コード例 #1
0
ファイル: main.c プロジェクト: Maelok/esc32
void main(void) {
    rccInit();
    timerInit();
    configInit();
    adcInit();
    fetInit();
    serialInit();
    runInit();
    cliInit();
    owInit();

    runDisarm(REASON_STARTUP);
    inputMode = ESC_INPUT_PWM;

    fetSetDutyCycle(0);
    fetBeep(200, 100);
    fetBeep(300, 100);
    fetBeep(400, 100);
    fetBeep(500, 100);
    fetBeep(400, 100);
    fetBeep(300, 100);
    fetBeep(200, 100);

    pwmInit();

    statusLed = digitalInit(GPIO_STATUS_LED_PORT, GPIO_STATUS_LED_PIN);
    digitalHi(statusLed);
    errorLed = digitalInit(GPIO_ERROR_LED_PORT, GPIO_ERROR_LED_PIN);
    digitalHi(errorLed);
#ifdef ESC_DEBUG
    tp = digitalInit(GPIO_TP_PORT, GPIO_TP_PIN);
    digitalLo(tp);
#endif

    // self calibrating idle timer loop
    {
        volatile unsigned long cycles;
        volatile unsigned int *DWT_CYCCNT = (int *)0xE0001004;
        volatile unsigned int *DWT_CONTROL = (int *)0xE0001000;
        volatile unsigned int *SCB_DEMCR = (int *)0xE000EDFC;

        *SCB_DEMCR = *SCB_DEMCR | 0x01000000;
        *DWT_CONTROL = *DWT_CONTROL | 1;	// enable the counter

	minCycles = 0xffff;
        while (1) {
            idleCounter++;

	    NOPS_4;

            cycles = *DWT_CYCCNT;
            *DWT_CYCCNT = 0;		    // reset the counter

            // record shortest number of instructions for loop
	    totalCycles += cycles;
            if (cycles < minCycles)
                minCycles = cycles;
        }
    }
}
コード例 #2
0
void supervisorLEDsOn(void) {
#ifdef SUPERVISOR_DEBUG_PORT
    digitalHi(supervisorData.debugLed);
#endif
    digitalHi(supervisorData.readyLed);
    digitalHi(supervisorData.gpsLed);
}
コード例 #3
0
ファイル: signal.c プロジェクト: ARMAZILA/FlightCode
void signalLED(LEDNUM_t led_num, LEDMODE_t led_mode)
{
	switch (led_mode)
	{

	case LEDMODE_OFF:
		digitalLo(gpio_cfg[led_num].gpio, gpio_cfg[led_num].pin);
		break;

	case LEDMODE_ON:
		digitalHi(gpio_cfg[led_num].gpio, gpio_cfg[led_num].pin);
		break;

	case LEDMODE_TOGGLE:
		digitalToggle(gpio_cfg[led_num].gpio, gpio_cfg[led_num].pin);
		break;

	case LEDMODE_BLINK1:
		digitalHi(gpio_cfg[led_num].gpio, gpio_cfg[led_num].pin);
		xTimerChangePeriod(LedTimer[led_num], 500, 10);
		break;

	case LEDMODE_BLINK2:

		break;
	}
}
コード例 #4
0
ファイル: drv_spi.c プロジェクト: kh4/openLRSngRX32_test
void selectRFM(uint8_t which)
{
  digitalHi(GPIOB,GPIO_Pin_12);
  digitalHi(GPIOC,GPIO_Pin_15);

  switch (which) {
  case 1: digitalLo(GPIOB,GPIO_Pin_12);
    break;
  case 2: digitalLo(GPIOC,GPIO_Pin_15);
    break;
  default:
    break;
  }
}
コード例 #5
0
static void i2cUnstick(void)
{
    GPIO_TypeDef *gpio;
    gpio_config_t cfg;
    uint16_t scl, sda;
    int i;

    // prepare pins
    gpio = i2cHardwareMap[I2Cx_index].gpio;
    scl = i2cHardwareMap[I2Cx_index].scl;
    sda = i2cHardwareMap[I2Cx_index].sda;

    digitalHi(gpio, scl | sda);

    cfg.pin = scl | sda;
    cfg.speed = Speed_2MHz;
    cfg.mode = Mode_Out_OD;
    gpioInit(gpio, &cfg);

    for (i = 0; i < 8; i++) {
        // Wait for any clock stretching to finish
        while (!digitalIn(gpio, scl))
            delayMicroseconds(10);

        // Pull low
        digitalLo(gpio, scl); // Set bus low
        delayMicroseconds(10);
        // Release high again
        digitalHi(gpio, scl); // Set bus high
        delayMicroseconds(10);
    }

    // Generate a start then stop condition
    // SCL  PB10
    // SDA  PB11
    digitalLo(gpio, sda); // Set bus data low
    delayMicroseconds(10);
    digitalLo(gpio, scl); // Set bus scl low
    delayMicroseconds(10);
    digitalHi(gpio, scl); // Set bus scl high
    delayMicroseconds(10);
    digitalHi(gpio, sda); // Set bus sda high

    // Init pins
    cfg.pin = scl | sda;
    cfg.speed = Speed_2MHz;
    cfg.mode = Mode_AF_OD;
    gpioInit(gpio, &cfg);
}
コード例 #6
0
ファイル: bus_spi.c プロジェクト: nico-dh/cleanflight
void spiSelect(bool select)
{
    if (select) {
        digitalLo(GPIOB, Pin_12);
    } else {
        digitalHi(GPIOB, Pin_12);
    }
}
コード例 #7
0
static void beepRev5(bool onoff)
{
    if (onoff) {
        digitalHi(BEEP_GPIO, BEEP_PIN);
    } else {
        digitalLo(BEEP_GPIO, BEEP_PIN);
    }
}
コード例 #8
0
ファイル: digital.c プロジェクト: benzeng/AutoQuad
void digitalTogg(digitalPin *p) {
    if (digitalGet(p)) {
	digitalLo(p);
    }
    else {
	digitalHi(p);
    }
}
コード例 #9
0
void setTxSignal(escSerial_t *escSerial, uint8_t state)
{
    if (state) {
        digitalHi(escSerial->rxTimerHardware->gpio, escSerial->rxTimerHardware->pin);
    } else {
        digitalLo(escSerial->rxTimerHardware->gpio, escSerial->rxTimerHardware->pin);
    }
}
コード例 #10
0
void setTxSignal(softSerial_t *softSerial, uint8_t state)
{
    if ((state == 1 && softSerial->isInverted == false) || (state == 0 && softSerial->isInverted == true)) {
        digitalHi(softSerial->txTimerHardware->gpio, softSerial->txTimerHardware->pin);
    } else {
        digitalLo(softSerial->txTimerHardware->gpio, softSerial->txTimerHardware->pin);
    }
}
コード例 #11
0
ファイル: adc.c プロジェクト: tenyan/quadfork
// every ~15.25us
void ADC_DMA_HANDLER(void) {
    register uint32_t flag = ADC_DMA_ISR;
    register unsigned long *s, *a;
    register uint16_t *w;
    int i;

