LibrePilot/flight/Modules/Actuator/actuator.c

/**
 ******************************************************************************
 * @addtogroup OpenPilotModules OpenPilot Modules
 * @{
 * @addtogroup ActuatorModule Actuator Module
 * @brief Compute servo/motor settings based on @ref ActuatorDesired "desired actuator positions" and aircraft type.
 * This is where all the mixing of channels is computed.
 * @{
 *
 * @file       actuator.c
 * @author     The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
 * @brief      Actuator module. Drives the actuators (servos, motors etc).
 *
 * @see        The GNU Public License (GPL) Version 3
 *
 *****************************************************************************/
/*
 * This program is free software; you can redistribute it and/or modify
 * it under the terms of the GNU General Public License as published by
 * the Free Software Foundation; either version 3 of the License, or
 * (at your option) any later version.
 *
 * This program is distributed in the hope that it will be useful, but
 * WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
 * or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
 * for more details.
 *
 * You should have received a copy of the GNU General Public License along
 * with this program; if not, write to the Free Software Foundation, Inc.,
 * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
 */


#include "openpilot.h"
#include "actuator.h"
#include "actuatorsettings.h"
#include "systemsettings.h"
#include "actuatordesired.h"
#include "actuatorcommand.h"
#include "manualcontrolcommand.h"
#include "mixersettings.h"
#include "mixerstatus.h"


// Private constants
#define MAX_QUEUE_SIZE 2

#if defined(PIOS_ACTUATOR_STACK_SIZE)
#define STACK_SIZE_BYTES PIOS_ACTUATOR_STACK_SIZE
#else
#define STACK_SIZE_BYTES 1312
#endif

#define TASK_PRIORITY (tskIDLE_PRIORITY+4)
#define FAILSAFE_TIMEOUT_MS 100
#define MAX_MIX_ACTUATORS ACTUATORCOMMAND_CHANNEL_NUMELEM

// Private types


// Private variables
static xQueueHandle queue;
static xTaskHandle taskHandle;

static float lastResult[MAX_MIX_ACTUATORS]={0,0,0,0,0,0,0,0};
static float lastFilteredResult[MAX_MIX_ACTUATORS]={0,0,0,0,0,0,0,0};
static float filterAccumulator[MAX_MIX_ACTUATORS]={0,0,0,0,0,0,0,0};


// Private functions
static void actuatorTask(void* parameters);
static void actuator_update_rate(UAVObjEvent *);
static int16_t scaleChannel(float value, int16_t max, int16_t min, int16_t neutral);
static void setFailsafe();
static float MixerCurve(const float throttle, const float* curve);
static bool set_channel(uint8_t mixer_channel, uint16_t value);

float ProcessMixer(const int index, const float curve1, const float curve2,
		   MixerSettingsData* mixerSettings, ActuatorDesiredData* desired,
		   const float period);

//this structure is equivalent to the UAVObjects for one mixer.
typedef struct {
	uint8_t type;
	int8_t matrix[5];
} __attribute__((packed)) Mixer_t;


/**
 * @brief Module initialization
 * @return 0
 */
int32_t ActuatorInitialize()
{
	// Create object queue
	queue = xQueueCreate(MAX_QUEUE_SIZE, sizeof(UAVObjEvent));

	// Listen for ExampleObject1 updates
	ActuatorDesiredConnectQueue(queue);
	
	// If settings change, update the output rate
	ActuatorSettingsConnectCallback(actuator_update_rate);
	
