Merge branch 'master' into seatbelt_multirotor

This commit is contained in:
Anton Babushkin
2013-05-17 12:23:48 +04:00
811 changed files with 23913 additions and 3861 deletions
@@ -0,0 +1,41 @@
############################################################################
#
# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
#
# Build multirotor position control
#
MODULE_COMMAND = multirotor_pos_control
SRCS = multirotor_pos_control.c \
multirotor_pos_control_params.c
@@ -0,0 +1,325 @@
/****************************************************************************
*
* Copyright (C) 2013 Anton Babushkin. All rights reserved.
* Author: Anton Babushkin <rk3dov@gmail.com>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file multirotor_pos_control.c
*
* Multirotor position controller
*/
#include <nuttx/config.h>
#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include <stdbool.h>
#include <unistd.h>
#include <fcntl.h>
#include <errno.h>
#include <debug.h>
#include <termios.h>
#include <time.h>
#include <sys/prctl.h>
#include <drivers/drv_hrt.h>
#include <uORB/uORB.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/vehicle_attitude_setpoint.h>
#include <uORB/topics/vehicle_local_position.h>
#include <uORB/topics/vehicle_local_position_setpoint.h>
#include <uORB/topics/vehicle_vicon_position.h>
#include <systemlib/systemlib.h>
#include <mavlink/mavlink_log.h>
#include "multirotor_pos_control_params.h"
static bool thread_should_exit = false; /**< Deamon exit flag */
static bool thread_running = false; /**< Deamon status flag */
static int deamon_task; /**< Handle of deamon task / thread */
__EXPORT int multirotor_pos_control_main(int argc, char *argv[]);
/**
* Mainloop of position controller.
*/
static int multirotor_pos_control_thread_main(int argc, char *argv[]);
/**
* Print the correct usage.
*/
static void usage(const char *reason);
static void usage(const char *reason) {
if (reason)
fprintf(stderr, "%s\n", reason);
fprintf(stderr, "usage: deamon {start|stop|status} [-p <additional params>]\n\n");
exit(1);
}
/**
* The deamon app only briefly exists to start
* the background job. The stack size assigned in the
* Makefile does only apply to this management task.
*
* The actual stack size should be set in the call
* to task_spawn().
*/
int multirotor_pos_control_main(int argc, char *argv[]) {
if (argc < 1)
usage("missing command");
if (!strcmp(argv[1], "start")) {
if (thread_running) {
printf("multirotor_pos_control already running\n");
/* this is not an error */
exit(0);
}
thread_should_exit = false;
deamon_task = task_spawn("multirotor_pos_control",
SCHED_DEFAULT,
SCHED_PRIORITY_MAX - 60,
4096,
multirotor_pos_control_thread_main,
(argv) ? (const char **)&argv[2] : (const char **)NULL);
exit(0);
}
if (!strcmp(argv[1], "stop")) {
thread_should_exit = true;
exit(0);
}
if (!strcmp(argv[1], "status")) {
if (thread_running) {
printf("\tmultirotor_pos_control app is running\n");
} else {
printf("\tmultirotor_pos_control app not started\n");
}
exit(0);
}
usage("unrecognized command");
exit(1);
}
static int multirotor_pos_control_thread_main(int argc, char *argv[]) {
/* welcome user */
printf("[multirotor_pos_control] started\n");
static int mavlink_fd;
mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
mavlink_log_info(mavlink_fd, "[multirotor_pos_control] started");
/* structures */
struct vehicle_status_s status;
memset(&status, 0, sizeof(status));
struct vehicle_attitude_s att;
memset(&att, 0, sizeof(att));
struct vehicle_attitude_setpoint_s att_sp;
memset(&att_sp, 0, sizeof(att_sp));
struct manual_control_setpoint_s manual;
memset(&manual, 0, sizeof(manual));
struct vehicle_local_position_s local_pos;
memset(&local_pos, 0, sizeof(local_pos));
struct vehicle_local_position_setpoint_s local_pos_sp;
memset(&local_pos_sp, 0, sizeof(local_pos_sp));
/* subscribe to attitude, motor setpoints and system state */
int param_sub = orb_subscribe(ORB_ID(parameter_update));