    // clear intr flags
    ADC_DMA_CR = (uint32_t)ADC_DMA_FLAGS;

    // second half?
    w = ((flag & ADC_DMA_TC_FLAG) == RESET) ? adcDMAData.adc123Raw1 : adcDMAData.adc123Raw2;

    // accumulate totals
    s = adcData.interrupt123Sums;
    *s++ += (w[36] + w[39] + w[42] + w[45]);	// rateX
    *s++ += (w[1]  + w[4]  + w[7]  + w[10]);	// rateY
    *s++ += (w[2]  + w[5]  + w[8]  + w[11]);	// rateZ
    *s++ += (w[0]  + w[3]  + w[6]  + w[9]);	// magX
    *s++ += (w[12] + w[15] + w[18] + w[21]);	// magY
    *s++ += (w[24] + w[27] + w[30] + w[33]);	// magZ
    *s++ += (w[14]);				// temp1
    *s++ += (w[32]);				// Vin
    *s++ += (w[13] + w[16] + w[19] + w[22]);	// accX
    *s++ += (w[25] + w[28] + w[31] + w[34]);	// accY
    *s++ += (w[37] + w[40] + w[43] + w[46]);	// accZ
    *s++ += (w[20] + w[23] + w[26] + w[29]);	// press1
    *s++ += (w[38] + w[41] + w[44] + w[47]);	// press2
    *s++ += (w[17]);				// temp2
    *s   += (w[35]);				// temp3

    if (++adcData.sample == ADC_SAMPLES) {
        register unsigned long micros = timerMicros();
        adcData.sample = 0;

        if (++adcData.loops & 0x01) {
            if (ADC_MAG_SIGN) {
                digitalLo(adcData.magSetReset);
            } else {
                digitalHi(adcData.magSetReset);
            }
        }

        s = adcData.interrupt123Sums;
        a = (unsigned long *)adcData.adcSums;
        for (i = 0; i < ADC_SENSORS; i++) {
            *a++ = *s;
            *s++ = 0;
        }

        adcData.sampleTime = micros - adcData.lastSample;
        adcData.lastSample = micros;

        CoEnterISR();
        isr_SetFlag(adcData.adcFlag);
        CoExitISR();
    }
}
コード例 #12
0
ファイル: run.c プロジェクト: Maelok/esc32
void runDisarm(int reason) {
    fetSetDutyCycle(0);
    timerCancelAlarm2();
    state = ESC_STATE_DISARMED;
    pwmIsrAllOn();
    digitalHi(statusLed);   // turn off
    digitalLo(errorLed);    // turn on
    disarmReason = reason;
}
コード例 #13
0
ファイル: system.c プロジェクト: MuesliReep/cleanflight
void systemInit(void)
{
#ifdef CC3D
    /* Accounts for OP Bootloader, set the Vector Table base address as specified in .ld file */
    extern void *isr_vector_table_base;

    NVIC_SetVectorTable((uint32_t)&isr_vector_table_base, 0x0);
#endif
    // Configure NVIC preempt/priority groups
    NVIC_PriorityGroupConfig(NVIC_PRIORITY_GROUPING);

#ifdef STM32F10X
    // Turn on clocks for stuff we use
    RCC_APB2PeriphClockCmd(RCC_APB2Periph_AFIO, ENABLE);
#endif

    // cache RCC->CSR value to use it in isMPUSoftreset() and others
    cachedRccCsrValue = RCC->CSR;
#ifdef STM32F40_41xxx
    /* Accounts for OP Bootloader, set the Vector Table base address as specified in .ld file */
    extern void *isr_vector_table_base;

    NVIC_SetVectorTable((uint32_t)&isr_vector_table_base, 0x0);

    RCC_AHB2PeriphClockCmd( RCC_AHB2Periph_OTG_FS, DISABLE);
#endif

    RCC_ClearFlag();

    enableGPIOPowerUsageAndNoiseReductions();

#ifdef STM32F10X
    // Set USART1 TX (PA9) to output and high state to prevent a rs232 break condition on reset.
    // See issue https://github.com/cleanflight/cleanflight/issues/1433
    gpio_config_t gpio;

    gpio.mode = Mode_Out_PP;
    gpio.speed = Speed_2MHz;
    gpio.pin = Pin_9;
    digitalHi(GPIOA, gpio.pin);
    gpioInit(GPIOA, &gpio);

    // Turn off JTAG port 'cause we're using the GPIO for leds
#define AFIO_MAPR_SWJ_CFG_NO_JTAG_SW            (0x2 << 24)
    AFIO->MAPR |= AFIO_MAPR_SWJ_CFG_NO_JTAG_SW;
#endif

    // Init cycle counter
    cycleCounterInit();


    memset(extiHandlerConfigs, 0x00, sizeof(extiHandlerConfigs));
    // SysTick
    SysTick_Config(SystemCoreClock / 1000);
}
コード例 #14
0
ファイル: run.c プロジェクト: Maelok/esc32
void runArm(void) {
    fetSetDutyCycle(0);
    timerCancelAlarm2();
    digitalHi(errorLed);
    state = ESC_STATE_STOPPED;
    digitalLo(statusLed);   // turn on
    if (inputMode == ESC_INPUT_UART)
	runMode = OPEN_LOOP;
    fetSetBraking(0);
    fetBeep(150, 800);
}
コード例 #15
0
ファイル: drv_spi.c プロジェクト: EvanLind/WingProject
void spiSelect(bool select)
{
    if (!isSPI)
        return;

    if (select) {
        digitalLo(GPIOB, Pin_12);
    } else {
        digitalHi(GPIOB, Pin_12);
    }
}
コード例 #16
0
static void i2cUnstick(void)
{
    gpio_config_t gpio;
    uint8_t i;

    gpio.pin = Pin_10 | Pin_11;
    gpio.speed = Speed_2MHz;
    gpio.mode = Mode_Out_OD;
    gpioInit(GPIOB, &gpio);

    digitalHi(GPIOB, Pin_10 | Pin_11);
    for (i = 0; i < 8; i++) {
        // Wait for any clock stretching to finish
        while (!digitalIn(GPIOB, Pin_10))
            delayMicroseconds(10);