	// Start main task
	xTaskCreate(actuatorTask, (signed char*)"Actuator", STACK_SIZE_BYTES/4, NULL, TASK_PRIORITY, &taskHandle);
	TaskMonitorAdd(TASKINFO_RUNNING_ACTUATOR, taskHandle);
	PIOS_WDG_RegisterFlag(PIOS_WDG_ACTUATOR);
	
	return 0;
}

/**
 * @brief Main Actuator module task
 *
 * Universal matrix based mixer for VTOL, helis and fixed wing.
 * Converts desired roll,pitch,yaw and throttle to servo/ESC outputs.
 *
 * Because of how the Throttle ranges from 0 to 1, the motors should too!
 *
 * Note this code depends on the UAVObjects for the mixers being all being the same
 * and in sequence. If you change the object definition, make sure you check the code!
 *
 * @return -1 if error, 0 if success
 */
static void actuatorTask(void* parameters)
{
	UAVObjEvent ev;
	portTickType lastSysTime;
	portTickType thisSysTime;
	float dT = 0.0f;
	ActuatorCommandData command;
	ActuatorSettingsData settings;

	SystemSettingsData sysSettings;
	MixerSettingsData mixerSettings;
	ActuatorDesiredData desired;
	MixerStatusData mixerStatus;
	ManualControlCommandData manualControl;
	
	ActuatorSettingsGet(&settings);
	PIOS_Servo_SetHz(&settings.ChannelUpdateFreq[0], ACTUATORSETTINGS_CHANNELUPDATEFREQ_NUMELEM);

	float * status = (float *)&mixerStatus; //access status objects as an array of floats

	// Go to the neutral (failsafe) values until an ActuatorDesired update is received
	setFailsafe();

	// Main task loop
	lastSysTime = xTaskGetTickCount();
	while (1)
	{		
		PIOS_WDG_UpdateFlag(PIOS_WDG_ACTUATOR);

		// Wait until the ActuatorDesired object is updated, if a timeout then go to failsafe
		if ( xQueueReceive(queue, &ev, FAILSAFE_TIMEOUT_MS / portTICK_RATE_MS) != pdTRUE )
		{
			setFailsafe();
			continue;
		}

		// Check how long since last update
		thisSysTime = xTaskGetTickCount();
		if(thisSysTime > lastSysTime) // reuse dt in case of wraparound
			dT = (thisSysTime - lastSysTime) / portTICK_RATE_MS / 1000.0f;
		lastSysTime = thisSysTime;


		ManualControlCommandGet(&manualControl);
		SystemSettingsGet(&sysSettings);
		MixerStatusGet(&mixerStatus);
		MixerSettingsGet (&mixerSettings);
		ActuatorDesiredGet(&desired);
		ActuatorCommandGet(&command);
		ActuatorSettingsGet(&settings);

		int nMixers = 0;
		Mixer_t * mixers = (Mixer_t *)&mixerSettings.Mixer1Type;
		for(int ct=0; ct < MAX_MIX_ACTUATORS; ct++)
		{
			if(mixers[ct].type != MIXERSETTINGS_MIXER1TYPE_DISABLED)
			{
				nMixers ++;
			}
		}
		if(nMixers < 2) //Nothing can fly with less than two mixers.
		{
			AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_WARNING);
			continue;
		}

		AlarmsClear(SYSTEMALARMS_ALARM_ACTUATOR);

		bool armed = manualControl.Armed == MANUALCONTROLCOMMAND_ARMED_TRUE;
		armed &= desired.Throttle > 0.00; //zero throttle stops the motors

		float curve1 = MixerCurve(desired.Throttle,mixerSettings.ThrottleCurve1);
		float curve2 = MixerCurve(desired.Throttle,mixerSettings.ThrottleCurve2);
		for(int ct=0; ct < MAX_MIX_ACTUATORS; ct++)
		{
			if(mixers[ct].type != MIXERSETTINGS_MIXER1TYPE_DISABLED)
			{
				status[ct] = ProcessMixer(ct, curve1, curve2, &mixerSettings, &desired, dT);

				if(!armed &&
				   mixers[ct].type == MIXERSETTINGS_MIXER1TYPE_MOTOR)
				{
					command.Channel[ct] = settings.ChannelMin[ct]; //force zero throttle
					filterAccumulator[ct] = 0;
					lastResult[ct] = 0;
				}else
				{
					// For motors when armed keep above neutral
					if((mixers[ct].type == MIXERSETTINGS_MIXER1TYPE_MOTOR) && (status[ct] < 0)) 
						status[ct] = 0;
						
					command.Channel[ct] = scaleChannel(status[ct],
									   settings.ChannelMax[ct],
									   settings.ChannelMin[ct],
									   settings.ChannelNeutral[ct]);
				}
			}
		}
		MixerStatusSet(&mixerStatus);

