Exemple #1
0
void telemetryListenerCB(evr_t e)
{
    if (expandEvr)
        telemetryPrintF("EVR-%s %8.3fs %s (%04x)\n", evrToSeverityStr(e.evr), (float)e.time/1000., evrToStr(e.evr), e.reason);
    else
        telemetryPrintF("EVR:%08x %04x %04x\n", e.time, e.evr, e.reason);
}
Exemple #2
0
int main(void)
{
	///////////////////////////////////////////////////////////////////////////

	uint32_t currentTime;

    systemInit();

    systemReady = true;

    while (1)
    {
    	///////////////////////////////

        if (frame_50Hz)
        {
        	frame_50Hz = false;

        	currentTime      = micros();
			deltaTime50Hz    = currentTime - previous50HzTime;
			previous50HzTime = currentTime;

			processFlightCommands();

			if (eepromConfig.osdEnabled)
			{
				if (eepromConfig.osdDisplayAlt)
				    displayAltitude(sensors.pressureAlt10Hz, 0.0f, DISENGAGED);

				if (eepromConfig.osdDisplayAH)
				    displayArtificialHorizon(sensors.attitude500Hz[ROLL], sensors.attitude500Hz[PITCH], flightMode);

				if (eepromConfig.osdDisplayAtt)
				    displayAttitude(sensors.attitude500Hz[ROLL], sensors.attitude500Hz[PITCH], flightMode);

				if (eepromConfig.osdDisplayHdg)
				    displayHeading(heading.mag);
			}

			executionTime50Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_10Hz)
        {
        	frame_10Hz = false;

        	currentTime      = micros();
			deltaTime10Hz    = currentTime - previous10HzTime;
			previous10HzTime = currentTime;

			if (newMagData == true)
			{
				sensors.mag10Hz[XAXIS] =   (float)rawMag[XAXIS].value * magScaleFactor[XAXIS] - eepromConfig.magBias[XAXIS];
			    sensors.mag10Hz[YAXIS] =   (float)rawMag[YAXIS].value * magScaleFactor[YAXIS] - eepromConfig.magBias[YAXIS];
			    sensors.mag10Hz[ZAXIS] = -((float)rawMag[ZAXIS].value * magScaleFactor[ZAXIS] - eepromConfig.magBias[ZAXIS]);

			    newMagData = false;
			    magDataUpdate = true;
			}

        	d1Average = d1Sum / 10;
        	d1Sum = 0;
        	calculateTemperature();
        	calculatePressureAltitude();

        	pressureAltValid = true;

        	switch (eepromConfig.gpsType)
			{
			    ///////////////////////

			    case NO_GPS:                // No GPS installed
			        break;

			    ///////////////////////

			    case MEDIATEK_3329_BINARY:  // MediaTek 3329 in binary mode
			    	decodeMediaTek3329BinaryMsg();
			    	break;

				///////////////////////

				case MEDIATEK_3329_NMEA:    // MediaTek 3329 in NMEA mode
				    decodeNMEAsentence();
	        	    break;

			    ///////////////////////

			    case UBLOX:                 // UBLOX in binary mode
			    	decodeUbloxMsg();
			    	break;

			    ///////////////////////
			}

        	cliCom();

        	rfCom();

            executionTime10Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_500Hz)
        {
			frame_500Hz = false;

       	    currentTime       = micros();
       	    deltaTime500Hz    = currentTime - previous500HzTime;
       	    previous500HzTime = currentTime;

       	    TIM_Cmd(TIM10, DISABLE);
       	 	timerValue = TIM_GetCounter(TIM10);
       	 	TIM_SetCounter(TIM10, 0);
       	 	TIM_Cmd(TIM10, ENABLE);

