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304 lines
11 KiB
C++
304 lines
11 KiB
C++
/*
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******************************************************************************
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*
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* @file grounddrivecontroller.cpp
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2015.
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* @brief Ground drive controller
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* the required PathDesired LAND mode.
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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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extern "C" {
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#include <openpilot.h>
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#include <callbackinfo.h>
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#include <math.h>
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#include <pid.h>
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#include <CoordinateConversions.h>
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#include <sin_lookup.h>
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#include <pathdesired.h>
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#include <paths.h>
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#include "plans.h"
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#include <sanitycheck.h>
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#include <homelocation.h>
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#include <accelstate.h>
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#include <groundpathfollowersettings.h>
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#include <flightstatus.h>
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#include <flightmodesettings.h>
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#include <pathstatus.h>
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#include <positionstate.h>
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#include <velocitystate.h>
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#include <velocitydesired.h>
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#include <stabilizationdesired.h>
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#include <airspeedstate.h>
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#include <attitudestate.h>
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#include <takeofflocation.h>
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#include <poilocation.h>
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#include <manualcontrolcommand.h>
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#include <systemsettings.h>
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#include <stabilizationbank.h>
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#include <stabilizationdesired.h>
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#include <pathsummary.h>
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#include <statusgrounddrive.h>
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}
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// C++ includes
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#include "grounddrivecontroller.h"
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// Private constants
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// pointer to a singleton instance
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GroundDriveController *GroundDriveController::p_inst = 0;
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GroundDriveController::GroundDriveController()
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: groundSettings(0), mActive(false), mMode(0)
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{}
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// Called when mode first engaged
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void GroundDriveController::Activate(void)
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{
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if (!mActive) {
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mActive = true;
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SettingsUpdated();
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controlNE.Activate();
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mMode = pathDesired->Mode;
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}
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}
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uint8_t GroundDriveController::IsActive(void)
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{
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return mActive;
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}
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uint8_t GroundDriveController::Mode(void)
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{
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return mMode;
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}
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// Objective updated in pathdesired
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void GroundDriveController::ObjectiveUpdated(void)
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{}
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void GroundDriveController::Deactivate(void)
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{
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if (mActive) {
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mActive = false;
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controlNE.Deactivate();
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}
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}
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void GroundDriveController::SettingsUpdated(void)
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{
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const float dT = groundSettings->UpdatePeriod / 1000.0f;
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controlNE.UpdatePositionalParameters(groundSettings->HorizontalPosP);
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controlNE.UpdateParameters(groundSettings->SpeedPI.Kp,
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groundSettings->SpeedPI.Ki,
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groundSettings->SpeedPI.Kd,
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groundSettings->SpeedPI.Beta,
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dT,
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groundSettings->HorizontalVelMax);
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// max/min are NE command values equivalent to thrust but must be symmetrical as this is NE not forward/reverse.
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controlNE.UpdateCommandParameters(-groundSettings->ThrustLimit.Max, groundSettings->ThrustLimit.Max, groundSettings->VelocityFeedForward);
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}
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/**
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* Initialise the module, called on startup
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* \returns 0 on success or -1 if initialisation failed
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*/
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int32_t GroundDriveController::Initialize(GroundPathFollowerSettingsData *ptr_groundSettings)
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{
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PIOS_Assert(ptr_groundSettings);
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groundSettings = ptr_groundSettings;
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return 0;
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}
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void GroundDriveController::UpdateAutoPilot()
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{
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uint8_t result = updateAutoPilotGround();
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if (result) {
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_OK);
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} else {
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pathStatus->Status = PATHSTATUS_STATUS_CRITICAL;
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AlarmsSet(SYSTEMALARMS_ALARM_GUIDANCE, SYSTEMALARMS_ALARM_WARNING);
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}
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PathStatusSet(pathStatus);
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}
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/**
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* fixed wing autopilot:
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* straight forward:
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* 1. update path velocity for limited motion crafts
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* 2. update attitude according to default fixed wing pathfollower algorithm
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*/
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uint8_t GroundDriveController::updateAutoPilotGround()
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{
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updatePathVelocity(groundSettings->CourseFeedForward);
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return updateGroundDesiredAttitude();
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}
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/**
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* Compute desired velocity from the current position and path
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*/
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void GroundDriveController::updatePathVelocity(float kFF)
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{
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PositionStateData positionState;
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PositionStateGet(&positionState);
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VelocityStateData velocityState;
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VelocityStateGet(&velocityState);
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VelocityDesiredData velocityDesired;
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controlNE.UpdateVelocityState(velocityState.North, velocityState.East);
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// look ahead kFF seconds
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float cur[3] = { positionState.North + (velocityState.North * kFF),
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positionState.East + (velocityState.East * kFF),
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positionState.Down + (velocityState.Down * kFF) };
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struct path_status progress;
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path_progress(pathDesired, cur, &progress, false);
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// GOTOENDPOINT: correction_vector is distance array to endpoint, path_vector is velocity vector
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// FOLLOWVECTOR: correct_vector is distance to vector path, path_vector is the desired velocity vector
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// Calculate the desired velocity from the lateral vector path errors (correct_vector) and the desired velocity vector (path_vector)
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controlNE.ControlPositionWithPath(&progress);
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float north, east;
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controlNE.GetVelocityDesired(&north, &east);
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velocityDesired.North = north;
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velocityDesired.East = east;
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velocityDesired.Down = 0.0f;
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// update pathstatus
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pathStatus->error = progress.error;
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pathStatus->fractional_progress = progress.fractional_progress;
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// FOLLOWVECTOR: desired velocity vector
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pathStatus->path_direction_north = progress.path_vector[0];
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pathStatus->path_direction_east = progress.path_vector[1];
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pathStatus->path_direction_down = progress.path_vector[2];
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// FOLLOWVECTOR: correction distance to vector path
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pathStatus->correction_direction_north = progress.correction_vector[0];
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pathStatus->correction_direction_east = progress.correction_vector[1];
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pathStatus->correction_direction_down = progress.correction_vector[2];
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VelocityDesiredSet(&velocityDesired);
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}
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/**
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* Compute desired attitude for ground vehicles
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*/
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uint8_t GroundDriveController::updateGroundDesiredAttitude()
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{
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StatusGroundDriveData statusGround;
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VelocityStateData velocityState;
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VelocityStateGet(&velocityState);
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AttitudeStateData attitudeState;
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AttitudeStateGet(&attitudeState);
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statusGround.State.Yaw = attitudeState.Yaw;
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statusGround.State.Velocity = sqrtf(velocityState.North * velocityState.North + velocityState.East * velocityState.East);
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StabilizationDesiredData stabDesired;
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StabilizationDesiredGet(&stabDesired);
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// estimate a north/east command value to control the velocity error.
