c90db01dc8
SimGear and TerraGear appear to have been split off at this time.
546 lines
14 KiB
C++
546 lines
14 KiB
C++
// fg_serial.cxx -- higher level serial port management routines
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//
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// Written by Curtis Olson, started November 1998.
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//
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// Copyright (C) 1998 Curtis L. Olson - curt@flightgear.org
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//
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// This program is free software; you can redistribute it and/or
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// modify it under the terms of the GNU General Public License as
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// published by the Free Software Foundation; either version 2 of the
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// License, or (at your option) any later version.
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//
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// This program is distributed in the hope that it will be useful, but
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// WITHOUT ANY WARRANTY; without even the implied warranty of
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// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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// General Public License for more details.
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//
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// You should have received a copy of the GNU General Public License
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// along with this program; if not, write to the Free Software
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// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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//
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// $Id$
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#include <Include/compiler.h>
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#ifdef FG_HAVE_STD_INCLUDES
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# include <cmath>
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# include <cstdlib> // atoi()
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#else
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# include <math.h>
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# include <stdlib.h> // atoi()
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#endif
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#include STL_STRING
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#include STL_IOSTREAM
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#include <vector>
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#include <Debug/logstream.hxx>
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#include <Aircraft/aircraft.hxx>
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#include <Include/fg_constants.h>
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#include <Serial/serial.hxx>
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#include <Time/fg_time.hxx>
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#include "options.hxx"
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#include "fg_serial.hxx"
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FG_USING_STD(string);
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FG_USING_STD(vector);
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// support an arbitrary number of serial channels. Each channel can
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// be assigned to an arbitrary port. Bi-directional communication is
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// supported by the underlying layer, but probably will never be
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// needed by FGFS?
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typedef vector < fgIOCHANNEL > io_container;
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typedef io_container::iterator io_iterator;
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typedef io_container::const_iterator const_io_iterator;
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// define the four channels
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io_container port_list;
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fgIOCHANNEL::fgIOCHANNEL() :
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kind( FG_SERIAL_DISABLED ),
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valid_config( false )
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{
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}
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fgIOCHANNEL::~fgIOCHANNEL() {
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}
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// configure a port based on the config string
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static fgIOCHANNEL parse_port_config( const string& config )
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{
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fgIOCHANNEL p;
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string::size_type begin, end;
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begin = 0;
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FG_LOG( FG_SERIAL, FG_INFO, "Parse serial port config: " << config );
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// device name
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end = config.find(",", begin);
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if ( end == string::npos ) {
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return p;
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}
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p.device = config.substr(begin, end - begin);
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begin = end + 1;
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FG_LOG( FG_SERIAL, FG_INFO, " device = " << p.device );
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// format
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end = config.find(",", begin);
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if ( end == string::npos ) {
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return p;
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}
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p.format = config.substr(begin, end - begin);
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begin = end + 1;
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FG_LOG( FG_SERIAL, FG_INFO, " format = " << p.format );
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// baud
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end = config.find(",", begin);
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if ( end == string::npos ) {
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return p;
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}
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p.baud = config.substr(begin, end - begin);
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begin = end + 1;
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FG_LOG( FG_SERIAL, FG_INFO, " baud = " << p.baud );
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// direction
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p.direction = config.substr(begin);
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FG_LOG( FG_SERIAL, FG_INFO, " direction = " << p.direction );
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p.valid_config = true;
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return p;
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}
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// configure a port based on the config info
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static bool config_port( fgIOCHANNEL &p )
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{
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if ( p.port.is_enabled() ) {