       	 	dt500Hz = (float)timerValue * 0.0000005f;  // For integrations in 500 Hz loop

            computeMPU6000TCBias();
            /*
            sensorTemp1 = computeMPU6000SensorTemp();
            sensorTemp2 = sensorTemp1 * sensorTemp1;
            sensorTemp3 = sensorTemp2 * sensorTemp1;
            */
            sensors.accel500Hz[XAXIS] =  ((float)accelSummedSamples500Hz[XAXIS] / 2.0f - accelTCBias[XAXIS]) * ACCEL_SCALE_FACTOR;
			sensors.accel500Hz[YAXIS] = -((float)accelSummedSamples500Hz[YAXIS] / 2.0f - accelTCBias[YAXIS]) * ACCEL_SCALE_FACTOR;
			sensors.accel500Hz[ZAXIS] = -((float)accelSummedSamples500Hz[ZAXIS] / 2.0f - accelTCBias[ZAXIS]) * ACCEL_SCALE_FACTOR;
            /*
            sensors.accel500Hz[XAXIS] =  ((float)accelSummedSamples500Hz[XAXIS] / 2.0f  +
                                          eepromConfig.accelBiasP0[XAXIS]               +
                                          eepromConfig.accelBiasP1[XAXIS] * sensorTemp1 +
                                          eepromConfig.accelBiasP2[XAXIS] * sensorTemp2 +
                                          eepromConfig.accelBiasP3[XAXIS] * sensorTemp3 ) * ACCEL_SCALE_FACTOR;

			sensors.accel500Hz[YAXIS] = -((float)accelSummedSamples500Hz[YAXIS] / 2.0f  +
			                              eepromConfig.accelBiasP0[YAXIS]               +
			                              eepromConfig.accelBiasP1[YAXIS] * sensorTemp1 +
			                              eepromConfig.accelBiasP2[YAXIS] * sensorTemp2 +
			                              eepromConfig.accelBiasP3[YAXIS] * sensorTemp3 ) * ACCEL_SCALE_FACTOR;

			sensors.accel500Hz[ZAXIS] = -((float)accelSummedSamples500Hz[ZAXIS] / 2.0f  +
			                              eepromConfig.accelBiasP0[ZAXIS]               +
			                              eepromConfig.accelBiasP1[ZAXIS] * sensorTemp1 +
			                              eepromConfig.accelBiasP2[ZAXIS] * sensorTemp2 +
			                              eepromConfig.accelBiasP3[ZAXIS] * sensorTemp3 ) * ACCEL_SCALE_FACTOR;
            */
            sensors.gyro500Hz[ROLL ] =  ((float)gyroSummedSamples500Hz[ROLL]  / 2.0f - gyroRTBias[ROLL ] - gyroTCBias[ROLL ]) * GYRO_SCALE_FACTOR;
			sensors.gyro500Hz[PITCH] = -((float)gyroSummedSamples500Hz[PITCH] / 2.0f - gyroRTBias[PITCH] - gyroTCBias[PITCH]) * GYRO_SCALE_FACTOR;
            sensors.gyro500Hz[YAW  ] = -((float)gyroSummedSamples500Hz[YAW]   / 2.0f - gyroRTBias[YAW  ] - gyroTCBias[YAW  ]) * GYRO_SCALE_FACTOR;
            /*
            sensors.gyro500Hz[ROLL ] =  ((float)gyroSummedSamples500Hz[ROLL ] / 2.0f  +
                                         gyroBiasP0[ROLL ]                            +
                                         eepromConfig.gyroBiasP1[ROLL ] * sensorTemp1 +
                                         eepromConfig.gyroBiasP2[ROLL ] * sensorTemp2 +
                                         eepromConfig.gyroBiasP3[ROLL ] * sensorTemp3 ) * GYRO_SCALE_FACTOR;

			sensors.gyro500Hz[PITCH] = -((float)gyroSummedSamples500Hz[PITCH] / 2.0f  +
			                             gyroBiasP0[PITCH]                            +
			                             eepromConfig.gyroBiasP1[PITCH] * sensorTemp1 +
			                             eepromConfig.gyroBiasP2[PITCH] * sensorTemp2 +
			                             eepromConfig.gyroBiasP3[PITCH] * sensorTemp3 ) * GYRO_SCALE_FACTOR;

