Working on segway controller, restructure of fixedwing.

This commit is contained in:
James Goppert
2013-07-28 01:35:43 -04:00
parent 95aa82f586
commit 1980d9dd63
22 changed files with 536 additions and 76 deletions
@@ -0,0 +1,56 @@
#include "BlockSegwayController.hpp"
void BlockSegwayController::update() {
// wait for a sensor update, check for exit condition every 100 ms
if (poll(&_attPoll, 1, 100) < 0) return; // poll error
uint64_t newTimeStamp = hrt_absolute_time();
float dt = (newTimeStamp - _timeStamp) / 1.0e6f;
_timeStamp = newTimeStamp;
// check for sane values of dt
// to prevent large control responses
if (dt > 1.0f || dt < 0) return;
// set dt for all child blocks
setDt(dt);
// check for new updates
if (_param_update.updated()) updateParams();
// get new information from subscriptions
updateSubscriptions();
// default all output to zero unless handled by mode
for (unsigned i = 2; i < NUM_ACTUATOR_CONTROLS; i++)
_actuators.control[i] = 0.0f;
// only update guidance in auto mode
if (_status.state_machine == SYSTEM_STATE_AUTO) {
// update guidance
}
// XXX handle STABILIZED (loiter on spot) as well
// once the system switches from manual or auto to stabilized
// the setpoint should update to loitering around this position
// handle autopilot modes
if (_status.state_machine == SYSTEM_STATE_AUTO ||
_status.state_machine == SYSTEM_STATE_STABILIZED) {
float spdCmd = phi2spd.update(_att.phi);
// output
_actuators.control[0] = spdCmd;
_actuators.control[1] = spdCmd;
} else if (_status.state_machine == SYSTEM_STATE_MANUAL) {
_actuators.control[0] = _manual.roll;
_actuators.control[1] = _manual.roll;
}
// update all publications
updatePublications();
}
@@ -0,0 +1,18 @@
#pragma once
#include <controllib/uorb/blocks.hpp>
using namespace control;
class BlockSegwayController : public control::BlockUorbEnabledAutopilot {
public:
BlockSegwayController() :
BlockUorbEnabledAutopilot(NULL,"SEG"),
phi2spd(this, "PHI2SPD")
{
}
void update();
private:
BlockP phi2spd;
};
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############################################################################
#
# 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.
#
############################################################################
#
# segway controller
#
MODULE_COMMAND = segway
SRCS = segway_main.cpp \
BlockSegwayController.cpp \
params.c
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#include <systemlib/param/param.h>
// currently tuned for easystar from arkhangar in HIL
//https://github.com/arktools/arkhangar
// 16 is max name length
// gyro low pass filter
PARAM_DEFINE_FLOAT(FWB_P_LP, 300.0f); // roll rate low pass cut freq
PARAM_DEFINE_FLOAT(FWB_Q_LP, 300.0f); // pitch rate low pass cut freq
PARAM_DEFINE_FLOAT(FWB_R_LP, 300.0f); // yaw rate low pass cut freq
// yaw washout
PARAM_DEFINE_FLOAT(FWB_R_HP, 1.0f); // yaw rate high pass
// stabilization mode
PARAM_DEFINE_FLOAT(FWB_P2AIL, 0.3f); // roll rate 2 aileron
PARAM_DEFINE_FLOAT(FWB_Q2ELV, 0.1f); // pitch rate 2 elevator
PARAM_DEFINE_FLOAT(FWB_R2RDR, 0.1f); // yaw rate 2 rudder
// psi -> phi -> p
PARAM_DEFINE_FLOAT(FWB_PSI2PHI, 0.5f); // heading 2 roll
PARAM_DEFINE_FLOAT(FWB_PHI2P, 1.0f); // roll to roll rate
PARAM_DEFINE_FLOAT(FWB_PHI_LIM_MAX, 0.3f); // roll limit, 28 deg
// velocity -> theta
PARAM_DEFINE_FLOAT(FWB_V2THE_P, 1.0f); // velocity to pitch angle PID, prop gain
PARAM_DEFINE_FLOAT(FWB_V2THE_I, 0.0f); // integral gain
PARAM_DEFINE_FLOAT(FWB_V2THE_D, 0.0f); // derivative gain
PARAM_DEFINE_FLOAT(FWB_V2THE_D_LP, 0.0f); // derivative low-pass