        // Pull low
        digitalLo(GPIOB, Pin_10); // Set bus low
        delayMicroseconds(10);
        // Release high again
        digitalHi(GPIOB, Pin_10); // Set bus high
        delayMicroseconds(10);
    }

    // Generate a start then stop condition
    // SCL  PB10
    // SDA  PB11
    digitalLo(GPIOB, Pin_11); // Set bus data low
    delayMicroseconds(10);
    digitalLo(GPIOB, Pin_10); // Set bus scl low
    delayMicroseconds(10);
    digitalHi(GPIOB, Pin_10); // Set bus scl high
    delayMicroseconds(10);
    digitalHi(GPIOB, Pin_11); // Set bus sda high

    // Init pins
    gpio.pin = Pin_10 | Pin_11;
    gpio.speed = Speed_2MHz;
    gpio.mode = Mode_AF_OD;
    gpioInit(GPIOB, &gpio);
}
コード例 #17
0
void setTxSignal(softSerial_t *softSerial, uint8_t state)
{
    if (softSerial->port.inversion == SERIAL_INVERTED) {
        state = !state;
    }

    if (state) {
        digitalHi(softSerial->txTimerHardware->gpio, softSerial->txTimerHardware->pin);
    } else {
        digitalLo(softSerial->txTimerHardware->gpio, softSerial->txTimerHardware->pin);
    }
}
コード例 #18
0
ファイル: serial_uart.c プロジェクト: Codeharp/cleanflight
void usartInitAllIOSignals(void)
{
#ifdef STM32F10X
    // Set UART1 TX to output and high state to prevent a rs232 break condition on reset.
    // See issue https://github.com/cleanflight/cleanflight/issues/1433
    gpio_config_t gpio;

    gpio.mode = Mode_Out_PP;
    gpio.speed = Speed_2MHz;
    gpio.pin = UART1_TX_PIN;
    digitalHi(UART1_GPIO, gpio.pin);
    gpioInit(UART1_GPIO, &gpio);

    // Set TX of UART2 and UART3 to input with pull-up to prevent floating TX outputs.
    gpio.mode = Mode_IPU;

#ifdef USE_UART2
    gpio.pin = UART2_TX_PIN;
    gpioInit(UART2_GPIO, &gpio);
#endif

#ifdef USE_UART3
    gpio.pin = UART3_TX_PIN;
    gpioInit(UART3_GPIO, &gpio);
#endif

#endif

#ifdef STM32F303
    // Set TX for UART1, UART2 and UART3 to input with pull-up to prevent floating TX outputs.
    gpio_config_t gpio;

    gpio.mode = Mode_IPU;
    gpio.speed = Speed_2MHz;

#ifdef USE_UART1
    gpio.pin = UART1_TX_PIN;
    gpioInit(UART1_GPIO, &gpio);
#endif

//#ifdef USE_UART2
//    gpio.pin = UART2_TX_PIN;
//    gpioInit(UART2_GPIO, &gpio);
//#endif

#ifdef USE_UART3
    gpio.pin = UART3_TX_PIN;
    gpioInit(UART3_GPIO, &gpio);
#endif

#endif
}
コード例 #19
0
void spiSelect(bool select, GPIO_TypeDef* port, GPIO_Pin pin)
{
    if (!isSPI)
        return;
		if (!port || !pin)
			  return;

    if (select) {
        digitalLo(port, pin);
    } else {
        digitalHi(port, pin);
    }
		
		delayMicroseconds(10);
}
コード例 #20
0
ファイル: run.c プロジェクト: Maelok/esc32
void runWatchDog(void) {
    register uint32_t t, d, p;

    __asm volatile ("cpsid i");
    t = timerMicros;
    d = detectedCrossing;
    p = pwmValidMicros;
    __asm volatile ("cpsie i");

    if (state == ESC_STATE_STARTING && fetGoodDetects > fetStartDetects) {
	state = ESC_STATE_RUNNING;
	digitalHi(statusLed);   // turn off
    }
    else if (state >= ESC_STATE_STOPPED) {   // running or starting
	d = (t >= d) ? (t - d) : (TIMER_MASK - d + t);

	// timeout if PWM signal disappears
	if (inputMode == ESC_INPUT_PWM) {
	    p = (t >= p) ? (t - p) : (TIMER_MASK - p + t);

	    if (p > PWM_TIMEOUT)
		runDisarm(REASON_PWM_TIMEOUT);
	}

//	if (state == ESC_STATE_RUNNING && d > ADC_CROSSING_TIMEOUT) {
	if (state >= ESC_STATE_STARTING && d > ADC_CROSSING_TIMEOUT) {
	    if (fetDutyCycle > 0) {
		runDisarm(REASON_CROSSING_TIMEOUT);
	    }
	    else {
		runArm();
		pwmIsrRunOn();
	    }
	}
	else if (state >= ESC_STATE_STARTING && fetBadDetects > fetDisarmDetects) {
	    if (fetDutyCycle > 0)
		runDisarm(REASON_BAD_DETECTS);
	}
	else if (state == ESC_STATE_STOPPED) {
	    adcAmpsOffset = adcAvgAmps;	// record current amperage offset
	}
    }
    else if (state == ESC_STATE_DISARMED && !(runMilis % 100)) {
	adcAmpsOffset = adcAvgAmps;	// record current amperage offset
	digitalTogg(errorLed);
    }
}
コード例 #21
0
ファイル: Arduino.cpp プロジェクト: simondlevy/BreezySTM32
void digitalWrite(uint8_t pin, uint8_t level)
{
    pin = 1<<pin;