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FG_LOG( FG_SERIAL, FG_ALERT, "This shouldn't happen, but the port "
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<< "is already in use, ignoring" );
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return false;
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}
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if ( ! p.port.open_port( p.device ) ) {
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FG_LOG( FG_SERIAL, FG_ALERT, "Error opening device: " << p.device );
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return false;
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}
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// cout << "fd = " << p.port.fd << endl;
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if ( ! p.port.set_baud( atoi( p.baud.c_str() ) ) ) {
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FG_LOG( FG_SERIAL, FG_ALERT, "Error setting baud: " << p.baud );
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return false;
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}
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if ( p.format == "nmea" ) {
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if ( p.direction == "out" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_NMEA_OUT;
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} else if ( p.direction == "in" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_NMEA_IN;
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} else {
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FG_LOG( FG_SERIAL, FG_ALERT, "Unknown direction" );
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return false;
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}
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} else if ( p.format == "garmin" ) {
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if ( p.direction == "out" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_GARMIN_OUT;
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} else if ( p.direction == "in" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_GARMIN_IN;
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} else {
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FG_LOG( FG_SERIAL, FG_ALERT, "Unknown direction" );
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return false;
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}
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} else if ( p.format == "fgfs" ) {
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if ( p.direction == "out" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_FGFS_OUT;
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} else if ( p.direction == "in" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_FGFS_IN;
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} else {
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FG_LOG( FG_SERIAL, FG_ALERT, "Unknown direction" );
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return false;
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}
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} else if ( p.format == "rul" ) {
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if ( p.direction == "out" ) {
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p.kind = fgIOCHANNEL::FG_SERIAL_RUL_OUT;
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} else if ( p.direction == "in" ) {
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FG_LOG( FG_SERIAL, FG_ALERT, "RUL format is outgoing only" );
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return false;
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} else {
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FG_LOG( FG_SERIAL, FG_ALERT, "Unknown direction" );
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return false;
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}
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} else {
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FG_LOG( FG_SERIAL, FG_ALERT, "Unknown format" );
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return false;
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}
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return true;
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}
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// step through the port config streams (from fgOPTIONS) and setup
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// serial port channels for each
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void fgSerialInit() {
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fgIOCHANNEL port;
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bool result;
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str_container port_options_list = current_options.get_port_options_list();
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// we could almost do this in a single step except pushing a valid
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// port onto the port list copies the structure and destroys the
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// original, which closes the port and frees up the fd ... doh!!!
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// parse the configuration strings and store the results in stub
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// fgIOCHANNEL structures
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const_str_iterator current_str = port_options_list.begin();
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const_str_iterator last_str = port_options_list.end();
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for ( ; current_str != last_str; ++current_str ) {
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port = parse_port_config( *current_str );
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if ( port.valid_config ) {
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result = config_port( port );
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if ( result ) {
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port_list.push_back( port );
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}
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}
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}
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}
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char calc_nmea_cksum(char *sentence) {
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unsigned char sum = 0;
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int i, len;
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// printf("%s\n", sentence);
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len = strlen(sentence);
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sum = sentence[0];
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for ( i = 1; i < len; i++ ) {
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// printf("%c", sentence[i]);
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sum ^= sentence[i];
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}
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// printf("\n");
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// printf("sum = %02x\n", sum);
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return sum;
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}
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static void send_nmea_out( fgIOCHANNEL *p ) {
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char rmc[256], gga[256];
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char rmc_sum[10], gga_sum[10];
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char dir;
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int deg;
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double min;
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FGInterface *f;
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FGTime *t;
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f = current_aircraft.fdm_state;
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t = FGTime::cur_time_params;