		// Store update time
		command.UpdateTime = 1000*dT;
		if(1000*dT > command.MaxUpdateTime)
			command.MaxUpdateTime = 1000*dT;
		
		// Update output object
		ActuatorCommandSet(&command);
		// Update in case read only (eg. during servo configuration)
		ActuatorCommandGet(&command);

		// Update servo outputs
		bool success = true;
		
		for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
		{
			success &= set_channel(n, command.Channel[n]);
		}

		if(!success) {
			command.NumFailedUpdates++;
			ActuatorCommandSet(&command);
			AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL); 
		}

	}
}



/**
 *Process mixing for one actuator
 */

float ProcessMixer(const int index, const float curve1, const float curve2,
		   MixerSettingsData* mixerSettings, ActuatorDesiredData* desired, const float period)
{
	Mixer_t * mixers = (Mixer_t *)&mixerSettings->Mixer1Type; //pointer to array of mixers in UAVObjects
	Mixer_t * mixer = &mixers[index];
	float result = ((mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_THROTTLECURVE1] / 128.0f) * curve1) +
	((mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_THROTTLECURVE2] / 128.0f) * curve2) +
	((mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_ROLL] / 128.0f) * desired->Roll) +
	((mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_PITCH] / 128.0f) * desired->Pitch) +
	((mixer->matrix[MIXERSETTINGS_MIXER1VECTOR_YAW] / 128.0f) * desired->Yaw);
	if(mixer->type == MIXERSETTINGS_MIXER1TYPE_MOTOR)
	{
		if(result < 0) //idle throttle
		{
			result = 0;
		}

		//feed forward
		float accumulator = filterAccumulator[index];
		accumulator += (result - lastResult[index]) * mixerSettings->FeedForward;
		lastResult[index] = result;
		result += accumulator;
		if(period !=0)
		{
			if(accumulator > 0)
			{
				float filter = mixerSettings->AccelTime / period;
				if(filter <1)
				{
					filter = 1;
				}
				accumulator -= accumulator / filter;
			}else
			{
				float filter = mixerSettings->DecelTime / period;
				if(filter <1)
				{
					filter = 1;
				}
				accumulator -= accumulator / filter;
			}
		}
		filterAccumulator[index] = accumulator;
		result += accumulator;

		//acceleration limit
		float dt = result - lastFilteredResult[index];
		float maxDt = mixerSettings->MaxAccel * period;
		if(dt > maxDt) //we are accelerating too hard
		{
			result = lastFilteredResult[index] + maxDt;
		}
		lastFilteredResult[index] = result;
	}
	return(result);
}


/**
 *Interpolate a throttle curve. Throttle input should be in the range 0 to 1.
 *Output is in the range 0 to 1.
 */

#define MIXER_CURVE_ENTRIES 5

static float MixerCurve(const float throttle, const float* curve)
{
	float scale = throttle * MIXER_CURVE_ENTRIES;
	int idx1 = scale;
	scale -= (float)idx1; //remainder
	if(curve[0] < -1)
	{
		return(throttle);
	}
	if (idx1 < 0)
	{
		idx1 = 0; //clamp to lowest entry in table
		scale = 0;
	}
	int idx2 = idx1 + 1;
	if(idx2 >= MIXER_CURVE_ENTRIES)
	{
		idx2 = MIXER_CURVE_ENTRIES -1; //clamp to highest entry in table
		if(idx1 >= MIXER_CURVE_ENTRIES)
		{
			idx1 = MIXER_CURVE_ENTRIES -1;
		}
	}
	return((curve[idx1] * (1 - scale)) + (curve[idx2] * scale));
}


