = 0;
} else {
flightStats.RxDataRate = 0;
flightStats.TxDataRate = 0;
flightStats.RxFailures = 0;
flightStats.TxFailures = 0;
flightStats.TxRetries = 0;
txErrors = 0;
txRetries = 0;
}
// Check for connection timeout
timeNow = xTaskGetTickCount() * portTICK_RATE_MS;
if (utalkStats.rxObjects > 0) {
timeOfLastObjectUpdate = timeNow;
}
if ((timeNow - timeOfLastObjectUpdate) > CONNECTION_TIMEOUT_MS) {
connectionTimeout = 1;
} else {
connectionTimeout = 0;
}
// Update connection state
forceUpdate = 1;
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED) {
// Wait for connection request
if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_HANDSHAKEREQ) {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_HANDSHAKEACK;
}
} else if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_HANDSHAKEACK) {
// Wait for connection
if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_CONNECTED) {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
} else if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_DISCONNECTED) {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
}
} else if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
if (gcsStats.Status != GCSTELEMETRYSTATS_STATUS_CONNECTED || connectionTimeout) {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
} else {
forceUpdate = 0;
}
} else {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
}
// Update the telemetry alarm
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
AlarmsClear(SYSTEMALARMS_ALARM_TELEMETRY);
} else {
AlarmsSet(SYSTEMALARMS_ALARM_TELEMETRY, SYSTEMALARMS_ALARM_ERROR);
}
// Update object
FlightTelemetryStatsSet(&flightStats);
// Force telemetry update if not connected
if (forceUpdate) {
FlightTelemetryStatsUpdated();
}
}
/**
* Processes queue events
*/
static void processObjEvent(UAVObjEvent * ev)
{
UAVObjMetadata metadata;
// FlightTelemetryStatsData flightStats;
// GCSTelemetryStatsData gcsTelemetryStatsData;
// int32_t retries;
// int32_t success;
if (ev->obj == 0) {
updateTelemetryStats();
} else if (ev->obj == GCSTelemetryStatsHandle()) {
gcsTelemetryStatsUpdated();
} else if (ev->obj == TelemetrySettingsHandle()) {
updateSettings();
} else {
// Get object metadata
UAVObjGetMetadata(ev->obj, &metadata);
// If this is a metaobject then make necessary telemetry updates
if (UAVObjIsMetaobject(ev->obj)) {
updateObject(UAVObjGetLinkedObj(ev->obj)); // linked object will be the actual object the metadata are for
}
mavlink_message_t msg;
mavlink_system.sysid = 20;
mavlink_system.compid = MAV_COMP_ID_IMU;
mavlink_system.type = MAV_TYPE_FIXED_WING;
uint8_t mavClass = MAV_AUTOPILOT_OPENPILOT;
AlarmsClear(SYSTEMALARMS_ALARM_TELEMETRY);
// Setup type and object id fields
uint32_t objId = UAVObjGetID(ev->obj);
// uint64_t timeStamp = 0;
switch(objId) {
case BAROALTITUDE_OBJID:
{
BaroAltitudeGet(&baroAltitude);
pressure.press_abs = baroAltitude.Pressure*10.0f;
pressure.temperature = baroAltitude.Temperature*100.0f;
mavlink_msg_scaled_pressure_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &pressure);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
break;
}
case FLIGHTTELEMETRYSTATS_OBJID:
{
// FlightTelemetryStatsData flightTelemetryStats;
FlightTelemetryStatsGet(&flightStats);
// XXX this is a hack to make it think it got a confirmed
// connection
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
GCSTelemetryStatsGet(&gcsTelemetryStatsData);
gcsTelemetryStatsData.Status = GCSTELEMETRYSTATS_STATUS_CONNECTED;
//
//
// //mavlink_msg_heartbeat_send(MAVLINK_COMM_0,mavlink_system.type,mavClass);
// mavlink_msg_heartbeat_pack(mavlink_system.sysid, mavlink_system.compid, &msg, mavlink_system.type, mavClass);
// // Copy the message to the send buffer
// uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// // Send buffer
// PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
break;
}
case SYSTEMSTATS_OBJID:
{
FlightStatusData flightStatus;
FlightStatusGet(&flightStatus);
uint8_t system_state = MAV_STATE_UNINIT;
uint8_t base_mode = 0;
uint8_t custom_mode = 0;
// Set flight mode
switch (flightStatus.FlightMode)
{
case FLIGHTSTATUS_FLIGHTMODE_MANUAL:
base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
break;
case FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD:
base_mode |= MAV_MODE_FLAG_GUIDED_ENABLED;
break;
case FLIGHTSTATUS_FLIGHTMODE_STABILIZED1:
base_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED;
break;
case FLIGHTSTATUS_FLIGHTMODE_STABILIZED2:
base_mode |= MAV_MODE_FLAG_GUIDED_ENABLED;
break;
case FLIGHTSTATUS_FLIGHTMODE_STABILIZED3:
base_mode |= MAV_MODE_FLAG_AUTO_ENABLED;
break;
case FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL:
base_mode |= MAV_MODE_FLAG_GUIDED_ENABLED;
break;
default:
base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
break;
}
// Set arming state
switch (flightStatus.Armed)
{
case FLIGHTSTATUS_ARMED_ARMING:
case FLIGHTSTATUS_ARMED_ARMED:
system_state = MAV_STATE_ACTIVE;
base_mode |= MAV_MODE_FLAG_SAFETY_ARMED;
break;
case FLIGHTSTATUS_ARMED_DISARMED:
system_state = MAV_STATE_STANDBY;
base_mode &= !MAV_MODE_FLAG_SAFETY_ARMED;
break;
}
// Set HIL
if (hilEnabled) base_mode |= MAV_MODE_FLAG_HIL_ENABLED;
mavlink_msg_heartbeat_send(MAVLINK_COMM_0, mavlink_system.type, mavClass, base_mode, custom_mode, system_state);
SystemStatsData stats;
SystemStatsGet(&stats);
FlightBatteryStateData flightBatteryData;
FlightBatteryStateGet(&flightBatteryData);
FlightBatterySettingsData flightBatterySettings;
FlightBatterySettingsGet(&flightBatterySettings);
uint16_t batteryVoltage = (uint16_t)(flightBatteryData.Voltage*1000.0f);
int16_t batteryCurrent = -1; // -1: Not present / not estimated
int8_t batteryPercent = -1; // -1: Not present / not estimated
// if (flightBatterySettings.SensorCalibrations[FLIGHTBATTERYSETTINGS_SENSORCALIBRATIONS_CURRENTFACTOR] == 0)
// {
// Factor is zero, sensor is not present
// Estimate remaining capacity based on lipo curve
batteryPercent = 100.0f*((flightBatteryData.Voltage - 9.6f)/(12.6f - 9.6f));
// }
// else
// {
// // Use capacity and current
// batteryPercent = 100.0f*((flightBatterySettings.Capacity - flightBatteryData.ConsumedEnergy) / flightBatterySettings.Capacity);
// batteryCurrent = flightBatteryData.Current*100;
// }
mavlink_msg_sys_status_send(MAVLINK_COMM_0, 0xFF, 0xFF, 0xFF, ((uint16_t)stats.CPULoad*10), batteryVoltage, batteryCurrent, batteryPercent, 0, 0, 0, 0, 0, 0);
// // Copy the message to the send buffer
// uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// // Send buffer
// PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
break;
}
case ATTITUDERAW_OBJID:
{
AttitudeRawGet(&attitudeRaw);
// Copy data
attitude_raw.xacc = attitudeRaw.accels[ATTITUDERAW_ACCELS_X];
attitude_raw.yacc = attitudeRaw.accels[ATTITUDERAW_ACCELS_Y];
attitude_raw.zacc = attitudeRaw.accels[ATTITUDERAW_ACCELS_Z];
attitude_raw.xgyro = attitudeRaw.gyros[ATTITUDERAW_GYROS_X];
attitude_raw.ygyro = attitudeRaw.gyros[ATTITUDERAW_GYROS_Y];
attitude_raw.zgyro = attitudeRaw.gyros[ATTITUDERAW_GYROS_Z];
attitude_raw.xmag = attitudeRaw.magnetometers[ATTITUDERAW_MAGNETOMETERS_X];
attitude_raw.ymag = attitudeRaw.magnetometers[ATTITUDERAW_MAGNETOMETERS_Y];
attitude_raw.zmag = attitudeRaw.magnetometers[ATTITUDERAW_MAGNETOMETERS_Z];
mavlink_msg_raw_imu_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &attitude_raw);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