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// run once every two seconds
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if ( p->last_time == t->get_cur_time() ) {
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return;
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}
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p->last_time = t->get_cur_time();
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if ( t->get_cur_time() % 2 != 0 ) {
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return;
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}
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char utc[10];
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sprintf( utc, "%02d%02d%02d",
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t->getGmt()->tm_hour, t->getGmt()->tm_min, t->getGmt()->tm_sec );
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char lat[20];
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double latd = f->get_Latitude() * RAD_TO_DEG;
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if ( latd < 0.0 ) {
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latd *= -1.0;
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dir = 'S';
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} else {
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dir = 'N';
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}
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deg = (int)(latd);
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min = (latd - (double)deg) * 60.0;
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sprintf( lat, "%02d%06.3f,%c", abs(deg), min, dir);
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char lon[20];
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double lond = f->get_Longitude() * RAD_TO_DEG;
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if ( lond < 0.0 ) {
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lond *= -1.0;
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dir = 'W';
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} else {
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dir = 'E';
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}
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deg = (int)(lond);
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min = (lond - (double)deg) * 60.0;
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sprintf( lon, "%03d%06.3f,%c", abs(deg), min, dir);
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char speed[10];
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sprintf( speed, "%05.1f", f->get_V_equiv_kts() );
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char heading[10];
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sprintf( heading, "%05.1f", f->get_Psi() * RAD_TO_DEG );
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char altitude_m[10];
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sprintf( altitude_m, "%02d", (int)(f->get_Altitude() * FEET_TO_METER) );
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char altitude_ft[10];
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sprintf( altitude_ft, "%02d", (int)f->get_Altitude() );
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char date[10];
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sprintf( date, "%02d%02d%02d", t->getGmt()->tm_mday,
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t->getGmt()->tm_mon+1, t->getGmt()->tm_year );
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// $GPRMC,HHMMSS,A,DDMM.MMM,N,DDDMM.MMM,W,XXX.X,XXX.X,DDMMYY,XXX.X,E*XX
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sprintf( rmc, "GPRMC,%s,A,%s,%s,%s,%s,%s,0.000,E",
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utc, lat, lon, speed, heading, date );
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sprintf( rmc_sum, "%02X", calc_nmea_cksum(rmc) );
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sprintf( gga, "GPGGA,%s,%s,%s,1,,,%s,F,,,,",
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utc, lat, lon, altitude_ft );
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sprintf( gga_sum, "%02X", calc_nmea_cksum(gga) );
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FG_LOG( FG_SERIAL, FG_DEBUG, rmc );
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FG_LOG( FG_SERIAL, FG_DEBUG, gga );
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// RMC sentence
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string rmc_sentence = "$";
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rmc_sentence += rmc;
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rmc_sentence += "*";
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rmc_sentence += rmc_sum;
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rmc_sentence += "\n";
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p->port.write_port(rmc_sentence);
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// cout << rmc_sentence;
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// GGA sentence
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string gga_sentence = "$";
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gga_sentence += gga;
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gga_sentence += "*";
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gga_sentence += gga_sum;
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gga_sentence += "\n";
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p->port.write_port(gga_sentence);
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// cout << gga_sentence;
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}
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static void read_nmea_in( fgIOCHANNEL *p ) {
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}
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static void send_garmin_out( fgIOCHANNEL *p ) {
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char rmc[256], rmc_sum[256], rmz[256], rmz_sum[256];
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char dir;
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int deg;
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double min;
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FGInterface *f;
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FGTime *t;
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f = current_aircraft.fdm_state;
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t = FGTime::cur_time_params;
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// run once per second
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if ( p->last_time == t->get_cur_time() ) {
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return;
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}
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p->last_time = t->get_cur_time();
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if ( t->get_cur_time() % 2 != 0 ) {
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return;
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}
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char utc[10];
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sprintf( utc, "%02d%02d%02d",
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t->getGmt()->tm_hour, t->getGmt()->tm_min, t->getGmt()->tm_sec );
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char lat[20];
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double latd = f->get_Latitude() * RAD_TO_DEG;
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if ( latd < 0.0 ) {
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latd *= -1.0;
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dir = 'S';
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} else {
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dir = 'N';
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}
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deg = (int)(latd);
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min = (latd - (double)deg) * 60.0;
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sprintf( lat, "%02d%06.3f,%c", abs(deg), min, dir);
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char lon[20];
