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Merge branch 'altitudehold' into revolution_overo
Conflicts: flight/OpenPilot/UAVObjects.inc flight/Project/OpenPilotOSX/OpenPilotOSX.xcodeproj/project.pbxproj flight/Revolution/Makefile flight/Revolution/ins.c
This commit is contained in:
commit
49a03a868b
180
flight/Modules/AltitudeHold/altitudehold.c
Normal file
180
flight/Modules/AltitudeHold/altitudehold.c
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@ -0,0 +1,180 @@
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/**
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||||
******************************************************************************
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||||
*
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||||
* @file guidance.c
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||||
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
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* @brief This module compared @ref PositionActuatl to @ref ActiveWaypoint
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* and sets @ref AttitudeDesired. It only does this when the FlightMode field
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* of @ref ManualControlCommand is Auto.
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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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||||
* 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
|
||||
*/
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||||
|
||||
/**
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* Input object: ActiveWaypoint
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* Input object: PositionActual
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* Input object: ManualControlCommand
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* Output object: AttitudeDesired
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*
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* This module will periodically update the value of the AttitudeDesired object.
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*
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* The module executes in its own thread in this example.
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*
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||||
* Modules have no API, all communication to other modules is done through UAVObjects.
|
||||
* However modules may use the API exposed by shared libraries.
|
||||
* See the OpenPilot wiki for more details.
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||||
* http://www.openpilot.org/OpenPilot_Application_Architecture
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*
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||||
*/
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||||
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#include "openpilot.h"
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#include "altitudeholdsettings.h"
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#include "altitudeholddesired.h" // object that will be updated by the module
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#include "positionactual.h"
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#include "stabilizationdesired.h"
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// Private constants
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#define MAX_QUEUE_SIZE 1
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#define STACK_SIZE_BYTES 1024
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#define TASK_PRIORITY (tskIDLE_PRIORITY+2)
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// Private types
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|
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// Private variables
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static xTaskHandle altitudeHoldTaskHandle;
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static xQueueHandle queue;
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||||
|
||||
// Private functions
|
||||
static void altitudeHoldTask(void *parameters);
|
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static void SettingsUpdatedCb(UAVObjEvent * ev);
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||||
|
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/**
|
||||
* Initialise the module, called on startup
|
||||
* \returns 0 on success or -1 if initialisation failed
|
||||
*/
|
||||
int32_t AltitudeHoldStart()
|
||||
{
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// Start main task
|
||||
xTaskCreate(altitudeHoldTask, (signed char *)"AltitudeHold", STACK_SIZE_BYTES/4, NULL, TASK_PRIORITY, &altitudeHoldTaskHandle);
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||||
// TaskMonitorAdd(TASKINFO_RUNNING_GUIDANCE, guidanceTaskHandle);
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||||
|
||||
return 0;
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||||
}
|
||||
|
||||
/**
|
||||
* Initialise the module, called on startup
|
||||
* \returns 0 on success or -1 if initialisation failed
|
||||
*/
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int32_t AltitudeHoldInitialize()
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||||
{
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AltitudeHoldSettingsInitialize();
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AltitudeHoldDesiredInitialize();
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// Create object queue
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queue = xQueueCreate(MAX_QUEUE_SIZE, sizeof(UAVObjEvent));
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|
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// Listen for updates.
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AltitudeHoldDesiredConnectQueue(queue);
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||||
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AltitudeHoldSettingsConnectCallback(&SettingsUpdatedCb);
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||||
|
||||
return 0;
|
||||
}
|
||||
MODULE_INITCALL(AltitudeHoldInitialize, AltitudeHoldStart)
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||||
|
||||
static float throttleIntegral = 0;
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||||
|
||||
/**
|
||||
* Module thread, should not return.