    GPIO_TypeDef * gpio = gpio_type_from_pin(pin);

    uint16_t gpio_pin = gpio_pin_from_pin(pin);

    switch (level) {
        case HIGH:
            digitalLo(gpio, gpio_pin);
            break;
        case LOW:
            digitalHi(gpio, gpio_pin);
            break;
    }
}
コード例 #22
0
// measurement reading is done asynchronously, using interrupt
void hcsr04_start_reading(void)
{
    uint32_t now = millis();

    if (now < (lastMeasurementAt + 60)) {
        // the repeat interval of trig signal should be greater than 60ms
        // to avoid interference between connective measurements.
        return;
    }

    lastMeasurementAt = now;

    digitalHi(GPIOB, sonarHardware->trigger_pin);
    //  The width of trig signal must be greater than 10us
    delayMicroseconds(11);
    digitalLo(GPIOB, sonarHardware->trigger_pin);
}
コード例 #23
0
ファイル: sonar_hcsr04.c プロジェクト: gurkenfolie/inav
/*
 * Start a range reading
 * Called periodically by the scheduler
 * Measurement reading is done asynchronously, using interrupt
 */
void hcsr04_start_reading(void)
{
#if !defined(UNIT_TEST)
     static uint32_t timeOfLastMeasurementMs = 0;
    // the firing interval of the trigger signal should be greater than 60ms
    // to avoid interference between consecutive measurements.
    #define HCSR04_MinimumFiringIntervalMs 60
    const uint32_t timeNowMs = millis();
    if (timeNowMs > timeOfLastMeasurementMs + HCSR04_MinimumFiringIntervalMs) {
        timeOfLastMeasurementMs = timeNowMs;
        digitalHi(sonarHcsr04Hardware.trigger_gpio, sonarHcsr04Hardware.trigger_pin);
        //  The width of trigger signal must be greater than 10us, according to device spec
        delayMicroseconds(11);
        digitalLo(sonarHcsr04Hardware.trigger_gpio, sonarHcsr04Hardware.trigger_pin);
    }
#endif
}
コード例 #24
0
ファイル: drv_hcsr04.c プロジェクト: CamBl98/afrodevices
// distance calculation is done asynchronously, using interrupt
void hcsr04_get_distance(volatile int32_t *distance)
{
    uint32_t current_time = millis();

    if (current_time < (last_measurement + 60)) {
        // the repeat interval of trig signal should be greater than 60ms
        // to avoid interference between connective measurements.
        return;
    }

    last_measurement = current_time;
    distance_ptr = distance;

    digitalHi(GPIOB, trigger_pin);
    //  The width of trig signal must be greater than 10us
    delayMicroseconds(11);
    digitalLo(GPIOB, trigger_pin);
}
コード例 #25
0
ファイル: nav.c プロジェクト: ChrelleP/autoquad
// Set fixType as a rough indication of GPS data quality
void navSetFixType(void) {
    unsigned long posTimeDlta = IMU_LASTUPD - gpsData.lastPosUpdate;
    float hAccMsk = gpsData.hAcc + runData.accMask;

    if (posTimeDlta < NAV_MAX_GPS_AGE && hAccMsk < NAV_MIN_GPS_ACC)
        navData.fixType = 3;
    else if (posTimeDlta < NAV_MAX_FIX_AGE && hAccMsk < NAV_MIN_FIX_ACC)
        navData.fixType = 2;
    else
        navData.fixType = 0;

    if (navData.fixType == 3) {
	if (!(supervisorData.state & STATE_CALIBRATION))
	    digitalHi(supervisorData.gpsLed);
    } else {
	if (!(supervisorData.state & STATE_CALIBRATION))
	    digitalLo(supervisorData.gpsLed);
    }
}
コード例 #26
0
void transponderIrDisable(void)
{
    GPIO_InitTypeDef GPIO_InitStructure;

    DMA_Cmd(TRANSPONDER_DMA_CHANNEL, DISABLE);
    TIM_Cmd(TRANSPONDER_TIMER, DISABLE);

    GPIO_StructInit(&GPIO_InitStructure);
    GPIO_InitStructure.GPIO_Pin = TRANSPONDER_PIN;
    GPIO_InitStructure.GPIO_Mode = GPIO_Mode_OUT;
    GPIO_InitStructure.GPIO_OType = GPIO_OType_PP;
    GPIO_InitStructure.GPIO_PuPd = GPIO_PuPd_DOWN;
    GPIO_InitStructure.GPIO_Speed = GPIO_Speed_50MHz;
    GPIO_Init(TRANSPONDER_GPIO, &GPIO_InitStructure);
#ifdef TRANSPONDER_INVERTED
    digitalHi(TRANSPONDER_GPIO, TRANSPONDER_PIN);
#else
    digitalLo(TRANSPONDER_GPIO, TRANSPONDER_PIN);
#endif
}
コード例 #27
0
ファイル: spi.c プロジェクト: KHIEM2812/auto_quad_fc
static void spiDeselect(spiClient_t *client) {
    digitalHi(client->cs);
}
コード例 #28
0
ファイル: supervisor.c プロジェクト: srinath4/Cartos-AQ
void supervisorTaskCode(void *unused) {
    uint32_t count = 0;

    AQ_NOTICE("Supervisor task started\n");

    // wait for ADC vIn data
    while (analogData.batCellCount == 0)
        yield(100);

    supervisorCreateSOCTable();

    supervisorData.vInLPF = analogData.vIn;
    supervisorData.soc = 100.0f;

    while (1) {
        yield(1000/SUPERVISOR_RATE);

    if (supervisorData.state & STATE_CALIBRATION) {
        int i;

        // try to indicate completion percentage
        i = constrainInt(20*((calibData.percentComplete)/(100.0f/3.0f)), 1, 21);
        if (i > 20)
            digitalHi(supervisorData.readyLed);
        else if (!(count % i))
            digitalTogg(supervisorData.readyLed);
#ifdef SUPERVISOR_DEBUG_PORT
        i = constrainInt(20*((calibData.percentComplete-100.0f/3.0f)/(100.0f/3.0f)), 1, 21);
        if (i > 20)
            digitalHi(supervisorData.debugLed);
        else if (!(count % i))
            digitalTogg(supervisorData.debugLed);
#endif
        i = constrainInt(20*((calibData.percentComplete-100.0f/3.0f*2.0f)/(100.0f/3.0f)), 1, 21);
        if (i > 20)
            digitalHi(supervisorData.gpsLed);
        else if (!(count % i))
            digitalTogg(supervisorData.gpsLed);