            sensors.gyro500Hz[YAW  ] = -((float)gyroSummedSamples500Hz[YAW]   / 2.0f  +
                                         gyroBiasP0[YAW  ]                            +
                                         eepromConfig.gyroBiasP1[YAW  ] * sensorTemp1 +
                                         eepromConfig.gyroBiasP2[YAW  ] * sensorTemp2 +
                                         eepromConfig.gyroBiasP3[YAW  ] * sensorTemp3 ) * GYRO_SCALE_FACTOR;
            */
            MargAHRSupdate( sensors.gyro500Hz[ROLL],   sensors.gyro500Hz[PITCH],  sensors.gyro500Hz[YAW],
                            sensors.accel500Hz[XAXIS], sensors.accel500Hz[YAXIS], sensors.accel500Hz[ZAXIS],
                            sensors.mag10Hz[XAXIS],    sensors.mag10Hz[YAXIS],    sensors.mag10Hz[ZAXIS],
                            eepromConfig.accelCutoff,
                            magDataUpdate,
                            dt500Hz );

            magDataUpdate = false;

            computeAxisCommands(dt500Hz);
            mixTable();
            writeServos();
            writeMotors();

       	    executionTime500Hz = micros() - currentTime;
		}

        ///////////////////////////////

        if (frame_100Hz)
        {
        	frame_100Hz = false;

        	currentTime       = micros();
			deltaTime100Hz    = currentTime - previous100HzTime;
			previous100HzTime = currentTime;

			TIM_Cmd(TIM11, DISABLE);
			timerValue = TIM_GetCounter(TIM11);
			TIM_SetCounter(TIM11, 0);
			TIM_Cmd(TIM11, ENABLE);

			dt100Hz = (float)timerValue * 0.0000005f;  // For integrations in 100 Hz loop

			sensors.accel100Hz[XAXIS] =  ((float)accelSummedSamples100Hz[XAXIS] / 10.0f - accelTCBias[XAXIS]) * ACCEL_SCALE_FACTOR;
			sensors.accel100Hz[YAXIS] = -((float)accelSummedSamples100Hz[YAXIS] / 10.0f - accelTCBias[YAXIS]) * ACCEL_SCALE_FACTOR;
			sensors.accel100Hz[ZAXIS] = -((float)accelSummedSamples100Hz[ZAXIS] / 10.0f - accelTCBias[ZAXIS]) * ACCEL_SCALE_FACTOR;

        	createRotationMatrix();
        	bodyAccelToEarthAccel();
        	vertCompFilter(dt100Hz);

        	if ( highSpeedTelem1Enabled == true )
            {
            	// 500 Hz Accels
            	telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.accel500Hz[XAXIS],
            	        			                     sensors.accel500Hz[YAXIS],
            	        			                     sensors.accel500Hz[ZAXIS]);
            }

            if ( highSpeedTelem2Enabled == true )
            {
            	// 500 Hz Gyros
            	telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.gyro500Hz[ROLL ],
            	        			                     sensors.gyro500Hz[PITCH],
            	        					             sensors.gyro500Hz[YAW  ]);
            }

            if ( highSpeedTelem3Enabled == true )
            {
            	// Roll Rate, Roll Rate Command
            	telemetryPrintF("%9.4f, %9.4f\n", sensors.gyro500Hz[ROLL],
            			                          rxCommand[ROLL]);
            }

            if ( highSpeedTelem4Enabled == true )
            {
            	// Pitch Rate, Pitch Rate Command
            	telemetryPrintF("%9.4f, %9.4f\n", sensors.gyro500Hz[PITCH],
            	            			          rxCommand[PITCH]);
            }

            if ( highSpeedTelem5Enabled == true )
            {
            	// Yaw Rate, Yaw Rate Command
            	telemetryPrintF("%9.4f, %9.4f\n", sensors.gyro500Hz[YAW],
            	            	                  rxCommand[YAW]);
            }

            if ( highSpeedTelem6Enabled == true )
            {
            	// 500 Hz Attitudes
            	telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.attitude500Hz[ROLL ],
            	        			                     sensors.attitude500Hz[PITCH],
            	        			                     sensors.attitude500Hz[YAW  ]);
            }

