From 7ca82801bd4d4b9d6f4a0ac515e5cfcdc28f2e05 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sat, 27 Apr 2013 14:42:12 +0200 Subject: Moved multirotor controllers --- src/modules/multirotor_att_control/module.mk | 42 ++ .../multirotor_att_control_main.c | 485 +++++++++++++++++++++ .../multirotor_attitude_control.c | 249 +++++++++++ .../multirotor_attitude_control.h | 57 +++ .../multirotor_rate_control.c | 230 ++++++++++ .../multirotor_rate_control.h | 56 +++ 6 files changed, 1119 insertions(+) create mode 100755 src/modules/multirotor_att_control/module.mk create mode 100644 src/modules/multirotor_att_control/multirotor_att_control_main.c create mode 100644 src/modules/multirotor_att_control/multirotor_attitude_control.c create mode 100644 src/modules/multirotor_att_control/multirotor_attitude_control.h create mode 100644 src/modules/multirotor_att_control/multirotor_rate_control.c create mode 100644 src/modules/multirotor_att_control/multirotor_rate_control.h (limited to 'src/modules/multirotor_att_control') diff --git a/src/modules/multirotor_att_control/module.mk b/src/modules/multirotor_att_control/module.mk new file mode 100755 index 000000000..2fd52c162 --- /dev/null +++ b/src/modules/multirotor_att_control/module.mk @@ -0,0 +1,42 @@ +############################################################################ +# +# 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. +# +############################################################################ + +# +# Makefile to build the multirotor attitude controller +# + +MODULE_COMMAND = multirotor_att_control + +SRCS = multirotor_att_control_main.c \ + multirotor_attitude_control.c \ + multirotor_rate_control.c diff --git a/src/modules/multirotor_att_control/multirotor_att_control_main.c b/src/modules/multirotor_att_control/multirotor_att_control_main.c new file mode 100644 index 000000000..d94c0a69c --- /dev/null +++ b/src/modules/multirotor_att_control/multirotor_att_control_main.c @@ -0,0 +1,485 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: Lorenz Meier + * + * 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_att_control_main.c + * + * Implementation of multirotor attitude control main loop. + * + * @author Lorenz Meier + */ + +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include + +#include +#include +#include + +#include "multirotor_attitude_control.h" +#include "multirotor_rate_control.h" + +PARAM_DEFINE_FLOAT(MC_RCLOSS_THR, 0.0f); // This defines the throttle when the RC signal is lost. + +__EXPORT int multirotor_att_control_main(int argc, char *argv[]); + +static bool thread_should_exit; +static int mc_task; +static bool motor_test_mode = false; + +static orb_advert_t actuator_pub; + +static struct vehicle_status_s state; + +static int +mc_thread_main(int argc, char *argv[]) +{ + /* declare and safely initialize all structs */ + memset(&state, 0, sizeof(state)); + 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 sensor_combined_s raw; + memset(&raw, 0, sizeof(raw)); + struct offboard_control_setpoint_s offboard_sp; + memset(&offboard_sp, 0, sizeof(offboard_sp)); + struct vehicle_rates_setpoint_s rates_sp; + memset(&rates_sp, 0, sizeof(rates_sp)); + + struct actuator_controls_s actuators; + memset(&actuators, 0, sizeof(actuators)); + + /* subscribe to attitude, motor setpoints and system state */ + int att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); + int param_sub = orb_subscribe(ORB_ID(parameter_update)); + int att_setpoint_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint)); + int setpoint_sub = orb_subscribe(ORB_ID(offboard_control_setpoint)); + int state_sub = orb_subscribe(ORB_ID(vehicle_status)); + int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); + int sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); + + /* + * Do not rate-limit the loop to prevent aliasing + * if rate-limiting would be desired later, the line below would + * enable