        // user looking to go back to DISARMED mode?
        if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500) {
            if (!supervisorData.armTime) {
                supervisorData.armTime = timerMicros();
            }
            else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
                supervisorDisarm();
                supervisorData.armTime = 0;
            }
        }
        else {
            supervisorData.armTime = 0;
        }
    }
    else if (supervisorData.state & STATE_DISARMED) {
#ifdef SUPERVISOR_DEBUG_PORT
        // 0.5 Hz blink debug LED if config file could be found on uSD card
        if (supervisorData.configRead && (!(count % SUPERVISOR_RATE))) {
            // only for first 15s
            if (timerMicros() > 15000000) {
                supervisorData.configRead = 0;
                digitalLo(supervisorData.debugLed);
            }
            else {
                digitalTogg(supervisorData.debugLed);
            }
        }
#endif

        // 1 Hz blink if disarmed, 5 Hz if writing to uSD card
        if (!(count % ((supervisorData.diskWait) ? SUPERVISOR_RATE/10 : SUPERVISOR_RATE/2)))
            digitalTogg(supervisorData.readyLed);

        // Arm if all the switches are in default (startup positions) - flaps down, aux2 centered
        if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD > +500 && RADIO_FLAPS < -250 && !navData.homeActionFlag && navData.headFreeMode == NAV_HEADFREE_OFF) {
            if (!supervisorData.armTime) {
                supervisorData.armTime = timerMicros();
            }
            else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
                supervisorArm();
                supervisorData.armTime = 0;
            }
        }
        else {
            supervisorData.armTime = 0;
        }

        // various functions
        if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500) {
#ifdef HAS_DIGITAL_IMU
            // tare function (lower left)
            if (RADIO_ROLL < -500 && RADIO_PITCH > +500) {
                supervisorTare();
            }
#endif
            // config write (upper right)
            if (RADIO_VALID && RADIO_ROLL > +500 && RADIO_PITCH < -500) {
                supervisorLEDsOn();
                configFlashWrite();
#ifdef DIMU_HAVE_EEPROM
                dIMURequestCalibWrite();
#endif
                supervisorLEDsOff();
            }

            // calibration mode (upper left)
            if (RADIO_ROLL < -500 && RADIO_PITCH < -500) {
                supervisorCalibrate();
            }
        }
    }
    else if (supervisorData.state & STATE_ARMED) {
        // Disarm only if in manual mode
        if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500 && navData.mode == NAV_STATUS_MANUAL) {
            if (!supervisorData.armTime) {
                supervisorData.armTime = timerMicros();
            }
            else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
                supervisorDisarm();
                supervisorData.armTime = 0;
            }
        }
        else {
            supervisorData.armTime = 0;
        }
    }

    // radio loss
    if ((supervisorData.state & STATE_FLYING) && (navData.mode < NAV_STATUS_MISSION || (supervisorData.state & STATE_RADIO_LOSS2))) {
        // regained?
        if (RADIO_QUALITY > 1.0f) {
            supervisorData.lastGoodRadioMicros = timerMicros();

            if (supervisorData.state & STATE_RADIO_LOSS1)
                AQ_NOTICE("Warning: radio signal regained\n");

            supervisorData.state &= ~(STATE_RADIO_LOSS1 | STATE_RADIO_LOSS2);
        }
        // loss 1
        else if (!(supervisorData.state & STATE_RADIO_LOSS1) && (timerMicros() - supervisorData.lastGoodRadioMicros) > SUPERVISOR_RADIO_LOSS1) {
            supervisorData.state |= STATE_RADIO_LOSS1;
            AQ_NOTICE("Warning: Radio loss stage 1 detected\n");

            // hold position
            RADIO_FLAPS = 0;    // position hold
            RADIO_AUX2 = 0;     // normal home mode
            RADIO_PITCH = 0;    // center sticks
            RADIO_ROLL = 0;
            RADIO_RUDD = 0;
            RADIO_THROT = RADIO_MID_THROTTLE;  // center throttle
        }
        // loss 2
        else if (!(supervisorData.state & STATE_RADIO_LOSS2) && (timerMicros() - supervisorData.lastGoodRadioMicros) > SUPERVISOR_RADIO_LOSS2) {
            supervisorData.state |= STATE_RADIO_LOSS2;
            AQ_NOTICE("Warning: Radio loss stage 2! Initiating recovery mission.\n");

            // only available with GPS
            if (navData.navCapable) {
                navMission_t *wp;
                uint8_t wpi = 0;
                uint8_t fsOption = (uint8_t)p[SPVR_FS_RAD_ST2];

                navClearWaypoints();
                wp = navGetWaypoint(wpi++);

                if (fsOption > SPVR_OPT_FS_RAD_ST2_LAND && navCalcDistance(gpsData.lat, gpsData.lon, navData.homeLeg.targetLat, navData.homeLeg.targetLon) > SUPERVISOR_HOME_POS_DETECT_RADIUS) {
                    float targetAltitude;

                    // ascend
                    if (fsOption == SPVR_OPT_FS_RAD_ST2_ASCEND && ALTITUDE < navData.homeLeg.targetAlt + p[SPVR_FS_ADD_ALT]) {
                        // the home leg's altitude is recorded without pressure offset
                        targetAltitude = navData.homeLeg.targetAlt + p[SPVR_FS_ADD_ALT] + navData.presAltOffset;

                        wp->type = NAV_LEG_GOTO;
                        wp->relativeAlt = 0;
                        wp->targetAlt = targetAltitude;
                        wp->targetLat = gpsData.lat;
                        wp->targetLon = gpsData.lon;
                        wp->targetRadius = SUPERVISOR_HOME_ALT_DETECT_MARGIN;
                        wp->maxHorizSpeed = navData.homeLeg.maxHorizSpeed;
                        wp->maxVertSpeed = navData.homeLeg.maxVertSpeed;
                        wp->poiHeading = navData.homeLeg.poiHeading;
                        wp->loiterTime = 0;
                        wp->poiAltitude = 0.0f;

                        wp = navGetWaypoint(wpi++);
                    }
                    else {
                        // the greater of our current altitude or home's altitude
                        targetAltitude = ((ALTITUDE > navData.homeLeg.targetAlt) ? ALTITUDE : navData.homeLeg.targetAlt) + navData.presAltOffset;
                    }

