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https://bitbucket.org/librepilot/librepilot.git
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d928676f5e
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1121 ebee16cc-31ac-478f-84a7-5cbb03baadba
290 lines
9.5 KiB
C
290 lines
9.5 KiB
C
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup ActuatorModule Actuator Module
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* @brief Compute servo/motor settings based on @ref ActuatorDesired "desired actuator positions" and aircraft type.
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* This is where all the mixing of channels is computed.
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* @{
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*
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* @file actuator.c
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
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* @brief Actuator module. Drives the actuators (servos, motors etc).
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*
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* @see The GNU Public License (GPL) Version 3
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*
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*****************************************************************************/
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/*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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#include "openpilot.h"
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#include "actuator.h"
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#include "actuatorsettings.h"
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#include "systemsettings.h"
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#include "actuatordesired.h"
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#include "actuatorcommand.h"
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// Private constants
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#define MAX_QUEUE_SIZE 2
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#define STACK_SIZE configMINIMAL_STACK_SIZE
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#define TASK_PRIORITY (tskIDLE_PRIORITY+4)
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#define FAILSAFE_TIMEOUT_MS 100
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// Private types
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// Private variables
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static xQueueHandle queue;
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static xTaskHandle taskHandle;
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// Private functions
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static void actuatorTask(void* parameters);
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static int32_t mixerFixedWing(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd);
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static int32_t mixerFixedWingElevon(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd);
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static int32_t mixerVTOL(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd);
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static int16_t scaleChannel(float value, int16_t max, int16_t min, int16_t neutral);
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static void setFailsafe();
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/**
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* @brief Module initialization
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* @return 0
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*/
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int32_t ActuatorInitialize()
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{
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// Create object queue
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queue = xQueueCreate(MAX_QUEUE_SIZE, sizeof(UAVObjEvent));
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// Listen for ExampleObject1 updates
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ActuatorDesiredConnectQueue(queue);
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// Start main task
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xTaskCreate(actuatorTask, (signed char*)"Actuator", STACK_SIZE, NULL, TASK_PRIORITY, &taskHandle);
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return 0;
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}
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/**
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* @brief Main module task
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*/
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static void actuatorTask(void* parameters)
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{
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UAVObjEvent ev;
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ActuatorSettingsData settings;
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SystemSettingsData sysSettings;
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ActuatorDesiredData desired;
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ActuatorCommandData cmd;
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// Set servo update frequency (done only on start-up)
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ActuatorSettingsGet(&settings);
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PIOS_Servo_SetHz(settings.ChannelUpdateFreq[0], settings.ChannelUpdateFreq[1]);
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// Go to the neutral (failsafe) values until an ActuatorDesired update is received
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setFailsafe();
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// Main task loop
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while (1)
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{
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// Wait until the ActuatorDesired object is updated, if a timeout then go to failsafe
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if ( xQueueReceive(queue, &ev, FAILSAFE_TIMEOUT_MS / portTICK_RATE_MS) != pdTRUE )
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{
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setFailsafe();
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continue;
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}
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// Read settings
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ActuatorSettingsGet(&settings);
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SystemSettingsGet(&sysSettings);
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// Reset ActuatorCommand to neutral values
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for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
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{
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cmd.Channel[n] = settings.ChannelNeutral[n];
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}
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// Read input object
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ActuatorDesiredGet(&desired);
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// Call appropriate mixer depending on the airframe configuration
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if ( sysSettings.AirframeType == SYSTEMSETTINGS_AIRFRAMETYPE_FIXEDWING )
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{
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if ( mixerFixedWing(&settings, &desired, &cmd) == -1 )
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{
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AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL);
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}
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else
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{
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AlarmsClear(SYSTEMALARMS_ALARM_ACTUATOR);
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}
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}
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else if ( sysSettings.AirframeType == SYSTEMSETTINGS_AIRFRAMETYPE_FIXEDWINGELEVON )
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{
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if ( mixerFixedWingElevon(&settings, &desired, &cmd) == -1 )
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{
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AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL);
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}
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else
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{
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AlarmsClear(SYSTEMALARMS_ALARM_ACTUATOR);
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}
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}
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else if ( sysSettings.AirframeType == SYSTEMSETTINGS_AIRFRAMETYPE_VTOL )
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{
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if ( mixerVTOL(&settings, &desired, &cmd) == -1 )
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{
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AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL);
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}
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else
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{
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AlarmsClear(SYSTEMALARMS_ALARM_ACTUATOR);
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}
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}
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// Update servo outputs
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for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
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{
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PIOS_Servo_Set( n, cmd.Channel[n] );
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}
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// Update output object
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ActuatorCommandSet(&cmd);
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}
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}
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/**
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* Mixer for Fixed Wing airframes. Converts desired roll,pitch,yaw and throttle to servo outputs.