it. + * + * rate-limit the attitude subscription to 200Hz to pace our loop + * orb_set_interval(att_sub, 5); + */ + struct pollfd fds[2] = { + { .fd = att_sub, .events = POLLIN }, + { .fd = param_sub, .events = POLLIN } + }; + + /* publish actuator controls */ + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) { + actuators.control[i] = 0.0f; + } + + actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, &actuators); + orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp); + orb_advert_t rates_sp_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint), &rates_sp); + int rates_sp_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint)); + + /* register the perf counter */ + perf_counter_t mc_loop_perf = perf_alloc(PC_ELAPSED, "multirotor_att_control_runtime"); + perf_counter_t mc_interval_perf = perf_alloc(PC_INTERVAL, "multirotor_att_control_interval"); + perf_counter_t mc_err_perf = perf_alloc(PC_COUNT, "multirotor_att_control_err"); + + /* welcome user */ + printf("[multirotor_att_control] starting\n"); + + /* store last control mode to detect mode switches */ + bool flag_control_manual_enabled = false; + bool flag_control_attitude_enabled = false; + bool flag_system_armed = false; + + /* store if yaw position or yaw speed has been changed */ + bool control_yaw_position = true; + + /* store if we stopped a yaw movement */ + bool first_time_after_yaw_speed_control = true; + + /* prepare the handle for the failsafe throttle */ + param_t failsafe_throttle_handle = param_find("MC_RCLOSS_THR"); + float failsafe_throttle = 0.0f; + + + while (!thread_should_exit) { + + /* wait for a sensor update, check for exit condition every 500 ms */ + int ret = poll(fds, 2, 500); + + if (ret < 0) { + /* poll error, count it in perf */ + perf_count(mc_err_perf); + + } else if (ret == 0) { + /* no return value, ignore */ + } else { + + /* only update parameters if they changed */ + if (fds[1].revents & POLLIN) { + /* read from param to clear updated flag */ + struct parameter_update_s update; + orb_copy(ORB_ID(parameter_update), param_sub, &update); + + /* update parameters */ + // XXX no params here yet + } + + /* only run controller if attitude changed */ + if (fds[0].revents & POLLIN) { + + perf_begin(mc_loop_perf); + + /* get a local copy of system state */ + bool updated; + orb_check(state_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(vehicle_status), state_sub, &state); + } + + /* get a local copy of manual setpoint */ + orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &manual); + /* get a local copy of attitude */ + orb_copy(ORB_ID(vehicle_attitude), att_sub, &att); + /* get a local copy of attitude setpoint */ + orb_copy(ORB_ID(vehicle_attitude_setpoint), att_setpoint_sub, &att_sp); + /* get a local copy of rates setpoint */ + orb_check(setpoint_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(offboard_control_setpoint), setpoint_sub, &offboard_sp); + } + + /* get a local copy of the current sensor values */ + orb_copy(ORB_ID(sensor_combined), sensor_sub, &raw); + + + /** STEP 1: Define which input is the dominating control input */ + if (state.flag_control_offboard_enabled) { + /* offboard inputs */ + if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_RATES) { + rates_sp.roll = offboard_sp.p1; + rates_sp.pitch = offboard_sp.p2; + rates_sp.yaw = offboard_sp.p3; + rates_sp.thrust = offboard_sp.p4; +// printf("thrust_rate=%8.4f\n",offboard_sp.p4); + rates_sp.timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp); + + } else if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE) { + att_sp.roll_body = offboard_sp.p1; + att_sp.pitch_body = offboard_sp.p2; + att_sp.yaw_body = offboard_sp.p3; + att_sp.thrust = offboard_sp.p4; +// printf("thrust_att=%8.4f\n",offboard_sp.p4); + att_sp.timestamp = hrt_absolute_time(); + /* STEP 2: publish the result to the vehicle actuators */ + orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + } + + + } else if (state.flag_control_manual_enabled) { + + if (state.flag_control_attitude_enabled) { + + /* initialize to current yaw if switching to manual or att control */ + if (state.flag_control_attitude_enabled != flag_control_attitude_enabled || + state.flag_control_manual_enabled != flag_control_manual_enabled || + state.flag_system_armed != flag_system_armed) { + att_sp.yaw_body = att.yaw; + } + + static bool rc_loss_first_time = true; + + /* if the RC signal is lost, try to stay level and go slowly back down to ground */ + if (state.rc_signal_lost) { + /* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */ + param_get(failsafe_throttle_handle, &failsafe_throttle); + att_sp.roll_body = 0.0f; + att_sp.pitch_body = 0.0f; + + /* + * Only go to failsafe throttle if last known throttle was + * high enough to create some lift to make hovering state likely. + * + * This is to prevent that someone landing, but not disarming his + * multicopter (throttle = 0) does not make it jump up in the air + * if shutting down his remote. + */ + if (isfinite(manual.throttle) && manual.throttle > 0.2f) { + att_sp.thrust = failsafe_throttle; + + } else { + att_sp.thrust = 0.0f; + } + + /* keep current yaw, do not attempt to go to north orientation, + * since if the pilot regains RC control, he will be lost regarding + * the current orientation. + */ + if (rc_loss_first_time) + att_sp.yaw_body = att.yaw; + + rc_loss_first_time = false; + + } else { + rc_loss_first_time = true; + + att_sp.roll_body = manual.roll; + att_sp.pitch_body = manual.pitch; + + /* set attitude if arming */ + if (!flag_control_attitude_enabled && state.flag_system_armed) { + att_sp.yaw_body = att.yaw; + } + + /* act if stabilization is active or if the (nonsense) direct pass through mode is set */ + if (state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS || + state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { + + if (state.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_RATE) { + rates_sp.yaw = manual.yaw; + control_yaw_position = false; + + } else { + /* + * This mode SHOULD be the default mode, which is: + * VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS + * + * However, we fall back to this setting for all other (nonsense) + * settings as well. + */ + + /* only move setpoint if manual input is != 0 */ + if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) { + rates_sp.yaw = manual.yaw; + control_yaw_position = false; + first_time_after_yaw_speed_control = true; + + } else { + if (first_time_after_yaw_speed_control) { + att_sp.yaw_body = att.yaw; + first_time_after_yaw_speed_control = false; + } + + control_yaw_position = true; + } + } + } + + att_sp.thrust = manual.throttle; + att_sp.timestamp = hrt_absolute_time(); + } + + /* STEP 2: publish the controller output */ + orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + + if (motor_test_mode) { + printf("testmode"); + att_sp.roll_body = 0.0f; + att_sp.pitch_body = 0.0f; + att_sp.yaw_body = 0.0f; + att_sp.thrust = 0.1f; + att_sp.timestamp = hrt_absolute_time(); + /* STEP 2: publish the result to the vehicle actuators */ + orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + } + + } else { + /* manual rate inputs, from RC control or joystick */ + if (state.flag_control_rates_enabled && + state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_RATES) { + rates_sp.roll = manual.roll; + + rates_sp.pitch = manual.pitch; + rates_sp.yaw = manual.yaw; + rates_sp.thrust = manual.throttle; + rates_sp.timestamp = hrt_absolute_time(); + } + } + + } + + /** STEP 3: Identify the controller setup to run and set up the inputs correctly */ + if (state.flag_control_attitude_enabled) { + multirotor_control_attitude(&att_sp, &att, &rates_sp, control_yaw_position); + + orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp); + } + + /* measure in what intervals the controller runs */ + perf_count(mc_interval_perf); + + float