                    // go home with previously determined altitude
                    wp->type = NAV_LEG_GOTO;
                    wp->relativeAlt = 0;
                    wp->targetAlt = targetAltitude;
                    wp->targetLat = navData.homeLeg.targetLat;
                    wp->targetLon = navData.homeLeg.targetLon;
                    wp->targetRadius = SUPERVISOR_HOME_POS_DETECT_RADIUS;
                    wp->maxHorizSpeed = navData.homeLeg.maxHorizSpeed;
                    wp->maxVertSpeed = navData.homeLeg.maxVertSpeed;
                    wp->poiHeading = navData.homeLeg.poiHeading;
                    wp->loiterTime = 0;
                    wp->poiAltitude = 0.0f;

                    wp = navGetWaypoint(wpi++);

                    // decend to home
                    wp->type = NAV_LEG_HOME;
                    wp->targetRadius = SUPERVISOR_HOME_POS_DETECT_RADIUS;
                    wp->loiterTime = 0;
                    wp->poiAltitude = 0.0f;

                    wp = navGetWaypoint(wpi++);
                }

                // land
                wp->type = NAV_LEG_LAND;
                wp->maxVertSpeed = p[NAV_LANDING_VEL];
                wp->maxHorizSpeed = 0.0f;
                wp->poiAltitude = 0.0f;

                // go
                navData.missionLeg = 0;
                RADIO_FLAPS = 500;                  // mission mode
            }
            // no GPS, slow decent in PH mode
            else {
                RADIO_FLAPS = 0;    // position hold
                RADIO_AUX2 = 0;     // normal home mode
                RADIO_PITCH = 0;    // center sticks
                RADIO_ROLL = 0;
                RADIO_RUDD = 0;
                RADIO_THROT = RADIO_MID_THROTTLE * 3 / 4;  // 1/4 max decent
            }
        }
    }

    // smooth vIn readings
    supervisorData.vInLPF += (analogData.vIn - supervisorData.vInLPF) * (0.1f / SUPERVISOR_RATE);

    // determine battery state of charge
    supervisorData.soc = supervisorSOCTableLookup(supervisorData.vInLPF);

    // low battery
    if (!(supervisorData.state & STATE_LOW_BATTERY1) && supervisorData.vInLPF < (p[SPVR_LOW_BAT1]*analogData.batCellCount)) {
        supervisorData.state |= STATE_LOW_BATTERY1;
        AQ_NOTICE("Warning: Low battery stage 1\n");

        // TODO: something
    }
    else if (!(supervisorData.state & STATE_LOW_BATTERY2) && supervisorData.vInLPF < (p[SPVR_LOW_BAT2]*analogData.batCellCount)) {
        supervisorData.state |= STATE_LOW_BATTERY2;
        AQ_NOTICE("Warning: Low battery stage 2\n");

        // TODO: something
    }

    if (supervisorData.state & STATE_FLYING) {
        // count flight time in seconds
        supervisorData.flightTime += (1.0f / SUPERVISOR_RATE);

        // calculate remaining flight time
        if (supervisorData.soc < 99.0f) {
            supervisorData.flightSecondsAvg += (supervisorData.flightTime / (100.0f - supervisorData.soc) - supervisorData.flightSecondsAvg) * (0.01f / SUPERVISOR_RATE);
            supervisorData.flightTimeRemaining = supervisorData.flightSecondsAvg * supervisorData.soc;
        }
        else {
            supervisorData.flightSecondsAvg = supervisorData.flightTime;
            supervisorData.flightTimeRemaining = 999.9f * 60.0f;		// unknown
        }

        // rapidly flash Ready LED if we are critically low on power
        if (supervisorData.state & STATE_LOW_BATTERY2)
            digitalTogg(supervisorData.readyLed);
    }
    else if (supervisorData.state & STATE_ARMED) {
        digitalHi(supervisorData.readyLed);
    }

#ifdef SUPERVISOR_DEBUG_PORT
    // DEBUG LED to indicate radio RX state
    if (!supervisorData.configRead && RADIO_INITIALIZED && supervisorData.state != STATE_CALIBRATION) {
        // packet received in the last 50ms?
        if (RADIO_VALID) {
            digitalHi(supervisorData.debugLed);
        }
        else {
            if (RADIO_BINDING)
                digitalTogg(supervisorData.debugLed);
            else
                digitalLo(supervisorData.debugLed);
        }
    }
#endif

    count++;

#ifdef USE_SIGNALING
    signalingEvent();
#endif
    }
}
コード例 #29
0
void supervisorConfigRead(void) {
    supervisorData.configRead = 1;
#ifdef SUPERVISOR_DEBUG_PORT
    digitalHi(supervisorData.debugLed);
#endif
}
コード例 #30
0
void supervisorTaskCode(void *unused) {
    unsigned long lastAqCounter = 0;  // used for idle time calc
    uint32_t count = 0;

    AQ_NOTICE("Supervisor task started\n");

    // wait for ADC vIn data
    while (analogData.batCellCount == 0)
	yield(100);

    supervisorData.vInLPF = analogData.vIn;

    if (analogData.extAmp > 0.0f)
	supervisorData.currentSenseValPtr = &analogData.extAmp;
    else if (canSensorsData.values[CAN_SENSORS_PDB_BATA] > 0.0f)
	supervisorData.currentSenseValPtr = &canSensorsData.values[CAN_SENSORS_PDB_BATA];
    else
	supervisorData.aOutLPF = SUPERVISOR_INVALID_AMPSOUT_VALUE;

    if (supervisorData.currentSenseValPtr)
	supervisorData.aOutLPF = *supervisorData.currentSenseValPtr;

    while (1) {
	yield(1000/SUPERVISOR_RATE);

	if (supervisorData.state & STATE_CALIBRATION) {
	    int i;

	    // try to indicate completion percentage
	    i = constrainInt(20*((calibData.percentComplete)/(100.0f/3.0f)), 1, 21);
	    if (i > 20)
		digitalHi(supervisorData.readyLed);
	    else if (!(count % i))
		digitalTogg(supervisorData.readyLed);