if (hilEnabled)
{
mavlink_hil_controls_t controls;
// Copy data
controls.roll_ailerons = 0.1;
controls.pitch_elevator = 0.1;
controls.yaw_rudder = 0.0;
controls.throttle = 0.8;
mavlink_msg_hil_controls_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &controls);
// Copy the message to the send buffer
len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
}
break;
}
case ATTITUDEMATRIX_OBJID:
{
AttitudeMatrixGet(&attitudeMatrix);
// Copy data
attitude.roll = attitudeMatrix.Roll;
attitude.pitch = attitudeMatrix.Pitch;
attitude.yaw = attitudeMatrix.Yaw;
attitude.rollspeed = attitudeMatrix.AngularRates[0];
attitude.pitchspeed = attitudeMatrix.AngularRates[1];
attitude.yawspeed = attitudeMatrix.AngularRates[2];
mavlink_msg_attitude_encode(mavlink_system.sysid,
mavlink_system.compid, &msg, &attitude);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
break;
}
case GPSPOSITION_OBJID:
{
GPSPositionGet(&gpsPosition);
gps_raw.time_usec = 0;
gps_raw.lat = gpsPosition.Latitude*10;
gps_raw.lon = gpsPosition.Longitude*10;
gps_raw.alt = gpsPosition.Altitude*10;
gps_raw.eph = gpsPosition.HDOP*100;
gps_raw.epv = gpsPosition.VDOP*100;
gps_raw.cog = gpsPosition.Heading*100;
gps_raw.satellites_visible = gpsPosition.Satellites;
gps_raw.fix_type = gpsPosition.Status;
mavlink_msg_gps_raw_int_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &gps_raw);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
// mavlink_msg_gps_raw_int_send(MAVLINK_COMM_0, gps_raw.usec, gps_raw.lat, gps_raw.lon, gps_raw.alt, gps_raw.eph, gps_raw.epv, gps_raw.hdg, gps_raw.satellites_visible, gps_raw.fix_type, 0);
break;
}
case POSITIONACTUAL_OBJID:
{
PositionActualData pos;
PositionActualGet(&pos);
mavlink_local_position_ned_t m_pos;
m_pos.time_boot_ms = 0;
m_pos.x = pos.North;
m_pos.y = pos.East;
m_pos.z = pos.Down;
m_pos.vx = 0.0f;
m_pos.vy = 0.0f;
m_pos.vz = 0.0f;
mavlink_msg_local_position_ned_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &m_pos);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(telemetryPort, mavlinkTxBuf, len);
}
break;
case ACTUATORCOMMAND_OBJID:
{
mavlink_rc_channels_scaled_t rc;
float val;
ManualControlCommandRollGet(&val);
rc.chan1_scaled = val*1000;
ManualControlCommandPitchGet(&val);
rc.chan2_scaled = val*1000;
ManualControlCommandYawGet(&val);
rc.chan3_scaled = val*1000;
ManualControlCommandThrottleGet(&val);
rc.chan4_scaled = val*1000;
ActuatorCommandData act;
ActuatorCommandGet(&act);
rc.chan5_scaled = act.Channel[0];
rc.chan6_scaled = act.Channel[1];
rc.chan7_scaled = act.Channel[2];
rc.chan8_scaled = act.Channel[3];
ManualControlCommandData cmd;
ManualControlCommandGet(&cmd);
rc.rssi = ((uint8_t)(cmd.Connected == MANUALCONTROLCOMMAND_CONNECTED_TRUE))*255;
rc.port = 0;
mavlink_msg_rc_channels_scaled_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &rc);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(PIOS_COM_TELEM_RF, mavlinkTxBuf, len);
break;
}
case MANUALCONTROLCOMMAND_OBJID:
{
mavlink_rc_channels_scaled_t rc;
float val;
ManualControlCommandRollGet(&val);
rc.chan1_scaled = val*1000;
ManualControlCommandPitchGet(&val);
rc.chan2_scaled = val*1000;
ManualControlCommandYawGet(&val);
rc.chan3_scaled = val*1000;
ManualControlCommandThrottleGet(&val);
rc.chan4_scaled = val*1000;
rc.chan5_scaled = 0;
rc.chan6_scaled = 0;
rc.chan7_scaled = 0;
rc.chan8_scaled = 0;
ManualControlCommandData cmd;
ManualControlCommandGet(&cmd);
rc.rssi = ((uint8_t)(cmd.Connected == MANUALCONTROLCOMMAND_CONNECTED_TRUE))*255;
rc.port = 0;
mavlink_msg_rc_channels_scaled_encode(mavlink_system.sysid, mavlink_system.compid, &msg, &rc);
// Copy the message to the send buffer
uint16_t len = mavlink_msg_to_send_buffer(mavlinkTxBuf, &msg);