int state_sub = orb_subscribe(ORB_ID(vehicle_status));
int att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
int att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
int local_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_local_position_setpoint));
int local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
/* publish setpoint */
orb_advert_t local_pos_sp_pub = orb_advertise(ORB_ID(vehicle_local_position_setpoint), &local_pos_sp);
orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp);
bool reset_sp_alt = true;
bool reset_sp_pos = true;
hrt_abstime t_prev = 0;
float alt_integral = 0.0f;
float alt_ctl_dz = 0.2f;
thread_running = true;
struct multirotor_position_control_params params;
struct multirotor_position_control_param_handles params_h;
parameters_init(&params_h);
parameters_update(&params_h, &params);
int paramcheck_counter = 0;
while (!thread_should_exit) {
orb_copy(ORB_ID(vehicle_status), state_sub, &status);
/* check parameters at 1 Hz*/
paramcheck_counter++;
if (paramcheck_counter == 50) {
bool param_updated;
orb_check(param_sub, &param_updated);
if (param_updated) {
parameters_update(&params_h, &params);
}
paramcheck_counter = 0;
}
/* Check if controller should act */
bool act = status.flag_system_armed && (
/* SAS modes */
(
status.flag_control_manual_enabled &&
status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS && (
status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ALTITUDE ||
status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_SIMPLE
)
) ||
/* AUTO mode */
status.state_machine == SYSTEM_STATE_AUTO
);
hrt_abstime t = hrt_absolute_time();
float dt;
if (t_prev != 0) {
dt = (t - t_prev) * 0.000001f;
} else {
dt = 0.0f;
}
t_prev = t;
if (act) {
orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &manual);
orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
orb_copy(ORB_ID(vehicle_attitude_setpoint), att_sp_sub, &att_sp);
orb_copy(ORB_ID(vehicle_local_position), local_pos_sub, &local_pos);
if (status.state_machine == SYSTEM_STATE_AUTO) {
orb_copy(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_sub, &local_pos_sp);
}
if (reset_sp_alt) {
reset_sp_alt = false;
local_pos_sp.z = local_pos.z;
alt_integral = manual.throttle;
char str[80];
sprintf(str, "reset alt setpoint: z = %.2f, throttle = %.2f", local_pos_sp.z, manual.throttle);
mavlink_log_info(mavlink_fd, str);
}
if (status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_SIMPLE && reset_sp_pos) {
reset_sp_pos = false;
local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y;
char str[80];
sprintf(str, "reset pos setpoint: x = %.2f, y = %.2f", local_pos_sp.x, local_pos_sp.y);
mavlink_log_info(mavlink_fd, str);
}
float err_linear_limit = params.alt_d / params.alt_p * params.alt_rate_max;
if (status.flag_control_manual_enabled) {
/* move altitude setpoint with manual controls */
float alt_ctl = manual.throttle - 0.5f;
if (fabs(alt_ctl) < alt_ctl_dz) {
alt_ctl = 0.0f;
} else {
if (alt_ctl > 0.0f)
alt_ctl = (alt_ctl - alt_ctl_dz) / (0.5f - alt_ctl_dz);
else
alt_ctl = (alt_ctl + alt_ctl_dz) / (0.5f - alt_ctl_dz);
local_pos_sp.z -= alt_ctl * params.alt_rate_max * dt;
if (local_pos_sp.z > local_pos.z + err_linear_limit)
local_pos_sp.z = local_pos.z + err_linear_limit;
else if (local_pos_sp.z < local_pos.z - err_linear_limit)
local_pos_sp.z = local_pos.z - err_linear_limit;
}
if (status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_SIMPLE) {
// TODO move position setpoint with manual controls
}
}
/* PID for altitude */
float alt_err = local_pos.z - local_pos_sp.z;
/* don't accelerate more than ALT_RATE_MAX, limit error to corresponding value */
if (alt_err > err_linear_limit) {
alt_err = err_linear_limit;
} else if (alt_err < -err_linear_limit) {
alt_err = -err_linear_limit;
}
/* P and D components */
float thrust_ctl_pd = alt_err * params.alt_p + local_pos.vz * params.alt_d;
/* add I component */