#ifdef SUPERVISOR_DEBUG_PORT
	    i = constrainInt(20*((calibData.percentComplete-100.0f/3.0f)/(100.0f/3.0f)), 1, 21);
	    if (i > 20)
		digitalHi(supervisorData.debugLed);
	    else if (!(count % i))
		digitalTogg(supervisorData.debugLed);
#endif //SUPERVISOR_DEBUG_PORT

	    i = constrainInt(20*((calibData.percentComplete-100.0f/3.0f*2.0f)/(100.0f/3.0f)), 1, 21);
	    if (i > 20)
		digitalHi(supervisorData.gpsLed);
	    else if (!(count % i))
		digitalTogg(supervisorData.gpsLed);

	    // user looking to go back to DISARMED mode?
	    if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500) {
		if (!supervisorData.armTime) {
		    supervisorData.armTime = timerMicros();
		}
		else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
		    supervisorDisarm();
		    supervisorData.armTime = 0;
		}
	    }
	    else {
		supervisorData.armTime = 0;
	    }
	}  // end if calibrating
	else if (supervisorData.state & STATE_DISARMED) {

#ifdef SUPERVISOR_DEBUG_PORT
	    // 0.5 Hz blink debug LED if config file could be found on uSD card
	    if (supervisorData.configRead && (!(count % SUPERVISOR_RATE))) {
		// only for first 15s
		if (timerMicros() > 15000000) {
		    supervisorData.configRead = 0;
		    digitalLo(supervisorData.debugLed);
		}
		else {
		    digitalTogg(supervisorData.debugLed);
		}
	    }
#endif // SUPERVISOR_DEBUG_PORT

	    // 1 Hz blink if disarmed, 5 Hz if writing to uSD card
	    if (!(count % ((supervisorData.diskWait) ? SUPERVISOR_RATE/10 : SUPERVISOR_RATE/2)))
		digitalTogg(supervisorData.readyLed);

	    // Attempt to arm if throttle down and yaw full right for 2sec.
	    if (RADIO_VALID && RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD > +500) {
		if (!supervisorData.armTime) {
		    supervisorData.armTime = timerMicros();
		}
		else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
		    supervisorArm();
		    supervisorData.armTime = 0;
		}
	    }
	    else {
		supervisorData.armTime = 0;
	    }

	    // various functions
	    if (RADIO_VALID && RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500) {
		if (!supervisorData.stickCmdTimer) {
		    supervisorData.stickCmdTimer = timerMicros();
		} else if ((timerMicros() - supervisorData.stickCmdTimer) > SUPERVISOR_STICK_CMD_TIME) {

#ifdef HAS_DIGITAL_IMU
		    // tare function (lower left)
		    if (RADIO_ROLL < -500 && RADIO_PITCH > +500) {
			supervisorTare();
			supervisorData.stickCmdTimer = 0;
		    }
		    else
#endif // HAS_DIGITAL_IMU
		    // config write (upper right)
		    if (RADIO_ROLL > +500 && RADIO_PITCH < -500) {
			supervisorLEDsOn();
			configSaveParamsToFlash();
#ifdef DIMU_HAVE_EEPROM
			dIMURequestCalibWrite();
#endif
			supervisorLEDsOff();
			supervisorData.stickCmdTimer = 0;
		    }
		    // calibration mode (upper left)
		    else if (RADIO_ROLL < -500 && RADIO_PITCH < -500) {
			supervisorCalibrate();
			supervisorData.stickCmdTimer = 0;
		    }
		    // clear waypoints (lower right with WP Record switch active)
		    else if (RADIO_ROLL > 500 && RADIO_PITCH > 500 && rcIsSwitchActive(NAV_CTRL_WP_REC)) {
			navClearWaypoints();
			supervisorData.stickCmdTimer = 0;
		    }
		} // end stick timer check
	    }
	    // no stick commands detected
	    else
		supervisorData.stickCmdTimer = 0;

	} // end if disarmed
	else if (supervisorData.state & STATE_ARMED) {
	    // Disarm only if in manual mode
	    if (RADIO_THROT < p[CTRL_MIN_THROT] && RADIO_RUDD < -500 && navData.mode == NAV_STATUS_MANUAL) {
		if (!supervisorData.armTime) {
		    supervisorData.armTime = timerMicros();
		}
		else if ((timerMicros() - supervisorData.armTime) > SUPERVISOR_DISARM_TIME) {
		    supervisorDisarm();
		    supervisorData.armTime = 0;
		}
	    }
	    else {
		supervisorData.armTime = 0;
	    }
	}
	// end of calibrating/disarmed/armed mode checks

	// radio loss
	if ((supervisorData.state & STATE_FLYING) && (navData.mode < NAV_STATUS_MISSION || (supervisorData.state & STATE_RADIO_LOSS2))) {
	    // regained?
	    if (RADIO_QUALITY > 1.0f) {
		supervisorData.lastGoodRadioMicros = timerMicros();

		if (supervisorData.state & STATE_RADIO_LOSS1)
		    AQ_NOTICE("Warning: radio signal regained\n");

		navData.spvrModeOverride = 0;
		supervisorData.state &= ~(STATE_RADIO_LOSS1 | STATE_RADIO_LOSS2);
	    }
	    // loss 1
	    else if (!(supervisorData.state & STATE_RADIO_LOSS1) && (timerMicros() - supervisorData.lastGoodRadioMicros) > SUPERVISOR_RADIO_LOSS1) {
		supervisorData.state |= STATE_RADIO_LOSS1;
		AQ_NOTICE("Warning: Radio loss stage 1 detected\n");

		// hold position
		navData.spvrModeOverride = NAV_STATUS_POSHOLD;
		RADIO_PITCH = 0;    // center sticks
		RADIO_ROLL = 0;
		RADIO_RUDD = 0;
		RADIO_THROT = RADIO_MID_THROTTLE;  // center throttle
	    }
	    // loss 2
	    else if (!(supervisorData.state & STATE_RADIO_LOSS2) && (timerMicros() - supervisorData.lastGoodRadioMicros) > SUPERVISOR_RADIO_LOSS2) {
		supervisorData.state |= STATE_RADIO_LOSS2;
		AQ_NOTICE("Warning: Radio loss stage 2! Initiating recovery.\n");

		// only available with GPS
		if (navData.navCapable) {
		    navMission_t *wp;
		    uint8_t wpi = 0;
		    uint8_t fsOption = (uint8_t)p[SPVR_FS_RAD_ST2];

		    navClearWaypoints();
		    wp = navGetWaypoint(wpi++);

		    if (fsOption > SPVR_OPT_FS_RAD_ST2_LAND && navCalcDistance(gpsData.lat, gpsData.lon, navData.homeLeg.targetLat, navData.homeLeg.targetLon) > SUPERVISOR_HOME_POS_DETECT_RADIUS) {
			float targetAltitude;

