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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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198 lines
5.7 KiB
C++
198 lines
5.7 KiB
C++
/****************************************************************************
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*
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* Copyright (C) 2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file esc.cpp
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*
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* @author Pavel Kirienko <pavel.kirienko@gmail.com>
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*/
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#include "esc.hpp"
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#include <systemlib/err.h>
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#define MOTOR_BIT(x) (1<<(x))
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UavcanEscController::UavcanEscController(uavcan::INode &node) :
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_node(node),
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_uavcan_pub_raw_cmd(node),
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_uavcan_sub_status(node),
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_orb_timer(node)
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{
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if (_perfcnt_invalid_input == nullptr) {
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errx(1, "uavcan: couldn't allocate _perfcnt_invalid_input");
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}
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if (_perfcnt_scaling_error == nullptr) {
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errx(1, "uavcan: couldn't allocate _perfcnt_scaling_error");
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}
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}
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UavcanEscController::~UavcanEscController()
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{
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perf_free(_perfcnt_invalid_input);
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perf_free(_perfcnt_scaling_error);
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}
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int UavcanEscController::init()
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{
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// ESC status subscription
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int res = _uavcan_sub_status.start(StatusCbBinder(this, &UavcanEscController::esc_status_sub_cb));
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if (res < 0) {
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warnx("ESC status sub failed %i", res);
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return res;
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}
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// ESC status will be relayed from UAVCAN bus into ORB at this rate
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_orb_timer.setCallback(TimerCbBinder(this, &UavcanEscController::orb_pub_timer_cb));
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_orb_timer.startPeriodic(uavcan::MonotonicDuration::fromMSec(1000 / ESC_STATUS_UPDATE_RATE_HZ));
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return res;
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}
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void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
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{
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if ((outputs == nullptr) ||
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(num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize) ||
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(num_outputs > esc_status_s::CONNECTED_ESC_MAX)) {
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perf_count(_perfcnt_invalid_input);
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return;
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}
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/*
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* Rate limiting - we don't want to congest the bus
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*/
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const auto timestamp = _node.getMonotonicTime();
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if ((timestamp - _prev_cmd_pub).toUSec() < (1000000 / MAX_RATE_HZ)) {
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return;
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}
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_prev_cmd_pub = timestamp;
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/*
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* Fill the command message
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* If unarmed, we publish an empty message anyway
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*/
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uavcan::equipment::esc::RawCommand msg;
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static const int cmd_max = uavcan::equipment::esc::RawCommand::FieldTypes::cmd::RawValueType::max();
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for (unsigned i = 0; i < num_outputs; i++) {
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if (_armed_mask & MOTOR_BIT(i)) {
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float scaled = (outputs[i] + 1.0F) * 0.5F * cmd_max;
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// trim negative values back to 0. Previously
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// we set this to 0.1, which meant motors kept
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// spinning when armed, but that should be a
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// policy decision for a specific vehicle
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// type, as it is not appropriate for all
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// types of vehicles (eg. fixed wing).
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if (scaled < 0.0F) {
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scaled = 0.0F;
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}
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if (scaled > cmd_max) {
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scaled = cmd_max;
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perf_count(_perfcnt_scaling_error);
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}
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msg.cmd.push_back(static_cast<int>(scaled));
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_esc_status.esc[i].esc_setpoint_raw = abs(static_cast<int>(scaled));
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} else {
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msg.cmd.push_back(static_cast<unsigned>(0));
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}
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}
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/*
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* Publish the command message to the bus
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* Note that for a quadrotor it takes one CAN frame
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*/
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(void)_uavcan_pub_raw_cmd.broadcast(msg);
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}
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void UavcanEscController::arm_all_escs(bool arm)
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{
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if (arm) {
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_armed_mask = -1;
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} else {
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_armed_mask = 0;
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}
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}
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void UavcanEscController::arm_single_esc(int num, bool arm)
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{
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if (arm) {
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_armed_mask = MOTOR_BIT(num);
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} else {
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_armed_mask = 0;
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}
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}
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void UavcanEscController::esc_status_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::esc::Status> &msg)
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{
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if (msg.esc_index < esc_status_s::CONNECTED_ESC_MAX) {
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_esc_status.esc_count = uavcan::max<int>(_esc_status.esc_count, msg.esc_index + 1);
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_esc_status.timestamp = msg.getMonotonicTimestamp().toUSec();
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auto &ref = _esc_status.esc[msg.esc_index];
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ref.esc_address = msg.getSrcNodeID().get();
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ref.esc_voltage = msg.voltage;
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ref.esc_current = msg.current;
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ref.esc_temperature = msg.temperature;
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ref.esc_setpoint = msg.power_rating_pct;
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ref.esc_rpm = msg.rpm;
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ref.esc_errorcount = msg.error_count;
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}
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}
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void UavcanEscController::orb_pub_timer_cb(const uavcan::TimerEvent &)
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{
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_esc_status.counter += 1;
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_esc_status.esc_connectiontype = esc_status_s::ESC_CONNECTION_TYPE_CAN;
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if (_esc_status_pub != nullptr) {
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(void)orb_publish(ORB_ID(esc_status), _esc_status_pub, &_esc_status);
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} else {
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_esc_status_pub = orb_advertise(ORB_ID(esc_status), &_esc_status);
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}
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}
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