gyro[3]; + + /* get current rate setpoint */ + bool rates_sp_valid = false; + orb_check(rates_sp_sub, &rates_sp_valid); + + if (rates_sp_valid) { + orb_copy(ORB_ID(vehicle_rates_setpoint), rates_sp_sub, &rates_sp); + } + + /* apply controller */ + gyro[0] = att.rollspeed; + gyro[1] = att.pitchspeed; + gyro[2] = att.yawspeed; + + multirotor_control_rates(&rates_sp, gyro, &actuators); + orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); + + /* update state */ + flag_control_attitude_enabled = state.flag_control_attitude_enabled; + flag_control_manual_enabled = state.flag_control_manual_enabled; + flag_system_armed = state.flag_system_armed; + + perf_end(mc_loop_perf); + } /* end of poll call for attitude updates */ + } /* end of poll return value check */ + } + + printf("[multirotor att control] stopping, disarming motors.\n"); + + /* kill all outputs */ + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) + actuators.control[i] = 0.0f; + + orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); + + + close(att_sub); + close(state_sub); + close(manual_sub); + close(actuator_pub); + close(att_sp_pub); + + perf_print_counter(mc_loop_perf); + perf_free(mc_loop_perf); + + fflush(stdout); + exit(0); +} + +static void +usage(const char *reason) +{ + if (reason) + fprintf(stderr, "%s\n", reason); + + fprintf(stderr, "usage: multirotor_att_control [-m ] [-t] {start|status|stop}\n"); + fprintf(stderr, " is 'rates' or 'attitude'\n"); + fprintf(stderr, " -t enables motor test mode with 10%% thrust\n"); + exit(1); +} + +int multirotor_att_control_main(int argc, char *argv[]) +{ + int ch; + unsigned int optioncount = 0; + + while ((ch = getopt(argc, argv, "tm:")) != EOF) { + switch (ch) { + case 't': + motor_test_mode = true; + optioncount += 1; + break; + + case ':': + usage("missing parameter"); + break; + + default: + fprintf(stderr, "option: -%c\n", ch); + usage("unrecognized option"); + break; + } + } + + argc -= optioncount; + //argv += optioncount; + + if (argc < 1) + usage("missing command"); + + if (!strcmp(argv[1 + optioncount], "start")) { + + thread_should_exit = false; + mc_task = task_spawn("multirotor_att_control", + SCHED_DEFAULT, + SCHED_PRIORITY_MAX - 15, + 2048, + mc_thread_main, + NULL); + exit(0); + } + + if (!strcmp(argv[1 + optioncount], "stop")) { + thread_should_exit = true; + exit(0); + } + + usage("unrecognized command"); + exit(1); +} diff --git a/src/modules/multirotor_att_control/multirotor_attitude_control.c b/src/modules/multirotor_att_control/multirotor_attitude_control.c new file mode 100644 index 000000000..76dbb36d3 --- /dev/null +++ b/src/modules/multirotor_att_control/multirotor_attitude_control.c @@ -0,0 +1,249 @@ +/**************************************************************************** + * + * Copyright (C) 2008-2012 PX4 Development Team. All rights reserved. + * Author: @author Thomas Gubler + * @author Julian Oes + * @author Laurens Mackay + * @author Tobias Naegeli + * @author Martin Rutschmann + * @author Lorenz Meier + * + * 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_attitude_control.c + * Implementation of attitude controller + */ + +#include "multirotor_attitude_control.h" +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include + +PARAM_DEFINE_FLOAT(MC_YAWPOS_P, 0.3f); +PARAM_DEFINE_FLOAT(MC_YAWPOS_I, 0.15f); +PARAM_DEFINE_FLOAT(MC_YAWPOS_D, 0.0f); +//PARAM_DEFINE_FLOAT(MC_YAWPOS_AWU, 1.0f); +//PARAM_DEFINE_FLOAT(MC_YAWPOS_LIM, 3.0f); + +PARAM_DEFINE_FLOAT(MC_ATT_P, 0.2f); +PARAM_DEFINE_FLOAT(MC_ATT_I, 0.0f); +PARAM_DEFINE_FLOAT(MC_ATT_D, 0.05f); +//PARAM_DEFINE_FLOAT(MC_ATT_AWU, 0.05f); +//PARAM_DEFINE_FLOAT(MC_ATT_LIM, 0.4f); + +//PARAM_DEFINE_FLOAT(MC_ATT_XOFF, 0.0f); +//PARAM_DEFINE_FLOAT(MC_ATT_YOFF, 0.0f); + +struct mc_att_control_params { + float yaw_p; + float yaw_i; + float yaw_d; + //float yaw_awu; + //float yaw_lim; + + float att_p; + float att_i; + float att_d; + //float att_awu; + //float