float thrust_ctl = thrust_ctl_pd + alt_integral;
alt_integral += thrust_ctl_pd / params.alt_p * params.alt_i * dt;
if (thrust_ctl < params.thr_min) {
thrust_ctl = params.thr_min;
} else if (thrust_ctl > params.thr_max) {
thrust_ctl = params.thr_max;
}
if (status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_SIMPLE || status.state_machine == SYSTEM_STATE_AUTO) {
// TODO add position controller
} else {
reset_sp_pos = true;
}
att_sp.thrust = thrust_ctl;
att_sp.timestamp = hrt_absolute_time();
if (status.flag_control_manual_enabled) {
/* publish local position setpoint in manual mode */
orb_publish(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_pub, &local_pos_sp);
}
/* publish new attitude setpoint */
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
} else {
reset_sp_alt = true;
reset_sp_pos = true;
}
/* run at approximately 50 Hz */
usleep(20000);
}
printf("[multirotor_pos_control] exiting\n");
mavlink_log_info(mavlink_fd, "[multirotor_pos_control] exiting");
thread_running = false;
fflush(stdout);
return 0;
}
@@ -0,0 +1,73 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: Tobias Naegeli <naegelit@student.ethz.ch>
* Lorenz Meier <lm@inf.ethz.ch>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/*
* @file multirotor_pos_control_params.c
*
* Parameters for multirotor_pos_control
*/
#include "multirotor_pos_control_params.h"
/* controller parameters */
PARAM_DEFINE_FLOAT(MPC_THR_MIN, 0.3f);
PARAM_DEFINE_FLOAT(MPC_THR_MAX, 0.7f);
PARAM_DEFINE_FLOAT(MPC_ALT_P, 0.1f);
PARAM_DEFINE_FLOAT(MPC_ALT_I, 0.01f);
PARAM_DEFINE_FLOAT(MPC_ALT_D, 0.2f);
PARAM_DEFINE_FLOAT(MPC_ALT_RATE_MAX, 3.0f);
int parameters_init(struct multirotor_position_control_param_handles *h)
{
h->thr_min = param_find("MPC_THR_MIN");
h->thr_max = param_find("MPC_THR_MAX");
/* PID parameters */
h->alt_p = param_find("MPC_ALT_P");
h->alt_i = param_find("MPC_ALT_I");
h->alt_d = param_find("MPC_ALT_D");
h->alt_rate_max = param_find("MPC_ALT_RATE_MAX");
return OK;
}
int parameters_update(const struct multirotor_position_control_param_handles *h, struct multirotor_position_control_params *p)
{
param_get(h->thr_min, &(p->thr_min));
param_get(h->thr_max, &(p->thr_max));
param_get(h->alt_p, &(p->alt_p));
param_get(h->alt_i, &(p->alt_i));
param_get(h->alt_d, &(p->alt_d));
param_get(h->alt_rate_max, &(p->alt_rate_max));
return OK;
}
@@ -0,0 +1,72 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: Tobias Naegeli <naegelit@student.ethz.ch>
* Lorenz Meier <lm@inf.ethz.ch>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/*
* @file multirotor_position_control_params.h
*
* Parameters for position controller
*/
#include <systemlib/param/param.h>
struct multirotor_position_control_params {
float thr_min;
float thr_max;
float alt_p;
float alt_i;
float alt_d;
float alt_rate_max;
};
struct multirotor_position_control_param_handles {
param_t thr_min;
param_t thr_max;
param_t alt_p;
param_t alt_i;
param_t alt_d;
param_t alt_rate_max;
};
/**
* Initialize all parameter handles and values
*
*/
int parameters_init(struct multirotor_position_control_param_handles *h);
/**
* Update all parameters
*
*/
int parameters_update(const struct multirotor_position_control_param_handles *h, struct multirotor_position_control_params *p);
@@ -0,0 +1,235 @@
// /****************************************************************************
// *
// * Copyright (C) 2008-2012 PX4 Development Team. All rights reserved.
// * Author: @author Lorenz Meier <lm@inf.ethz.ch>
// * @author Laurens Mackay <mackayl@student.ethz.ch>
// * @author Tobias Naegeli <naegelit@student.ethz.ch>
// * @author Martin Rutschmann <rutmarti@student.ethz.ch>
// *
// * Redistribution and use in source and binary forms, with or without
// * modification, are permitted provided that the following conditions
// * are met:
// *
// * 1. Redistributions of source code must retain the above copyright
// * notice, this list of conditions and the following disclaimer.