/**
 * Convert channel from -1/+1 to servo pulse duration in microseconds
 */
static int16_t scaleChannel(float value, int16_t max, int16_t min, int16_t neutral)
{
	int16_t valueScaled;
	// Scale
	if ( value >= 0.0)
	{
		valueScaled = (int16_t)(value*((float)(max-neutral))) + neutral;
	}
	else
	{
		valueScaled = (int16_t)(value*((float)(neutral-min))) + neutral;
	}

	if (max>min)
	{
		if( valueScaled > max ) valueScaled = max;
		if( valueScaled < min ) valueScaled = min;
	}
	else
	{
		if( valueScaled < max ) valueScaled = max;
		if( valueScaled > min ) valueScaled = min;
	}

	return valueScaled;
}

/**
 * Set actuator output to the neutral values (failsafe)
 */
static void setFailsafe()
{
	ActuatorCommandData command;
	ActuatorSettingsData settings;

	ActuatorCommandGet(&command);
	ActuatorSettingsGet(&settings);

	MixerSettingsData mixerSettings;
	MixerSettingsGet (&mixerSettings);
	Mixer_t * mixers = (Mixer_t *)&mixerSettings.Mixer1Type; //pointer to array of mixers in UAVObjects

	// Reset ActuatorCommand to safe values
	for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
	{
		if(mixers[n].type == MIXERSETTINGS_MIXER1TYPE_MOTOR)
		{
			command.Channel[n] = settings.ChannelMin[n];
		}
		else
		{
			command.Channel[n] = settings.ChannelNeutral[n];
		}
	}

	// Set alarm
	AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL);

	// Update servo outputs
	for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
	{
		set_channel(n, command.Channel[n]);
	}

	// Update output object
	ActuatorCommandSet(&command);
}


/**
 * @brief Update the servo update rate
 */
static void actuator_update_rate(UAVObjEvent * ev)
{
	ActuatorSettingsData settings;
	if ( ev->obj == ActuatorSettingsHandle() ) {
		ActuatorSettingsGet(&settings);		
		PIOS_Servo_SetHz(&settings.ChannelUpdateFreq[0], ACTUATORSETTINGS_CHANNELUPDATEFREQ_NUMELEM);
	}
}

#if defined(ARCH_POSIX) || defined(ARCH_WIN32)
static bool set_channel(uint8_t mixer_channel, uint16_t value) {
	return true;
}
#else
static bool set_channel(uint8_t mixer_channel, uint16_t value) {
	
	ActuatorSettingsData settings;
	ActuatorSettingsGet(&settings);
		
	switch(settings.ChannelType[mixer_channel]) {
		case ACTUATORSETTINGS_CHANNELTYPE_PWM:
			PIOS_Servo_Set(settings.ChannelAddr[mixer_channel], value);
			return true;
#if defined(PIOS_INCLUDE_I2C_ESC)
		case ACTUATORSETTINGS_CHANNELTYPE_MK: 
		{
			ManualControlCommandData manual;
			ManualControlCommandGet(&manual);
			/* Unfortunately MK controller take forever to start so keep */
			/* them spinning when armed */			 
			if(manual.Armed)
				value = (value < 0) ? 1 : value;
			else 
				value = 0;

			return PIOS_SetMKSpeed(settings.ChannelAddr[mixer_channel],value);
			break;
		}
		case ACTUATORSETTINGS_CHANNELTYPE_ASTEC4:
			return PIOS_SetAstec4Speed(settings.ChannelAddr[mixer_channel],value);
			break;
#endif
		default:
			return false;
	}			
	
	return false;
	
}
#endif


/**
 * @}
 * @}
 */