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// ThrustLimits.Max(+-) limits the range. Think of this as a command unit vector
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// of the ultimate direction to reduce lateral error and achieve the target direction (desired angle).
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float northCommand, eastCommand;
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controlNE.GetNECommand(&northCommand, &eastCommand);
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// Get current vehicle orientation
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float angle_radians = DEG2RAD(attitudeState.Yaw); // (+-pi)
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float cos_angle = cosf(angle_radians);
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float sine_angle = sinf(angle_radians);
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float courseCommand = 0.0f;
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float speedCommand = 0.0f;
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float lateralCommand = boundf(-northCommand * sine_angle + eastCommand * cos_angle, -groundSettings->ThrustLimit.Max, groundSettings->ThrustLimit.Max);
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float forwardCommand = boundf(northCommand * cos_angle + eastCommand * sine_angle, -groundSettings->ThrustLimit.Max, groundSettings->ThrustLimit.Max);
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// +ve facing correct direction, lateral command should just correct angle,
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if (forwardCommand > 0.0f) {
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// if +ve forward command, -+ lateralCommand drives steering to manage lateral error and angular error
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courseCommand = boundf(lateralCommand, -1.0f, 1.0f);
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speedCommand = boundf(forwardCommand, groundSettings->ThrustLimit.SlowForward, groundSettings->ThrustLimit.Max);
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// reinstate max thrust
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controlNE.UpdateCommandParameters(-groundSettings->ThrustLimit.Max, groundSettings->ThrustLimit.Max, groundSettings->VelocityFeedForward);
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statusGround.ControlState = STATUSGROUNDDRIVE_CONTROLSTATE_ONTRACK;
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} else {
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// -ve facing opposite direction, lateral command irrelevant, need to turn to change direction and do so slowly.
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// Reduce steering angle based on current velocity
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float steeringReductionFactor = 1.0f;
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if (stabDesired.Thrust > 0.3f) {
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steeringReductionFactor = (groundSettings->HorizontalVelMax - statusGround.State.Velocity) / groundSettings->HorizontalVelMax;
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steeringReductionFactor = boundf(steeringReductionFactor, 0.05f, 1.0f);
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}
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// should we turn left or right?
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if (lateralCommand >= 0.1f) {
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courseCommand = 1.0f * steeringReductionFactor;
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statusGround.ControlState = STATUSGROUNDDRIVE_CONTROLSTATE_TURNAROUNDRIGHT;
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} else {
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courseCommand = -1.0f * steeringReductionFactor;
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statusGround.ControlState = STATUSGROUNDDRIVE_CONTROLSTATE_TURNAROUNDLEFT;
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}
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// Impose limits to slow down.
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controlNE.UpdateCommandParameters(-groundSettings->ThrustLimit.SlowForward, groundSettings->ThrustLimit.SlowForward, 0.0f);
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speedCommand = groundSettings->ThrustLimit.SlowForward;
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}
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stabDesired.Roll = 0.0f;
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stabDesired.Pitch = 0.0f;
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stabDesired.Yaw = courseCommand;
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// Mix yaw into thrust limit TODO
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stabDesired.Thrust = boundf(speedCommand, groundSettings->ThrustLimit.Min, groundSettings->ThrustLimit.Max);
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stabDesired.StabilizationMode.Roll = STABILIZATIONDESIRED_STABILIZATIONMODE_MANUAL;
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stabDesired.StabilizationMode.Pitch = STABILIZATIONDESIRED_STABILIZATIONMODE_MANUAL;
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stabDesired.StabilizationMode.Yaw = STABILIZATIONDESIRED_STABILIZATIONMODE_MANUAL;
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stabDesired.StabilizationMode.Thrust = STABILIZATIONDESIRED_STABILIZATIONMODE_MANUAL;
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StabilizationDesiredSet(&stabDesired);
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statusGround.NECommand.North = northCommand;
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statusGround.NECommand.East = eastCommand;
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statusGround.State.Thrust = stabDesired.Thrust;
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statusGround.BodyCommand.Forward = forwardCommand;
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statusGround.BodyCommand.Right = lateralCommand;
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statusGround.ControlCommand.Course = courseCommand;
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statusGround.ControlCommand.Speed = speedCommand;
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StatusGroundDriveSet(&statusGround);
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return 1;
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}
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