            if ( highSpeedTelem7Enabled == true )
            {
               	// Vertical Variables
            	telemetryPrintF("%9.4f, %9.4f, %9.4f, %9.4f\n", earthAxisAccels[ZAXIS],
            			                                        sensors.pressureAlt10Hz,
            			                                        hDotEstimate,
            			                                        hEstimate);
            }

            executionTime100Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_5Hz)
        {
        	frame_5Hz = false;

        	currentTime     = micros();
			deltaTime5Hz    = currentTime - previous5HzTime;
			previous5HzTime = currentTime;

			if (execUp == true)
			    BLUE_LED_TOGGLE;

        	executionTime5Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_1Hz)
        {
        	frame_1Hz = false;

        	currentTime     = micros();
			deltaTime1Hz    = currentTime - previous1HzTime;
			previous1HzTime = currentTime;

			if (execUp == true)
			    GREEN_LED_TOGGLE;

			if (execUp == false)
			    execUpCount++;

			if ((execUpCount == 5) && (execUp == false))
			    execUp = true;

			executionTime1Hz = micros() - currentTime;
        }

        ////////////////////////////////
    }

    ///////////////////////////////////////////////////////////////////////////
}
Exemple #3
0
int main(void)
{
	///////////////////////////////////////////////////////////////////////////

	uint32_t currentTime;

    systemReady = false;

    systemInit();

    systemReady = true;

    evrPush(EVR_StartingMain, 0);

    while (1)
    {
    	evrCheck();

    	///////////////////////////////

        if (frame_50Hz)
        {
        	frame_50Hz = false;

        	currentTime      = micros();
			deltaTime50Hz    = currentTime - previous50HzTime;
			previous50HzTime = currentTime;

			processFlightCommands();

            if (newTemperatureReading && newPressureReading)
            {
                d1Value = d1.value;
                d2Value = d2.value;

                calculateTemperature();
                calculatePressureAltitude();

                newTemperatureReading = false;
                newPressureReading    = false;
            }

            sensors.pressureAlt50Hz = firstOrderFilter(sensors.pressureAlt50Hz, &firstOrderFilters[PRESSURE_ALT_LOWPASS]);

			executionTime50Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_10Hz)
        {
        	frame_10Hz = false;

        	currentTime      = micros();
			deltaTime10Hz    = currentTime - previous10HzTime;
			previous10HzTime = currentTime;

			if (newMagData == true)
			{
				sensors.mag10Hz[XAXIS] =   (float)rawMag[XAXIS].value * magScaleFactor[XAXIS] - eepromConfig.magBias[XAXIS];
			    sensors.mag10Hz[YAXIS] = -((float)rawMag[YAXIS].value * magScaleFactor[YAXIS] - eepromConfig.magBias[YAXIS]);
			    sensors.mag10Hz[ZAXIS] = -((float)rawMag[ZAXIS].value * magScaleFactor[ZAXIS] - eepromConfig.magBias[ZAXIS]);

			    newMagData = false;
			    magDataUpdate = true;
            }

        	decodeUbloxMsg();

        	batMonTick();

            cliCom();

            if (eepromConfig.mavlinkEnabled == true)
            {
				mavlinkSendAttitude();
				mavlinkSendVfrHud();
			}
			else
			{
				rfCom();
			}

        	executionTime10Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_500Hz)
        {
			frame_500Hz = false;

       	    currentTime       = micros();
       	    deltaTime500Hz    = currentTime - previous500HzTime;
       	    previous500HzTime = currentTime;

       	    TIM_Cmd(TIM6, DISABLE);
       	 	timerValue = TIM_GetCounter(TIM6);
       	 	TIM_SetCounter(TIM6, 0);
       	 	TIM_Cmd(TIM6, ENABLE);

       	 	dt500Hz = (float)timerValue * 0.0000005f;  // For integrations in 500 Hz loop

       	    computeMPU6000TCBias();

       	    sensors.accel500Hz[XAXIS] = -((float)accelSummedSamples500Hz[XAXIS] * 0.5f - eepromConfig.accelBiasMPU[XAXIS] - accelTCBias[XAXIS]) * eepromConfig.accelScaleFactorMPU[XAXIS];
            sensors.accel500Hz[YAXIS] =  ((float)accelSummedSamples500Hz[YAXIS] * 0.5f - eepromConfig.accelBiasMPU[YAXIS] - accelTCBias[YAXIS]) * eepromConfig.accelScaleFactorMPU[YAXIS];
            sensors.accel500Hz[ZAXIS] = -((float)accelSummedSamples500Hz[ZAXIS] * 0.5f - eepromConfig.accelBiasMPU[ZAXIS] - accelTCBias[ZAXIS]) * eepromConfig.accelScaleFactorMPU[ZAXIS];