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*/
|
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static void altitudeHoldTask(void *parameters)
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{
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AltitudeHoldSettingsData altitudeHoldSettings;
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||||
AltitudeHoldDesiredData altitudeHoldDesired;
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||||
PositionActualData positionActual;
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||||
StabilizationDesiredData stabilizationDesired;
|
||||
|
||||
portTickType thisTime;
|
||||
portTickType lastSysTime;
|
||||
UAVObjEvent ev;
|
||||
|
||||
// Force update of the settings
|
||||
SettingsUpdatedCb(&ev);
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||||
|
||||
// Main task loop
|
||||
lastSysTime = xTaskGetTickCount();
|
||||
while (1) {
|
||||
|
||||
// Wait until the AttitudeRaw object is updated, if a timeout then go to failsafe
|
||||
if ( xQueueReceive(queue, &ev, 100 / portTICK_RATE_MS) != pdTRUE )
|
||||
{
|
||||
// Todo: Add alarm if it should be running
|
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throttleIntegral = 0;
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continue;
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} else {
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||||
PositionActualGet(&positionActual);
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||||
StabilizationDesiredGet(&stabilizationDesired);
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||||
float dT;
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||||
|
||||
thisTime = xTaskGetTickCount();
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if(thisTime > lastSysTime) // reuse dt in case of wraparound
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dT = (thisTime - lastSysTime) / portTICK_RATE_MS / 1000.0f;
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lastSysTime = thisTime;
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|
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static float altitude;
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const float altitudeTau = 0.1;
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||||
|
||||
|
||||
// Flipping sign on error since altitude is "down"
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||||
float error = - (altitudeHoldDesired.Down - positionActual.Down);
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||||
static float
|
||||
throttleIntegral += error * altitudeHoldSettings.Ki * dT * 1000;
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||||
if(throttleIntegral > altitudeHoldSettings.ILimit)
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throttleIntegral = altitudeHoldSettings.ILimit;
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else if (throttleIntegral < 0)
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throttleIntegral = 0;
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stabilizationDesired.Throttle = error * altitudeHoldSettings.Kp + throttleIntegral;
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if(stabilizationDesired.Throttle > 1)
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stabilizationDesired.Throttle = 1;
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else if (stabilizationDesired.Throttle < 0)
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stabilizationDesired.Throttle = 0;
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_ROLL] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_PITCH] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_YAW] = STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK;
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stabilizationDesired.Roll = altitudeHoldDesired.Roll;
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||||
stabilizationDesired.Pitch = altitudeHoldDesired.Pitch;
|
||||
stabilizationDesired.Yaw = altitudeHoldDesired.Yaw;
|
||||
StabilizationDesiredSet(&stabilizationDesired);
|
||||
}
|
||||
|
||||
}
|
||||
}
|
||||
|
||||
static void SettingsUpdatedCb(UAVObjEvent * ev)
|
||||
{
|
||||
AltitudeHoldDesiredGet(&altitudeHoldDesired);
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||||
AltitudeHoldSettingsGet(&altitudeHoldSettings);
|
||||
|
||||
const float fakeDt = 0.0025;
|
||||
if(settings.GyroTau < 0.0001)
|
||||
gyro_alpha = 0; // not trusting this to resolve to 0
|
||||
else
|
||||
gyro_alpha = expf(-fakeDt / settings.GyroTau);
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||||
|
||||
}
|
31
flight/Modules/AltitudeHold/inc/altitudehold.h
Normal file
31
flight/Modules/AltitudeHold/inc/altitudehold.h
Normal file
@ -0,0 +1,31 @@
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||||
/**
|
||||
******************************************************************************
|
||||
*
|
||||
* @file examplemodperiodic.c
|
||||
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
|
||||
* @brief Example module to be used as a template for actual modules.