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* @return -1 if error, 0 if success
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*/
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static int32_t mixerFixedWing(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd)
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{
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// Check settings
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if ( settings->FixedWingPitch1 == ACTUATORSETTINGS_FIXEDWINGPITCH1_NONE ||
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settings->FixedWingRoll1 == ACTUATORSETTINGS_FIXEDWINGROLL1_NONE ||
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settings->FixedWingThrottle == ACTUATORSETTINGS_FIXEDWINGTHROTTLE_NONE )
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{
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return -1;
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}
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// Set pitch servo command
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cmd->Channel[ settings->FixedWingPitch1 ] = scaleChannel(desired->Pitch, settings->ChannelMax[ settings->FixedWingPitch1 ],
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settings->ChannelMin[ settings->FixedWingPitch1 ],
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settings->ChannelNeutral[ settings->FixedWingPitch1 ]);
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if ( settings->FixedWingPitch2 != ACTUATORSETTINGS_FIXEDWINGPITCH2_NONE )
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{
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cmd->Channel[ settings->FixedWingPitch2 ] = scaleChannel(desired->Pitch, settings->ChannelMax[ settings->FixedWingPitch2 ],
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settings->ChannelMin[ settings->FixedWingPitch2 ],
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settings->ChannelNeutral[ settings->FixedWingPitch2 ]);
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}
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// Set roll servo command
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cmd->Channel[ settings->FixedWingRoll1 ] = scaleChannel(desired->Roll, settings->ChannelMax[ settings->FixedWingRoll1 ],
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settings->ChannelMin[ settings->FixedWingRoll1 ],
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settings->ChannelNeutral[ settings->FixedWingRoll1 ]);
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if ( settings->FixedWingRoll2 != ACTUATORSETTINGS_FIXEDWINGROLL2_NONE )
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{
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cmd->Channel[ settings->FixedWingRoll2 ] = scaleChannel(desired->Roll, settings->ChannelMax[ settings->FixedWingRoll2 ],
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settings->ChannelMin[ settings->FixedWingRoll2 ],
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settings->ChannelNeutral[ settings->FixedWingRoll2 ]);
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}
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// Set yaw servo command
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if ( settings->FixedWingYaw != ACTUATORSETTINGS_FIXEDWINGYAW_NONE )
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{
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cmd->Channel[ settings->FixedWingYaw ] = scaleChannel(desired->Yaw, settings->ChannelMax[ settings->FixedWingYaw ],
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settings->ChannelMin[ settings->FixedWingYaw ],
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settings->ChannelNeutral[ settings->FixedWingYaw ]);
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}
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// Set throttle servo command
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cmd->Channel[ settings->FixedWingThrottle ] = scaleChannel(desired->Throttle, settings->ChannelMax[ settings->FixedWingThrottle ],
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settings->ChannelMin[ settings->FixedWingThrottle ],
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settings->ChannelNeutral[ settings->FixedWingThrottle ]);
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// Done
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return 0;
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}
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/**
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* Mixer for Fixed Wing airframes with elevons. Converts desired roll,pitch,yaw and throttle to servo outputs.
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* @return -1 if error, 0 if success
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*/
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static int32_t mixerFixedWingElevon(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd)
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{
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// TODO: Implement elevon mixer
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return -1;
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}
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/**
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* Mixer for VTOL (quads and octo copters). Converts desired roll,pitch,yaw and throttle to servo outputs.
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* @return -1 if error, 0 if success
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*/
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static int32_t mixerVTOL(const ActuatorSettingsData* settings, const ActuatorDesiredData* desired, ActuatorCommandData* cmd)
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{
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// TODO: Implement VTOL mixer
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return -1;
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}
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/**
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* Convert channel from -1/+1 to servo pulse duration in microseconds
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*/
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static int16_t scaleChannel(float value, int16_t max, int16_t min, int16_t neutral)
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{
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int16_t valueScaled;
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// Scale
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if ( value >= 0.0)
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{
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valueScaled = (int16_t)(value*((float)(max-neutral))) + neutral;
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}
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else
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{
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valueScaled = (int16_t)(value*((float)(neutral-min))) + neutral;
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}
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return valueScaled;
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}
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/**
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* Set actuator output to the neutral values (failsafe)
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*/
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static void setFailsafe()
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{
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ActuatorSettingsData settings;
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ActuatorCommandData cmd;
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// Read settings
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ActuatorSettingsGet(&settings);
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// Reset ActuatorCommand to neutral values
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for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
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{
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cmd.Channel[n] = settings.ChannelNeutral[n];
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}
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// Set alarm
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AlarmsSet(SYSTEMALARMS_ALARM_ACTUATOR, SYSTEMALARMS_ALARM_CRITICAL);
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// Update servo outputs
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for (int n = 0; n < ACTUATORCOMMAND_CHANNEL_NUMELEM; ++n)
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{
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PIOS_Servo_Set( n, cmd.Channel[n] );
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}
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// Update output object
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ActuatorCommandSet(&cmd);
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}
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/**
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* @}
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* @}
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*/
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