            //sensors.accel500Hz[XAXIS] = firstOrderFilter(sensors.accel500Hz[XAXIS], &firstOrderFilters[ACCEL500HZ_X_LOWPASS]);
            //sensors.accel500Hz[YAXIS] = firstOrderFilter(sensors.accel500Hz[YAXIS], &firstOrderFilters[ACCEL500HZ_Y_LOWPASS]);
            //sensors.accel500Hz[ZAXIS] = firstOrderFilter(sensors.accel500Hz[ZAXIS], &firstOrderFilters[ACCEL500HZ_Z_LOWPASS]);

            sensors.gyro500Hz[ROLL ] = -((float)gyroSummedSamples500Hz[ROLL]  / 2.0f - gyroRTBias[ROLL ] - gyroTCBias[ROLL ]) * GYRO_SCALE_FACTOR;
            sensors.gyro500Hz[PITCH] =  ((float)gyroSummedSamples500Hz[PITCH] / 2.0f - gyroRTBias[PITCH] - gyroTCBias[PITCH]) * GYRO_SCALE_FACTOR;
            sensors.gyro500Hz[YAW  ] = -((float)gyroSummedSamples500Hz[YAW]   / 2.0f - gyroRTBias[YAW  ] - gyroTCBias[YAW  ]) * GYRO_SCALE_FACTOR;

            MargAHRSupdate( sensors.gyro500Hz[ROLL],   sensors.gyro500Hz[PITCH],  sensors.gyro500Hz[YAW],
                            sensors.accel500Hz[XAXIS], sensors.accel500Hz[YAXIS], sensors.accel500Hz[ZAXIS],
                            sensors.mag10Hz[XAXIS],    sensors.mag10Hz[YAXIS],    sensors.mag10Hz[ZAXIS],
                            eepromConfig.accelCutoff,
                            magDataUpdate,
                            dt500Hz );

            magDataUpdate = false;

            computeAxisCommands(dt500Hz);
            mixTable();
            writeServos();
            writeMotors();

       	    executionTime500Hz = micros() - currentTime;
		}

        ///////////////////////////////

        if (frame_100Hz)
        {
        	frame_100Hz = false;

        	currentTime       = micros();
			deltaTime100Hz    = currentTime - previous100HzTime;
			previous100HzTime = currentTime;

			TIM_Cmd(TIM7, DISABLE);
			timerValue = TIM_GetCounter(TIM7);
			TIM_SetCounter(TIM7, 0);
			TIM_Cmd(TIM7, ENABLE);

			dt100Hz = (float)timerValue * 0.0000005f;  // For integrations in 100 Hz loop

            sensors.accel100Hz[XAXIS] = -((float)accelSummedSamples100Hz[XAXIS] * 0.1f - eepromConfig.accelBiasMPU[XAXIS] - accelTCBias[XAXIS]) * eepromConfig.accelScaleFactorMPU[XAXIS];
            sensors.accel100Hz[YAXIS] =  ((float)accelSummedSamples100Hz[YAXIS] * 0.1f - eepromConfig.accelBiasMPU[YAXIS] - accelTCBias[YAXIS]) * eepromConfig.accelScaleFactorMPU[YAXIS];
            sensors.accel100Hz[ZAXIS] = -((float)accelSummedSamples100Hz[ZAXIS] * 0.1f - eepromConfig.accelBiasMPU[ZAXIS] - accelTCBias[ZAXIS]) * eepromConfig.accelScaleFactorMPU[ZAXIS];