|
||||
*
|
||||
* @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
|
||||
*/
|
||||
#ifndef EXAMPLEMODPERIODIC_H
|
||||
#define EXAMPLEMODPERIODIC_H
|
||||
|
||||
int32_t ExampleModPeriodicInitialize();
|
||||
int32_t GuidanceInitialize(void);
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||||
#endif // EXAMPLEMODPERIODIC_H
|
@ -39,6 +39,7 @@ typedef enum {FLIGHTMODE_UNDEFINED = 0, FLIGHTMODE_MANUAL = 1, FLIGHTMODE_STABIL
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED1) ? FLIGHTMODE_STABILIZED : \
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED2) ? FLIGHTMODE_STABILIZED : \
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED3) ? FLIGHTMODE_STABILIZED : \
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD) ? FLIGHTMODE_GUIDANCE : \
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL) ? FLIGHTMODE_GUIDANCE : \
|
||||
(x == FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD) ? FLIGHTMODE_GUIDANCE : FLIGHTMODE_UNDEFINED \
|
||||
)
|
||||
|
@ -44,6 +44,8 @@
|
||||
#include "flightstatus.h"
|
||||
#include "accessorydesired.h"
|
||||
#include "receiveractivity.h"
|
||||
#include "altitudeholddesired.h"
|
||||
#include "positionactual.h"
|
||||
|
||||
// Private constants
|
||||
#if defined(PIOS_MANUAL_STACK_SIZE)
|
||||
@ -79,6 +81,7 @@ static portTickType lastSysTime;
|
||||
// Private functions
|
||||
static void updateActuatorDesired(ManualControlCommandData * cmd);
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||||
static void updateStabilizationDesired(ManualControlCommandData * cmd, ManualControlSettingsData * settings);
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||||
static void altitudeHoldDesired(ManualControlCommandData * cmd);
|
||||
static void processFlightMode(ManualControlSettingsData * settings, float flightMode);
|
||||
static void processArm(ManualControlCommandData * cmd, ManualControlSettingsData * settings);
|
||||
static void setArmedIfChanged(uint8_t val);
|
||||
@ -375,7 +378,13 @@ static void manualControlTask(void *parameters)
|
||||
updateStabilizationDesired(&cmd, &settings);
|
||||
break;
|
||||
case FLIGHTMODE_GUIDANCE:
|
||||
// TODO: Implement
|
||||
switch(flightStatus.FlightMode) {
|
||||
case FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD:
|
||||
altitudeHoldDesired(&cmd);
|
||||
break;
|
||||
default:
|
||||
AlarmsSet(SYSTEMALARMS_ALARM_MANUALCONTROL, SYSTEMALARMS_ALARM_CRITICAL);
|
||||
}
|
||||
break;
|
||||
}
|
||||
}
|
||||
@ -588,6 +597,47 @@ static void updateStabilizationDesired(ManualControlCommandData * cmd, ManualCon
|
||||
StabilizationDesiredSet(&stabilization);
|
||||
}
|
||||
|
||||
// TODO: Need compile flag to exclude this from copter control
|
||||
static void altitudeHoldDesired(ManualControlCommandData * cmd)
|
||||
{
|
||||
const float DEADBAND_HIGH = 0.55;
|
||||
const float DEADBAND_LOW = 0.45;
|
||||
|
||||
static portTickType lastSysTime;
|
||||
static bool zeroed = false;
|
||||
portTickType thisSysTime;
|
||||
float dT;
|
||||
AltitudeHoldDesiredData altitudeHoldDesired;
|
||||
AltitudeHoldDesiredGet(&altitudeHoldDesired);
|
||||
|
||||
StabilizationSettingsData stabSettings;
|
||||
StabilizationSettingsGet(&stabSettings);
|
||||
|
||||
thisSysTime = xTaskGetTickCount();
|
||||
if(thisSysTime > lastSysTime) // reuse dt in case of wraparound
|
||||
dT = (thisSysTime - lastSysTime) / portTICK_RATE_MS / 1000.0f;
|
||||
lastSysTime = thisSysTime;
|
||||
|
||||
altitudeHoldDesired.Roll = cmd->Roll * stabSettings.RollMax;
|
||||
altitudeHoldDesired.Pitch = cmd->Pitch * stabSettings.PitchMax;
|
||||
altitudeHoldDesired.Yaw = cmd->Yaw * stabSettings.ManualRate[STABILIZATIONSETTINGS_MANUALRATE_YAW];
|
||||
|
||||
float currentDown;
|
||||
PositionActualDownGet(¤tDown);
|
||||
if(dT > 1) {
|
||||
// After not being in this mode for a while init at current height
|
||||
altitudeHoldDesired.Down = currentDown;
|
||||
zeroed = false;
|
||||
} else if (cmd->Throttle > DEADBAND_HIGH && zeroed)
|
||||
altitudeHoldDesired.Down += (DEADBAND_HIGH - cmd->Throttle) * dT;
|
||||
else if (cmd->Throttle < DEADBAND_LOW && zeroed)
|
||||
altitudeHoldDesired.Down += (DEADBAND_LOW - cmd->Throttle) * dT;
|
||||
else if (cmd->Throttle >= DEADBAND_LOW && cmd->Throttle <= DEADBAND_HIGH) // Require the stick to enter the dead band before they can move height
|
||||
zeroed = true;
|
||||
|
||||
AltitudeHoldDesiredSet(&altitudeHoldDesired);
|
||||
}
|
||||
|
||||
/**
|
||||
* Convert channel from servo pulse duration (microseconds) to scaled -1/+1 range.