// * 2. Redistributions in binary form must reproduce the above copyright
// * notice, this list of conditions and the following disclaimer in
// * the documentation and/or other materials provided with the
// * distribution.
// * 3. Neither the name PX4 nor the names of its contributors may be
// * used to endorse or promote products derived from this software
// * without specific prior written permission.
// *
// * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
// * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
// * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
// * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
// * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
// * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
// * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
// * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
// * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
// * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
// * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
// * POSSIBILITY OF SUCH DAMAGE.
// *
// ****************************************************************************/
// /**
// * @file multirotor_position_control.c
// * Implementation of the position control for a multirotor VTOL
// */
// #include <stdio.h>
// #include <stdlib.h>
// #include <stdio.h>
// #include <stdint.h>
// #include <math.h>
// #include <stdbool.h>
// #include <float.h>
// #include <systemlib/pid/pid.h>
// #include "multirotor_position_control.h"
// void control_multirotor_position(const struct vehicle_state_s *vstatus, const struct vehicle_manual_control_s *manual,
// const struct vehicle_attitude_s *att, const struct vehicle_local_position_s *local_pos,
// const struct vehicle_local_position_setpoint_s *local_pos_sp, struct vehicle_attitude_setpoint_s *att_sp)
// {
// static PID_t distance_controller;
// static int read_ret;
// static global_data_position_t position_estimated;
// static uint16_t counter;
// static bool initialized;
// static uint16_t pm_counter;
// static float lat_next;
// static float lon_next;
// static float pitch_current;
// static float thrust_total;
// if (initialized == false) {
// pid_init(&distance_controller,
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_P],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_I],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_D],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_AWU],
// PID_MODE_DERIVATIV_CALC, 150);//150
// // pid_pos_lim = global_data_parameter_storage->pm.param_values[PARAM_PID_POS_LIM];
// // pid_pos_z_lim = global_data_parameter_storage->pm.param_values[PARAM_PID_POS_Z_LIM];
// thrust_total = 0.0f;
// /* Position initialization */
// /* Wait for new position estimate */
// do {
// read_ret = read_lock_position(&position_estimated);
// } while (read_ret != 0);
// lat_next = position_estimated.lat;
// lon_next = position_estimated.lon;
// /* attitude initialization */
// global_data_lock(&global_data_attitude->access_conf);
// pitch_current = global_data_attitude->pitch;
// global_data_unlock(&global_data_attitude->access_conf);
// initialized = true;
// }
// /* load new parameters with 10Hz */
// if (counter % 50 == 0) {
// if (global_data_trylock(&global_data_parameter_storage->access_conf) == 0) {
// /* check whether new parameters are available */
// if (global_data_parameter_storage->counter > pm_counter) {
// pid_set_parameters(&distance_controller,
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_P],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_I],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_D],
// global_data_parameter_storage->pm.param_values[PARAM_PID_POS_AWU]);
// //
// // pid_pos_lim = global_data_parameter_storage->pm.param_values[PARAM_PID_POS_LIM];
// // pid_pos_z_lim = global_data_parameter_storage->pm.param_values[PARAM_PID_POS_Z_LIM];
// pm_counter = global_data_parameter_storage->counter;
// printf("Position controller changed pid parameters\n");
// }
// }
// global_data_unlock(&global_data_parameter_storage->access_conf);
// }
// /* Wait for new position estimate */
// do {
// read_ret = read_lock_position(&position_estimated);
// } while (read_ret != 0);
// /* Get next waypoint */ //TODO: add local copy
// if (0 == global_data_trylock(&global_data_position_setpoint->access_conf)) {