att_lim; + + //float att_xoff; + //float att_yoff; +}; + +struct mc_att_control_param_handles { + param_t yaw_p; + param_t yaw_i; + param_t yaw_d; + //param_t yaw_awu; + //param_t yaw_lim; + + param_t att_p; + param_t att_i; + param_t att_d; + //param_t att_awu; + //param_t att_lim; + + //param_t att_xoff; + //param_t att_yoff; +}; + +/** + * Initialize all parameter handles and values + * + */ +static int parameters_init(struct mc_att_control_param_handles *h); + +/** + * Update all parameters + * + */ +static int parameters_update(const struct mc_att_control_param_handles *h, struct mc_att_control_params *p); + + +static int parameters_init(struct mc_att_control_param_handles *h) +{ + /* PID parameters */ + h->yaw_p = param_find("MC_YAWPOS_P"); + h->yaw_i = param_find("MC_YAWPOS_I"); + h->yaw_d = param_find("MC_YAWPOS_D"); + //h->yaw_awu = param_find("MC_YAWPOS_AWU"); + //h->yaw_lim = param_find("MC_YAWPOS_LIM"); + + h->att_p = param_find("MC_ATT_P"); + h->att_i = param_find("MC_ATT_I"); + h->att_d = param_find("MC_ATT_D"); + //h->att_awu = param_find("MC_ATT_AWU"); + //h->att_lim = param_find("MC_ATT_LIM"); + + //h->att_xoff = param_find("MC_ATT_XOFF"); + //h->att_yoff = param_find("MC_ATT_YOFF"); + + return OK; +} + +static int parameters_update(const struct mc_att_control_param_handles *h, struct mc_att_control_params *p) +{ + param_get(h->yaw_p, &(p->yaw_p)); + param_get(h->yaw_i, &(p->yaw_i)); + param_get(h->yaw_d, &(p->yaw_d)); + //param_get(h->yaw_awu, &(p->yaw_awu)); + //param_get(h->yaw_lim, &(p->yaw_lim)); + + param_get(h->att_p, &(p->att_p)); + param_get(h->att_i, &(p->att_i)); + param_get(h->att_d, &(p->att_d)); + //param_get(h->att_awu, &(p->att_awu)); + //param_get(h->att_lim, &(p->att_lim)); + + //param_get(h->att_xoff, &(p->att_xoff)); + //param_get(h->att_yoff, &(p->att_yoff)); + + return OK; +} + +void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, + const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position) +{ + static uint64_t last_run = 0; + static uint64_t last_input = 0; + float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; + float dT_input = (hrt_absolute_time() - last_input) / 1000000.0f; + last_run = hrt_absolute_time(); + + if (last_input != att_sp->timestamp) { + last_input = att_sp->timestamp; + } + + static int sensor_delay; + sensor_delay = hrt_absolute_time() - att->timestamp; + + static int motor_skip_counter = 0; + + static PID_t pitch_controller; + static PID_t roll_controller; + + static struct mc_att_control_params p; + static struct mc_att_control_param_handles h; + + static bool initialized = false; + + static float yaw_error; + + /* initialize the pid controllers when the function is called for the first time */ + if (initialized == false) { + parameters_init(&h); + parameters_update(&h, &p); + + pid_init(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, + 1000.0f, PID_MODE_DERIVATIV_SET); + pid_init(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, + 1000.0f, PID_MODE_DERIVATIV_SET); + + initialized = true; + } + + /* load new parameters with lower rate */ + if (motor_skip_counter % 500 == 0) { + /* update parameters from storage */ + parameters_update(&h, &p); + + /* apply parameters */ + pid_set_parameters(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); + pid_set_parameters(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); + } + + /* reset integral if on ground */ + if (att_sp->thrust < 0.1f) { + pid_reset_integral(&pitch_controller); + pid_reset_integral(&roll_controller); + } + + + /* calculate current control outputs */ + + /* control pitch (forward) output */ + rates_sp->pitch = pid_calculate(&pitch_controller, att_sp->pitch_body , + att->pitch, att->pitchspeed, deltaT); + + /* control roll (left/right) output */ + rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body , + att->roll, att->rollspeed, deltaT); + + if (control_yaw_position) { + /* control yaw rate */ + + /* positive