			// ascend
			if (fsOption == SPVR_OPT_FS_RAD_ST2_ASCEND && ALTITUDE < navData.homeLeg.targetAlt + p[SPVR_FS_ADD_ALT]) {
			    // the home leg's altitude is recorded without pressure offset
			    targetAltitude = navData.homeLeg.targetAlt + p[SPVR_FS_ADD_ALT] + navData.presAltOffset;

			    wp->type = NAV_LEG_GOTO;
			    wp->relativeAlt = 0;
			    wp->targetAlt = targetAltitude;
			    wp->targetLat = gpsData.lat;
			    wp->targetLon = gpsData.lon;
			    wp->targetRadius = SUPERVISOR_HOME_ALT_DETECT_MARGIN;
			    wp->maxHorizSpeed = navData.homeLeg.maxHorizSpeed;
			    wp->maxVertSpeed = navData.homeLeg.maxVertSpeed;
			    wp->poiHeading = navData.homeLeg.poiHeading;
			    wp->loiterTime = 0;
			    wp->poiAltitude = 0.0f;

			    wp = navGetWaypoint(wpi++);
			}
			else {
			    // the greater of our current altitude or home's altitude
			    targetAltitude = ((ALTITUDE > navData.homeLeg.targetAlt) ? ALTITUDE : navData.homeLeg.targetAlt) + navData.presAltOffset;
			}

			// go home with previously determined altitude
			wp->type = NAV_LEG_GOTO;
			wp->relativeAlt = 0;
			wp->targetAlt = targetAltitude;
			wp->targetLat = navData.homeLeg.targetLat;
			wp->targetLon = navData.homeLeg.targetLon;
			wp->targetRadius = SUPERVISOR_HOME_POS_DETECT_RADIUS;
			wp->maxHorizSpeed = navData.homeLeg.maxHorizSpeed;
			wp->maxVertSpeed = navData.homeLeg.maxVertSpeed;
			wp->poiHeading = navData.homeLeg.poiHeading;
			wp->loiterTime = 0;
			wp->poiAltitude = 0.0f;

			wp = navGetWaypoint(wpi++);

			// decend to home
			wp->type = NAV_LEG_HOME;
			wp->targetRadius = SUPERVISOR_HOME_POS_DETECT_RADIUS;
			wp->loiterTime = 0;
			wp->poiAltitude = 0.0f;

			wp = navGetWaypoint(wpi++);
		    }

		    // land
		    wp->type = NAV_LEG_LAND;
		    wp->maxVertSpeed = NAV_DFLT_LND_SPEED;
		    wp->maxHorizSpeed = 0.0f;
		    wp->poiAltitude = 0.0f;

		    // go
		    navData.missionLeg = 0;
		    navData.tempMissionLoaded = 1;
		    navData.spvrModeOverride = NAV_STATUS_MISSION;
		}
		// no GPS, slow decent in PH mode
		else {
		    navData.spvrModeOverride = NAV_STATUS_POSHOLD;
		    RADIO_PITCH = 0;    // center sticks
		    RADIO_ROLL = 0;
		    RADIO_RUDD = 0;
		    RADIO_THROT = RADIO_MID_THROTTLE * 3 / 4;  // 1/4 max decent
		}
	    }
	}
	// end radio loss check

	// calculate idle time
	supervisorData.idlePercent = (counter - lastAqCounter) * minCycles * 100.0f / ((1e6f / SUPERVISOR_RATE) * rccClocks.SYSCLK_Frequency / 1e6f);
	lastAqCounter = counter;

	// smooth vIn readings
	supervisorData.vInLPF += (analogData.vIn - supervisorData.vInLPF) * (0.1f / SUPERVISOR_RATE);

	// smooth current flow readings, if any
	if (supervisorData.currentSenseValPtr)
	    supervisorData.aOutLPF += (*supervisorData.currentSenseValPtr - supervisorData.aOutLPF) * (0.1f / SUPERVISOR_RATE);

	//calculate remaining battery % based on configured low batt stg 2 level -- ASSumes 4.2v/cell maximum
	supervisorData.battRemainingPrct = (supervisorData.vInLPF - p[SPVR_LOW_BAT2] * analogData.batCellCount) / ((4.2f - p[SPVR_LOW_BAT2]) * analogData.batCellCount) * 100;

	// low battery
	if (!(supervisorData.state & STATE_LOW_BATTERY1) && supervisorData.vInLPF < (p[SPVR_LOW_BAT1]*analogData.batCellCount)) {
	    supervisorData.state |= STATE_LOW_BATTERY1;
	    AQ_NOTICE("Warning: Low battery stage 1\n");

	    // TODO: something
	}
	else if (!(supervisorData.state & STATE_LOW_BATTERY2) && supervisorData.vInLPF < (p[SPVR_LOW_BAT2]*analogData.batCellCount)) {
	    supervisorData.state |= STATE_LOW_BATTERY2;
	    AQ_NOTICE("Warning: Low battery stage 2\n");

	    // TODO: something
	}
	// end battery level checks

	supervisorSetSystemStatus();

	if (supervisorData.state & STATE_FLYING) {
	    // count flight time in seconds
	    supervisorData.flightTime += (1.0f / SUPERVISOR_RATE);

	    // rapidly flash Ready LED if we are critically low on power
	    if (supervisorData.state & STATE_LOW_BATTERY2)
		digitalTogg(supervisorData.readyLed);
	}
	else if (supervisorData.state & STATE_ARMED) {
	    digitalHi(supervisorData.readyLed);
	}

#ifdef SUPERVISOR_DEBUG_PORT
	// DEBUG LED to indicate radio RX state
	if (!supervisorData.configRead && RADIO_INITIALIZED && supervisorData.state != STATE_CALIBRATION) {
	    // packet received in the last 50ms?
	    if (RADIO_VALID) {
		digitalHi(supervisorData.debugLed);
	    }
	    else {
		if (RADIO_BINDING)
		    digitalTogg(supervisorData.debugLed);
		else
		    digitalLo(supervisorData.debugLed);
	    }
	}
#endif

	count++;

#ifdef USE_SIGNALING
	signalingEvent();
#endif
    }
}