// lat_next = global_data_position_setpoint->x;
// lon_next = global_data_position_setpoint->y;
// global_data_unlock(&global_data_position_setpoint->access_conf);
// }
// /* Get distance to waypoint */
// float distance_to_waypoint = get_distance_to_next_waypoint(position_estimated.lat , position_estimated.lon, lat_next, lon_next);
// // if(counter % 5 == 0)
// // printf("distance_to_waypoint: %.4f\n", distance_to_waypoint);
// /* Get bearing to waypoint (direction on earth surface to next waypoint) */
// float bearing = get_bearing_to_next_waypoint(position_estimated.lat, position_estimated.lon, lat_next, lon_next);
// if (counter % 5 == 0)
// printf("bearing: %.4f\n", bearing);
// /* Calculate speed in direction of bearing (needed for controller) */
// float speed_norm = sqrtf(position_estimated.vx * position_estimated.vx + position_estimated.vy * position_estimated.vy);
// // if(counter % 5 == 0)
// // printf("speed_norm: %.4f\n", speed_norm);
// float speed_to_waypoint = 0; //(position_estimated.vx * cosf(bearing) + position_estimated.vy * sinf(bearing))/speed_norm; //FIXME, TODO: re-enable this once we have a full estimate of the speed, then we can do a PID for the distance controller
// /* Control Thrust in bearing direction */
// float horizontal_thrust = -pid_calculate(&distance_controller, 0, distance_to_waypoint, speed_to_waypoint,
// CONTROL_PID_POSITION_INTERVAL); //TODO: maybe this "-" sign is an error somewhere else
// // if(counter % 5 == 0)
// // printf("horizontal thrust: %.4f\n", horizontal_thrust);
// /* Get total thrust (from remote for now) */
// if (0 == global_data_trylock(&global_data_rc_channels->access_conf)) {
// thrust_total = (float)global_data_rc_channels->chan[THROTTLE].scale; //TODO: how should we use the RC_CHANNELS_FUNCTION enum?
// global_data_unlock(&global_data_rc_channels->access_conf);
// }
// const float max_gas = 500.0f;
// thrust_total *= max_gas / 20000.0f; //TODO: check this
// thrust_total += max_gas / 2.0f;
// if (horizontal_thrust > thrust_total) {
// horizontal_thrust = thrust_total;
// } else if (horizontal_thrust < -thrust_total) {
// horizontal_thrust = -thrust_total;
// }
// //TODO: maybe we want to add a speed controller later...
// /* Calclulate thrust in east and north direction */
// float thrust_north = cosf(bearing) * horizontal_thrust;
// float thrust_east = sinf(bearing) * horizontal_thrust;
// if (counter % 10 == 0) {
// printf("thrust north: %.4f\n", thrust_north);
// printf("thrust east: %.4f\n", thrust_east);
// fflush(stdout);
// }
// /* Get current attitude */
// if (0 == global_data_trylock(&global_data_attitude->access_conf)) {
// pitch_current = global_data_attitude->pitch;
// global_data_unlock(&global_data_attitude->access_conf);
// }
// /* Get desired pitch & roll */
// float pitch_desired = 0.0f;
// float roll_desired = 0.0f;
// if (thrust_total != 0) {
// float pitch_fraction = -thrust_north / thrust_total;
// float roll_fraction = thrust_east / (cosf(pitch_current) * thrust_total);
// if (roll_fraction < -1) {
// roll_fraction = -1;
// } else if (roll_fraction > 1) {
// roll_fraction = 1;
// }
// // if(counter % 5 == 0)
// // {
// // printf("pitch_fraction: %.4f, roll_fraction: %.4f\n",pitch_fraction, roll_fraction);
// // fflush(stdout);
// // }
// pitch_desired = asinf(pitch_fraction);
// roll_desired = asinf(roll_fraction);
// }
// att_sp.roll = roll_desired;
// att_sp.pitch = pitch_desired;
// counter++;
// }
@@ -0,0 +1,50 @@
/****************************************************************************
*
* Copyright (C) 2008-2012 PX4 Development Team. All rights reserved.
* Author: @author Lorenz Meier <lm@inf.ethz.ch>
* @author Laurens Mackay <mackayl@student.ethz.ch>
* @author Tobias Naegeli <naegelit@student.ethz.ch>
* @author Martin Rutschmann <rutmarti@student.ethz.ch>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file multirotor_position_control.h
* Definition of the position control for a multirotor VTOL
*/
// #ifndef POSITION_CONTROL_H_
// #define POSITION_CONTROL_H_
// void control_multirotor_position(const struct vehicle_state_s *vstatus, const struct vehicle_manual_control_s *manual,
// const struct vehicle_attitude_s *att, const struct vehicle_local_position_s *local_pos,
// const struct vehicle_local_position_setpoint_s *local_pos_sp, struct vehicle_attitude_setpoint_s *att_sp);
// #endif /* POSITION_CONTROL_H_ */