|
||||
*/
|
||||
|
@ -461,7 +461,7 @@ static void SettingsUpdatedCb(UAVObjEvent * ev)
|
||||
if(settings.GyroTau < 0.0001)
|
||||
gyro_alpha = 0; // not trusting this to resolve to 0
|
||||
else
|
||||
gyro_alpha = exp(-fakeDt / settings.GyroTau);
|
||||
gyro_alpha = expf(-fakeDt / settings.GyroTau);
|
||||
}
|
||||
|
||||
|
||||
|
@ -49,7 +49,7 @@ endif
|
||||
FLASH_TOOL = OPENOCD
|
||||
|
||||
# List of modules to include
|
||||
MODULES = Sensors Attitude/revolution ManualControl Stabilization Altitude/revolution Actuator GPS FirmwareIAP
|
||||
MODULES = Sensors Attitude/revolution ManualControl Stabilization Altitude/revolution Actuator GPS FirmwareIAP AltitudeHold
|
||||
MODULES += Telemetry
|
||||
MODULES += OveroSync
|
||||
PYMODULES =
|
||||
|
@ -75,6 +75,8 @@ UAVOBJSRCFILENAMES += hwsettings
|
||||
UAVOBJSRCFILENAMES += receiveractivity
|
||||
UAVOBJSRCFILENAMES += cameradesired
|
||||
UAVOBJSRCFILENAMES += camerastabsettings
|
||||
UAVOBJSRCFILENAMES += altitudeholdsettings
|
||||
UAVOBJSRCFILENAMES += altitudeholddesired
|
||||
|
||||
UAVOBJSRC = $(foreach UAVOBJSRCFILE,$(UAVOBJSRCFILENAMES),$(UAVOBJSYNTHDIR)/$(UAVOBJSRCFILE).c )
|
||||
UAVOBJDEFINE = $(foreach UAVOBJSRCFILE,$(UAVOBJSRCFILENAMES),-DUAVOBJ_INIT_$(UAVOBJSRCFILE) )
|
||||
|
@ -26,6 +26,9 @@ OTHER_FILES += UAVObjects.pluginspec
|
||||
HEADERS += $$UAVOBJECT_SYNTHETICS/accessorydesired.h \
|
||||
$$UAVOBJECT_SYNTHETICS/baroaltitude.h \
|
||||
$$UAVOBJECT_SYNTHETICS/attitudeactual.h \
|
||||
$$UAVOBJECT_SYNTHETICS/altitudeholddesired.h \
|
||||
$$UAVOBJECT_SYNTHETICS/altitudeholdsettings.h \
|
||||
$$UAVOBJECT_SYNTHETICS/inssettings.h \
|
||||
$$UAVOBJECT_SYNTHETICS/revocalibration.h \
|
||||
$$UAVOBJECT_SYNTHETICS/gcstelemetrystats.h \
|
||||
$$UAVOBJECT_SYNTHETICS/gyros.h \
|
||||
@ -80,6 +83,9 @@ HEADERS += $$UAVOBJECT_SYNTHETICS/accessorydesired.h \
|
||||
SOURCES += $$UAVOBJECT_SYNTHETICS/accessorydesired.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/baroaltitude.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/attitudeactual.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/altitudeholddesired.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/altitudeholdsettings.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/inssettings.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/revocalibration.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/gcstelemetrystats.cpp \
|
||||
$$UAVOBJECT_SYNTHETICS/accels.cpp \
|
||||
|
13
shared/uavobjectdefinition/altitudeholddesired.xml
Normal file
13
shared/uavobjectdefinition/altitudeholddesired.xml
Normal file
@ -0,0 +1,13 @@
|
||||
<xml>
|
||||
<object name="AltitudeHoldDesired" singleinstance="true" settings="false">
|
||||
<description>Holds the desired altitude (from manual control) as well as the desired attitude to pass through</description>
|
||||
<field name="Down" units="m" type="float" elements="1"/>
|
||||
<field name="Roll" units="deg" type="float" elements="1"/>
|
||||