// Send buffer
PIOS_COM_SendBufferNonBlocking(PIOS_COM_TELEM_RF, mavlinkTxBuf, len);
break;
}
default:
{
//printf("unknown object: %x\n",(unsigned int)objId);
break;
}
}
}
}
/**
* Update telemetry statistics and handle connection handshake
*/
static void updateTelemetryStats()
{
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
// gcsStats.Status = GCSTELEMETRYSTATS_STATUS_CONNECTED;
FlightTelemetryStatsData flightStats;
GCSTelemetryStatsData gcsStats;
uint8_t forceUpdate;
uint8_t connectionTimeout;
uint32_t timeNow;
// Get object data
FlightTelemetryStatsGet(&flightStats);
GCSTelemetryStatsGet(&gcsStats);
// Update stats object
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
//flightStats.RxDataRate = (float)utalkStats.rxBytes / ((float)STATS_UPDATE_PERIOD_MS / 1000.0);
//flightStats.TxDataRate = (float)utalkStats.txBytes / ((float)STATS_UPDATE_PERIOD_MS / 1000.0);
//flightStats.RxFailures += utalkStats.rxErrors;
flightStats.TxFailures += txErrors;
flightStats.TxRetries += txRetries;
txErrors = 0;
txRetries = 0;
} else {
flightStats.RxDataRate = 0;
flightStats.TxDataRate = 0;
flightStats.RxFailures = 0;
flightStats.TxFailures = 0;
flightStats.TxRetries = 0;
txErrors = 0;
txRetries = 0;
}
// Check for connection timeout
timeNow = xTaskGetTickCount() * portTICK_RATE_MS;
if ((timeNow - lastOperatorHeartbeat) > CONNECTION_TIMEOUT_MS) {
connectionTimeout = 1;
} else {
connectionTimeout = 0;
}
// Update connection state
forceUpdate = 1;
// FIXME Hardcode value for now
// connectionTimeout = 0;
// If the GCS heartbeat has been received in the last five seconds
// set as connected
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED) {
if (connectionTimeout == 0) {
// Switching from disconnected to connected
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
gcsStats.Status = GCSTELEMETRYSTATS_STATUS_CONNECTED;
} else {
// Not switching, no update needed
forceUpdate = 0;
}
} else {
// We were connected, checking if we're still connected
if (connectionTimeout == 1) {
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
gcsStats.Status = GCSTELEMETRYSTATS_STATUS_DISCONNECTED;
} else {
// We were connected and still are, no update needed
forceUpdate = 0;
}
}
// FIXME HARDCODED VALUES
flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
gcsStats.Status = GCSTELEMETRYSTATS_STATUS_CONNECTED;
forceUpdate = 1;
// if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED) {
// // Wait for connection request
// if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_HANDSHAKEREQ) {
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_HANDSHAKEACK;
// }
// } else if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_HANDSHAKEACK) {
// // Wait for connection
// if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_CONNECTED) {
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_CONNECTED;
// } else if (gcsStats.Status == GCSTELEMETRYSTATS_STATUS_DISCONNECTED) {
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
// }
// } else if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
// if (gcsStats.Status != GCSTELEMETRYSTATS_STATUS_CONNECTED || connectionTimeout) {
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
// } else {
// forceUpdate = 0;
// }
// } else {
// flightStats.Status = FLIGHTTELEMETRYSTATS_STATUS_DISCONNECTED;
// }
// Update the telemetry alarm
if (flightStats.Status == FLIGHTTELEMETRYSTATS_STATUS_CONNECTED) {
AlarmsClear(SYSTEMALARMS_ALARM_TELEMETRY);
} else {
AlarmsSet(SYSTEMALARMS_ALARM_TELEMETRY, SYSTEMALARMS_ALARM_ERROR);
}
// Update object
FlightTelemetryStatsSet(&flightStats);
// Force telemetry update if not connected
if (forceUpdate) {
FlightTelemetryStatsUpdated();
}
}