PARAM_DEFINE_FLOAT(FWB_V2THE_I_MAX, 0.0f); // integrator wind up guard
PARAM_DEFINE_FLOAT(FWB_THE_MIN, -0.5f); // the max commanded pitch angle
PARAM_DEFINE_FLOAT(FWB_THE_MAX, 0.5f); // the min commanded pitch angle
// theta -> q
PARAM_DEFINE_FLOAT(FWB_THE2Q_P, 1.0f); // pitch angle to pitch-rate PID
PARAM_DEFINE_FLOAT(FWB_THE2Q_I, 0.0f);
PARAM_DEFINE_FLOAT(FWB_THE2Q_D, 0.0f);
PARAM_DEFINE_FLOAT(FWB_THE2Q_D_LP, 0.0f);
PARAM_DEFINE_FLOAT(FWB_THE2Q_I_MAX, 0.0f);
// h -> thr
PARAM_DEFINE_FLOAT(FWB_H2THR_P, 0.01f); // altitude to throttle PID
PARAM_DEFINE_FLOAT(FWB_H2THR_I, 0.0f);
PARAM_DEFINE_FLOAT(FWB_H2THR_D, 0.0f);
PARAM_DEFINE_FLOAT(FWB_H2THR_D_LP, 0.0f);
PARAM_DEFINE_FLOAT(FWB_H2THR_I_MAX, 0.0f);
// crosstrack
PARAM_DEFINE_FLOAT(FWB_XT2YAW_MAX, 1.57f); // cross-track to yaw angle limit 90 deg
PARAM_DEFINE_FLOAT(FWB_XT2YAW, 0.005f); // cross-track to yaw angle gain
// speed command
PARAM_DEFINE_FLOAT(FWB_V_MIN, 10.0f); // minimum commanded velocity
PARAM_DEFINE_FLOAT(FWB_V_CMD, 12.0f); // commanded velocity
PARAM_DEFINE_FLOAT(FWB_V_MAX, 16.0f); // maximum commanded velocity
// rate of climb
// this is what rate of climb is commanded (in m/s)
// when the pitch stick is fully defelcted in simple mode
PARAM_DEFINE_FLOAT(FWB_CR_MAX, 1.0f);
// climb rate -> thr
PARAM_DEFINE_FLOAT(FWB_CR2THR_P, 0.01f); // rate of climb to throttle PID
PARAM_DEFINE_FLOAT(FWB_CR2THR_I, 0.0f);
PARAM_DEFINE_FLOAT(FWB_CR2THR_D, 0.0f);
PARAM_DEFINE_FLOAT(FWB_CR2THR_D_LP, 0.0f);
PARAM_DEFINE_FLOAT(FWB_CR2THR_I_MAX, 0.0f);
PARAM_DEFINE_FLOAT(FWB_TRIM_THR, 0.8f); // trim throttle (0,1)
PARAM_DEFINE_FLOAT(FWB_TRIM_V, 12.0f); // trim velocity, m/s
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/****************************************************************************
*
* Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
* Author: James Goppert
*
* 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 segway_main.cpp
* @author James Goppert
*
* Segway controller using control library
*/
#include <nuttx/config.h>
#include <unistd.h>
#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>
#include <drivers/drv_hrt.h>
#include <math.h>
#include "BlockSegwayController.hpp"
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 */
/**
* Deamon management function.
*/
extern "C" __EXPORT int segway_main(int argc, char *argv[]);
/**
* Mainloop of deamon.
*/
int control_demo_thread_main(int argc, char *argv[]);
/**
* Test function
*/
void test();
/**
* 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: segway {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_create().
*/
int segway_main(int argc, char *argv[])
{
if (argc < 1)
usage("missing command");
if (!strcmp(argv[1], "start")) {
if (thread_running) {
warnx("already running");
/* this is not an error */
exit(0);
}
thread_should_exit = false;
deamon_task = task_spawn_cmd("segway",
SCHED_DEFAULT,
SCHED_PRIORITY_MAX - 10,
5120,
control_demo_thread_main,
(argv) ? (const char **)&argv[2] : (const char **)NULL);
exit(0);
}
if (!strcmp(argv[1], "test")) {
test();
exit(0);
}
if (!strcmp(argv[1], "stop")) {
thread_should_exit = true;
exit(0);
}
if (!strcmp(argv[1], "status")) {
if (thread_running) {
warnx("is running");
} else {
warnx("not started");
}
exit(0);
}
usage("unrecognized command");
exit(1);
}
int control_demo_thread_main(int argc, char *argv[])
{
warnx("starting");
using namespace control;
BlockSegwayController autopilot;
thread_running = true;
while (!thread_should_exit) {
autopilot.update();
}
warnx("exiting.");
thread_running = false;
return 0;
}
void test()
{
warnx("beginning control lib test");
control::basicBlocksTest();
}