mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-06 17:58:54 +08:00
Main UAVCAN protocol handling and ESC updates run on the same thread/wq as before. There are 2 WorkItems for separate scheduling of the 2, so that ESC updates run in sync with actuator_control updates. UAVCAN is scheduled at a fixed rate of 3ms (previously the poll timeout) and on each UAVCAN bus event. This leads to roughly the same behavior as before. CPU & RAM usage are pretty much the same (tested on Pixhawk 4). Testing done: Motors still work (with feedback), param changes and a UAVCAN optical flow sensor.
186 lines
5.8 KiB
C++
186 lines
5.8 KiB
C++
/****************************************************************************
|
|
*
|
|
* Copyright (C) 2014 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.
|
|
*
|
|
****************************************************************************/
|
|
|
|
/**
|
|
* @file esc.cpp
|
|
*
|
|
* @author Pavel Kirienko <pavel.kirienko@gmail.com>
|
|
*/
|
|
|
|
#include "esc.hpp"
|
|
#include <systemlib/err.h>
|
|
#include <drivers/drv_hrt.h>
|
|
|
|
#define MOTOR_BIT(x) (1<<(x))
|
|
|
|
using namespace time_literals;
|
|
|
|
UavcanEscController::UavcanEscController(uavcan::INode &node) :
|
|
_node(node),
|
|
_uavcan_pub_raw_cmd(node),
|
|
_uavcan_sub_status(node),
|
|
_orb_timer(node)
|
|
{
|
|
_uavcan_pub_raw_cmd.setPriority(UAVCAN_COMMAND_TRANSFER_PRIORITY);
|
|
}
|
|
|
|
UavcanEscController::~UavcanEscController()
|
|
{
|
|
}
|
|
|
|
int
|
|
UavcanEscController::init()
|
|
{
|
|
// ESC status subscription
|
|
int res = _uavcan_sub_status.start(StatusCbBinder(this, &UavcanEscController::esc_status_sub_cb));
|
|
|
|
if (res < 0) {
|
|
PX4_ERR("ESC status sub failed %i", res);
|
|
return res;
|
|
}
|
|
|
|
// ESC status will be relayed from UAVCAN bus into ORB at this rate
|
|
_orb_timer.setCallback(TimerCbBinder(this, &UavcanEscController::orb_pub_timer_cb));
|
|
_orb_timer.startPeriodic(uavcan::MonotonicDuration::fromMSec(1000 / ESC_STATUS_UPDATE_RATE_HZ));
|
|
|
|
return res;
|
|
}
|
|
|
|
void
|
|
UavcanEscController::update_outputs(bool stop_motors, uint16_t outputs[MAX_ACTUATORS], unsigned num_outputs)
|
|
{
|
|
if (num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize) {
|
|
num_outputs = uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize;
|
|
}
|
|
|
|
if (num_outputs > esc_status_s::CONNECTED_ESC_MAX) {
|
|
num_outputs = esc_status_s::CONNECTED_ESC_MAX;
|
|
}
|
|
|
|
/*
|
|
* Rate limiting - we don't want to congest the bus
|
|
*/
|
|
const auto timestamp = _node.getMonotonicTime();
|
|
|
|
if ((timestamp - _prev_cmd_pub).toUSec() < (1000000 / MAX_RATE_HZ)) {
|
|
return;
|
|
}
|
|
|
|
_prev_cmd_pub = timestamp;
|
|
|
|
/*
|
|
* Fill the command message
|
|
* If unarmed, we publish an empty message anyway
|
|
*/
|
|
uavcan::equipment::esc::RawCommand msg;
|
|
|
|
for (unsigned i = 0; i < num_outputs; i++) {
|
|
if (stop_motors || outputs[i] == DISARMED_OUTPUT_VALUE) {
|
|
msg.cmd.push_back(static_cast<unsigned>(0));
|
|
|
|
} else {
|
|
msg.cmd.push_back(static_cast<int>(outputs[i]));
|
|
}
|
|
}
|
|
|
|
/*
|
|
* Remove channels that are always zero.
|
|
* The objective of this optimization is to avoid broadcasting multi-frame transfers when a single frame
|
|
* transfer would be enough. This is a valid optimization as the UAVCAN specification implies that all
|
|
* non-specified ESC setpoints should be considered zero.
|
|
* The positive outcome is a (marginally) lower bus traffic and lower CPU load.
|
|
*
|
|
* From the standpoint of the PX4 architecture, however, this is a hack. It should be investigated why
|
|
* the mixer returns more outputs than are actually used.
|
|
*/
|
|
for (int index = int(msg.cmd.size()) - 1; index >= _max_number_of_nonzero_outputs; index--) {
|
|
if (msg.cmd[index] != 0) {
|
|
_max_number_of_nonzero_outputs = index + 1;
|
|
break;
|
|
}
|
|
}
|
|
|
|
msg.cmd.resize(_max_number_of_nonzero_outputs);
|
|
|
|
/*
|
|
* Publish the command message to the bus
|
|
* Note that for a quadrotor it takes one CAN frame
|
|
*/
|
|
_uavcan_pub_raw_cmd.broadcast(msg);
|
|
}
|
|
|
|
void
|
|
UavcanEscController::esc_status_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::esc::Status> &msg)
|
|
{
|
|
if (msg.esc_index < esc_status_s::CONNECTED_ESC_MAX) {
|
|
auto &ref = _esc_status.esc[msg.esc_index];
|
|
|
|
ref.esc_address = msg.getSrcNodeID().get();
|
|
ref.timestamp = hrt_absolute_time();
|
|
ref.esc_voltage = msg.voltage;
|
|
ref.esc_current = msg.current;
|
|
ref.esc_temperature = msg.temperature;
|
|
ref.esc_rpm = msg.rpm;
|
|
ref.esc_errorcount = msg.error_count;
|
|
}
|
|
}
|
|
|
|
void
|
|
UavcanEscController::orb_pub_timer_cb(const uavcan::TimerEvent &)
|
|
{
|
|
_esc_status.timestamp = hrt_absolute_time();
|
|
_esc_status.esc_count = _rotor_count;
|
|
_esc_status.counter += 1;
|
|
_esc_status.esc_connectiontype = esc_status_s::ESC_CONNECTION_TYPE_CAN;
|
|
_esc_status.esc_online_flags = check_escs_status();
|
|
|
|
_esc_status_pub.publish(_esc_status);
|
|
}
|
|
|
|
uint8_t
|
|
UavcanEscController::check_escs_status()
|
|
{
|
|
int esc_status_flags = 0;
|
|
const hrt_abstime now = hrt_absolute_time();
|
|
|
|
for (int index = 0; index < esc_status_s::CONNECTED_ESC_MAX; index++) {
|
|
|
|
if (_esc_status.esc[index].timestamp > 0 && now - _esc_status.esc[index].timestamp < 1200_ms) {
|
|
esc_status_flags |= (1 << index);
|
|
}
|
|
|
|
}
|
|
|
|
return esc_status_flags;
|
|
}
|