			//sensors.accel100Hz[XAXIS] = firstOrderFilter(sensors.accel100Hz[XAXIS], &firstOrderFilters[ACCEL100HZ_X_LOWPASS]);
			//sensors.accel100Hz[YAXIS] = firstOrderFilter(sensors.accel100Hz[YAXIS], &firstOrderFilters[ACCEL100HZ_Y_LOWPASS]);
			//sensors.accel100Hz[ZAXIS] = firstOrderFilter(sensors.accel100Hz[ZAXIS], &firstOrderFilters[ACCEL100HZ_Z_LOWPASS]);

			createRotationMatrix();
            bodyAccelToEarthAccel();
            vertCompFilter(dt100Hz);

            if (armed == true)
            {
				if ( eepromConfig.activeTelemetry == 1 )
                {
            	    // 500 Hz Accels
            	    telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.accel500Hz[XAXIS],
            	            			                     sensors.accel500Hz[YAXIS],
            	            			                     sensors.accel500Hz[ZAXIS]);
                }

                if ( eepromConfig.activeTelemetry == 2 )
                {
            	    // 500 Hz Gyros
            	    telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.gyro500Hz[ROLL ],
            	            			                     sensors.gyro500Hz[PITCH],
            	            					             sensors.gyro500Hz[YAW  ]);
                }

                if ( eepromConfig.activeTelemetry == 4 )
                {
            	    // 500 Hz Attitudes
            	    telemetryPrintF("%9.4f, %9.4f, %9.4f\n", sensors.attitude500Hz[ROLL ],
            	            			                     sensors.attitude500Hz[PITCH],
            	            			                     sensors.attitude500Hz[YAW  ]);
                }

                if ( eepromConfig.activeTelemetry == 8 )
                {
               	    // Vertical Variables
            	    telemetryPrintF("%9.4f, %9.4f, %9.4f, %9.4f, %4ld\n", earthAxisAccels[ZAXIS],
            	    		                                              sensors.pressureAlt50Hz,
            	    		                                              hDotEstimate,
            	    		                                              hEstimate,
            	    		                                              ms5611Temperature);
                }

                if ( eepromConfig.activeTelemetry == 16 )
                {
               	    // Vertical Variables
            	    telemetryPrintF("%9.4f, %9.4f, %9.4f, %4ld, %1d, %9.4f, %9.4f\n", verticalVelocityCmd,
            	    		                                                          hDotEstimate,
            	    		                                                          hEstimate,
            	    		                                                          ms5611Temperature,
            	    		                                                          verticalModeState,
            	    		                                                          throttleCmd,
            	    		                                                          eepromConfig.PID[HDOT_PID].iTerm);
                }

            }

            executionTime100Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_5Hz)
        {
        	frame_5Hz = false;

        	currentTime     = micros();
			deltaTime5Hz    = currentTime - previous5HzTime;
			previous5HzTime = currentTime;

			gpsUpdated();

            if (eepromConfig.mavlinkEnabled == true)
            {
				mavlinkSendGpsRaw();
			}

			if (batMonVeryLowWarning > 0)
			{
				BEEP_TOGGLE;
				batMonVeryLowWarning--;
			}

			if (execUp == true)
			    LED0_TOGGLE;

			executionTime5Hz = micros() - currentTime;
        }

        ///////////////////////////////

        if (frame_1Hz)
        {
        	frame_1Hz = false;

        	currentTime     = micros();
			deltaTime1Hz    = currentTime - previous1HzTime;
			previous1HzTime = currentTime;

			if (execUp == false)
			    execUpCount++;

			if ((execUpCount == 5) && (execUp == false))
			{
			    execUp = true;

			    pwmEscInit();

			    homeData.magHeading = sensors.attitude500Hz[YAW];
			}

			if (batMonLowWarning > 0)
			{
				BEEP_TOGGLE;
				batMonLowWarning--;
			}

            if (eepromConfig.mavlinkEnabled == true)
            {
				mavlinkSendHeartbeat();
				mavlinkSendSysStatus();
			}

			executionTime1Hz = micros() - currentTime;
        }

        ////////////////////////////////
    }

    ///////////////////////////////////////////////////////////////////////////
}