<field name="Pitch" units="deg" type="float" elements="1"/>
|
||||
<field name="Yaw" units="deg/s" type="float" elements="1"/>
|
||||
<access gcs="readwrite" flight="readwrite"/>
|
||||
<telemetrygcs acked="false" updatemode="manual" period="0"/>
|
||||
<telemetryflight acked="false" updatemode="onchange" period="0"/>
|
||||
<logging updatemode="periodic" period="1000"/>
|
||||
</object>
|
||||
</xml>
|
13
shared/uavobjectdefinition/altitudeholdsettings.xml
Normal file
13
shared/uavobjectdefinition/altitudeholdsettings.xml
Normal file
@ -0,0 +1,13 @@
|
||||
<xml>
|
||||
<object name="AltitudeHoldSettings" singleinstance="true" settings="true">
|
||||
<description>Settings for the @ref AltitudeHold module</description>
|
||||
<field name="Kp" units="throttle/m" type="float" elements="1" defaultvalue="0.025"/>
|
||||
<field name="Ki" units="throttle/m" type="float" elements="1" defaultvalue="0.025"/>
|
||||
<field name="Kd" units="throttle/m" type="float" elements="1" defaultvalue="0.25"/>
|
||||
<field name="AltitudeTau" units="s" type="float" elements="1" defaultvalue="0.1"/>
|
||||
<access gcs="readwrite" flight="readwrite"/>
|
||||
<telemetrygcs acked="true" updatemode="onchange" period="0"/>
|
||||
<telemetryflight acked="true" updatemode="onchange" period="0"/>
|
||||
<logging updatemode="never" period="0"/>
|
||||
</object>
|
||||
</xml>
|
@ -4,7 +4,7 @@
|
||||
<field name="Armed" units="" type="enum" elements="1" options="Disarmed,Arming,Armed" defaultvalue="Disarmed"/>
|
||||
|
||||
<!-- Note these enumerated values should be the same as ManualControlSettings -->
|
||||
<field name="FlightMode" units="" type="enum" elements="1" options="Manual,Stabilized1,Stabilized2,Stabilized3,VelocityControl,PositionHold"/>
|
||||
<field name="FlightMode" units="" type="enum" elements="1" options="Manual,Stabilized1,Stabilized2,Stabilized3,AltitudeHold,VelocityControl,PositionHold"/>
|
||||
|
||||
<access gcs="readwrite" flight="readwrite"/>
|
||||
<telemetrygcs acked="false" updatemode="manual" period="0"/>
|
||||
|
@ -21,7 +21,7 @@
|
||||
<field name="Stabilization3Settings" units="" type="enum" elementnames="Roll,Pitch,Yaw" options="None,Rate,Attitude,AxisLock,WeakLeveling" defaultvalue="Attitude,Attitude,Rate"/>
|
||||
|
||||
<!-- Note these options values should be identical to those defined in FlightMode -->
|
||||
<field name="FlightModePosition" units="" type="enum" elements="3" options="Manual,Stabilized1,Stabilized2,Stabilized3,VelocityControl,PositionHold" defaultvalue="Manual,Stabilized1,Stabilized2"/>
|
||||
<field name="FlightModePosition" units="" type="enum" elements="3" options="Manual,Stabilized1,Stabilized2,Stabilized3,AltitudeHold,VelocityControl,PositionHold" defaultvalue="Manual,Stabilized1,Stabilized2"/>
|
||||
|
||||
<field name="ArmedTimeout" units="ms" type="uint16" elements="1" defaultvalue="30000"/>
|
||||
<access gcs="readwrite" flight="readwrite"/>
|
||||
|
Loading…
Reference in New Issue
Block a user