error: rotate to right, negative error, rotate to left (NED frame) */ + // yaw_error = _wrap_pi(att_sp->yaw_body - att->yaw); + + yaw_error = att_sp->yaw_body - att->yaw; + + if (yaw_error > M_PI_F) { + yaw_error -= M_TWOPI_F; + + } else if (yaw_error < -M_PI_F) { + yaw_error += M_TWOPI_F; + } + + rates_sp->yaw = p.yaw_p * (yaw_error) - (p.yaw_d * att->yawspeed); + } + + rates_sp->thrust = att_sp->thrust; + + motor_skip_counter++; +} diff --git a/src/modules/multirotor_att_control/multirotor_attitude_control.h b/src/modules/multirotor_att_control/multirotor_attitude_control.h new file mode 100644 index 000000000..2cf83e443 --- /dev/null +++ b/src/modules/multirotor_att_control/multirotor_attitude_control.h @@ -0,0 +1,57 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Thomas Gubler + * @author Julian Oes + * @author Laurens Mackay + * @author Tobias Naegeli + * @author Martin Rutschmann + * @author Lorenz Meier + * + * 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_attitude_control.h + * Attitude control for multi rotors. + */ + +#ifndef MULTIROTOR_ATTITUDE_CONTROL_H_ +#define MULTIROTOR_ATTITUDE_CONTROL_H_ + +#include +#include +#include +#include +#include + +void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, + const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position); + +#endif /* MULTIROTOR_ATTITUDE_CONTROL_H_ */ diff --git a/src/modules/multirotor_att_control/multirotor_rate_control.c b/src/modules/multirotor_att_control/multirotor_rate_control.c new file mode 100644 index 000000000..deba1ac03 --- /dev/null +++ b/src/modules/multirotor_att_control/multirotor_rate_control.c @@ -0,0 +1,230 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: Tobias Naegeli + * Lorenz Meier + * + * 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_rate_control.c + * + * Implementation of rate controller + * + * @author Tobias Naegeli + * @author Lorenz Meier + */ + +#include "multirotor_rate_control.h" +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include +#include + +PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.0f); /* same on Flamewheel */ +PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f); +PARAM_DEFINE_FLOAT(MC_YAWRATE_I, 0.0f); +//PARAM_DEFINE_FLOAT(MC_YAWRATE_AWU, 0.0f); +//PARAM_DEFINE_FLOAT(MC_YAWRATE_LIM, 1.0f); + +PARAM_DEFINE_FLOAT(MC_ATTRATE_P, 0.0f); /* 0.15 F405 Flamewheel */ +PARAM_DEFINE_FLOAT(MC_ATTRATE_D, 0.0f); +PARAM_DEFINE_FLOAT(MC_ATTRATE_I, 0.0f); +//PARAM_DEFINE_FLOAT(MC_ATTRATE_AWU, 0.05f); +//PARAM_DEFINE_FLOAT(MC_ATTRATE_LIM, 1.0f); /**< roughly < 500 deg/s limit */ + +struct mc_rate_control_params { + + float yawrate_p; + float yawrate_d; + float yawrate_i; + //float yawrate_awu; + //float yawrate_lim; + + float attrate_p; + float attrate_d; + float attrate_i; + //float attrate_awu; + //float attrate_lim; + + float rate_lim; +}; + +struct mc_rate_control_param_handles { + + param_t yawrate_p; + param_t yawrate_i; + param_t yawrate_d; + //param_t yawrate_awu; + //param_t yawrate_lim; + + param_t attrate_p; + param_t attrate_i; + param_t attrate_d; + //param_t attrate_awu; + //param_t attrate_lim; +}; + +/** + * Initialize all parameter handles and values + * + */ +static int parameters_init(struct mc_rate_control_param_handles *h); + +/** + * Update all parameters + * + */ +static int parameters_update(const struct mc_rate_control_param_handles *h, struct mc_rate_control_params *p); + + +static int parameters_init(struct mc_rate_control_param_handles *h) +{ + /* PID parameters */ + h->yawrate_p = param_find("MC_YAWRATE_P"); + h->yawrate_i = param_find("MC_YAWRATE_I"); + h->yawrate_d = param_find("MC_YAWRATE_D"); + //h->yawrate_awu = param_find("MC_YAWRATE_AWU"); + //h->yawrate_lim = param_find("MC_YAWRATE_LIM"); + + h->attrate_p = param_find("MC_ATTRATE_P"); + h->attrate_i = param_find("MC_ATTRATE_I"); + h->attrate_d = param_find("MC_ATTRATE_D"); + //h->attrate_awu = param_find("MC_ATTRATE_AWU"); + //h->attrate_lim = param_find("MC_ATTRATE_LIM"); + + return OK; +} + +static int parameters_update(const struct mc_rate_control_param_handles *h, struct mc_rate_control_params *p) +{ + param_get(h->yawrate_p, &(p->yawrate_p)); + param_get(h->yawrate_i, &(p->yawrate_i)); + param_get(h->yawrate_d, &(p->yawrate_d)); + //param_get(h->yawrate_awu, &(p->yawrate_awu)); + //param_get(h->yawrate_lim, &(p->yawrate_lim)); + + param_get(h->attrate_p, &(p->attrate_p)); + param_get(h->attrate_i, &(p->attrate_i)); + param_get(h->attrate_d, &(p->attrate_d)); + //param_get(h->attrate_awu, &(p->attrate_awu)); + //param_get(h->attrate_lim, &(p->attrate_lim)); + + return OK; +} + +void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, + const float rates[], struct actuator_controls_s *actuators) +{ + static float roll_control_last = 0; + static float pitch_control_last = 0; + static uint64_t last_run = 0; + const float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; + static uint64_t last_input = 0; + + float dT_input = (hrt_absolute_time() - last_input) / 1000000.0f; + + if (last_input != rate_sp->timestamp) { + last_input = rate_sp->timestamp; + } + + last_run = hrt_absolute_time(); + + static int motor_skip_counter = 0; + + static struct mc_rate_control_params p; + static struct mc_rate_control_param_handles h; + + static bool initialized = false; + + /* initialize the pid controllers when the function is called for the first time */ + if (initialized == false) { + parameters_init(&h); + parameters_update(&h, &p); + initialized = true; + } + + /* load new parameters with lower rate */ + if (motor_skip_counter % 2500 == 0) { + /* update parameters from storage */ + parameters_update(&h, &p); + // warnx("rate ctrl: p.yawrate_p: %8.4f, loop: %d Hz, input: %d Hz", + // (double)p.yawrate_p, (int)(1.0f/deltaT), (int)(1.0f/dT_input)); + } + + /* calculate current control outputs */ + + /* control pitch (forward) output */ + float pitch_control = p.attrate_p * (rate_sp->pitch - rates[1]) - (p.attrate_d * pitch_control_last); + + /* increase resilience to faulty control inputs */ + if (isfinite(pitch_control)) { + pitch_control_last = pitch_control; + + } else { + pitch_control = 0.0f; + warnx("rej. NaN ctrl pitch"); + } + + /* control roll (left/right) output */ + float roll_control = p.attrate_p * (rate_sp->roll - rates[0]) - (p.attrate_d * roll_control_last); + + /* increase resilience to faulty control inputs */ + if (isfinite(roll_control)) { + roll_control_last = roll_control; + + } else { + roll_control = 0.0f; + warnx("rej. NaN ctrl roll"); + } + + /* control yaw rate */ + float yaw_rate_control = p.yawrate_p * (rate_sp->yaw - rates[2]); + + /* increase resilience to faulty control inputs */ + if (!isfinite(yaw_rate_control)) { + yaw_rate_control = 0.0f; + warnx("rej. NaN ctrl yaw"); + } + + actuators->control[0] = roll_control; + actuators->control[1] = pitch_control; + actuators->control[2] = yaw_rate_control; + actuators->control[3] = rate_sp->thrust; + + motor_skip_counter++; +} diff --git a/src/modules/multirotor_att_control/multirotor_rate_control.h b/src/modules/multirotor_att_control/multirotor_rate_control.h new file mode 100644 index 000000000..03dec317a --- /dev/null +++ b/src/modules/multirotor_att_control/multirotor_rate_control.h @@ -0,0 +1,56 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Thomas Gubler + * @author Julian Oes + * @author Laurens Mackay + * @author Tobias Naegeli + * @author Martin Rutschmann + * @author Lorenz Meier + * + * 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_attitude_control.h + * Attitude control for multi rotors. + */ + +#ifndef MULTIROTOR_RATE_CONTROL_H_ +#define MULTIROTOR_RATE_CONTROL_H_ + +#include +#include +#include +#include + +void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, + const float rates[], struct actuator_controls_s *actuators); + +#endif /* MULTIROTOR_RATE_CONTROL_H_ */ -- cgit v1.2.3