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double lond = f->get_Longitude() * RAD_TO_DEG;
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if ( lond < 0.0 ) {
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lond *= -1.0;
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dir = 'W';
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} else {
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dir = 'E';
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}
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deg = (int)(lond);
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min = (lond - (double)deg) * 60.0;
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sprintf( lon, "%03d%06.3f,%c", abs(deg), min, dir);
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char speed[10];
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sprintf( speed, "%05.1f", f->get_V_equiv_kts() );
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char heading[10];
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sprintf( heading, "%05.1f", f->get_Psi() * RAD_TO_DEG );
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char altitude_m[10];
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sprintf( altitude_m, "%02d", (int)(f->get_Altitude() * FEET_TO_METER) );
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char altitude_ft[10];
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sprintf( altitude_ft, "%02d", (int)f->get_Altitude() );
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char date[10];
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sprintf( date, "%02d%02d%02d", t->getGmt()->tm_mday,
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t->getGmt()->tm_mon+1, t->getGmt()->tm_year );
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// $GPRMC,HHMMSS,A,DDMM.MMM,N,DDDMM.MMM,W,XXX.X,XXX.X,DDMMYY,XXX.X,E*XX
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sprintf( rmc, "GPRMC,%s,A,%s,%s,%s,%s,%s,000.0,E",
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utc, lat, lon, speed, heading, date );
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sprintf( rmc_sum, "%02X", calc_nmea_cksum(rmc) );
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// sprintf( gga, "$GPGGA,%s,%s,%s,1,04,0.0,%s,M,00.0,M,,*00\r\n",
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// utc, lat, lon, altitude_m );
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sprintf( rmz, "PGRMZ,%s,f,3", altitude_ft );
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sprintf( rmz_sum, "%02X", calc_nmea_cksum(rmz) );
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FG_LOG( FG_SERIAL, FG_DEBUG, rmc );
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FG_LOG( FG_SERIAL, FG_DEBUG, rmz );
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// RMC sentence
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string rmc_sentence = "$";
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rmc_sentence += rmc;
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rmc_sentence += "*";
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rmc_sentence += rmc_sum;
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rmc_sentence += "\n";
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p->port.write_port(rmc_sentence);
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// cout << rmc_sentence;
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// RMZ sentence (garmin proprietary)
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string rmz_sentence = "$";
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rmz_sentence += rmz;
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rmz_sentence += "*";
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rmz_sentence += rmz_sum;
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rmz_sentence += "\n";
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p->port.write_port(rmz_sentence);
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// cout << rmz_sentence;
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}
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static void read_garmin_in( fgIOCHANNEL *p ) {
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}
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static void send_fgfs_out( fgIOCHANNEL *p ) {
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}
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static void read_fgfs_in( fgIOCHANNEL *p ) {
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}
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// "RUL" output format (for some sort of motion platform)
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//
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// The Baud rate is 2400 , one start bit, eight data bits, 1 stop bit,
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// no parity.
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//
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// For position it requires a 3-byte data packet defined as follows:
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//
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// First bite: ascII character"p" ( 80 decimal )
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// Second byte X pos. (1-255) 1 being 0* and 255 being 359*
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// Third byte Y pos.( 1-255) 1 being 0* and 255 359*
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//
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// So sending 80 127 127 to the two axis motors will position on 180*
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// The RS- 232 port is a nine pin connector and the only pins used are
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// 3&5.
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static void send_rul_out( fgIOCHANNEL *p ) {
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char rul[256];
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FGInterface *f;
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FGTime *t;
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f = current_aircraft.fdm_state;
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t = FGTime::cur_time_params;
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// run as often as possibleonce per second
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// this runs once per second
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// if ( p->last_time == t->get_cur_time() ) {
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// return;
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// }
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// p->last_time = t->get_cur_time();
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// if ( t->get_cur_time() % 2 != 0 ) {
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// return;
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// }
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// get roll and pitch, convert to degrees
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double roll_deg = f->get_Phi() * RAD_TO_DEG;
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while ( roll_deg < -180.0 ) {
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roll_deg += 360.0;
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}
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while ( roll_deg > 180.0 ) {
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roll_deg -= 360.0;
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}
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double pitch_deg = f->get_Theta() * RAD_TO_DEG;
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while ( pitch_deg < -180.0 ) {
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pitch_deg += 360.0;
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}
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while ( pitch_deg > 180.0 ) {
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pitch_deg -= 360.0;
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}
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// scale roll and pitch to output format (1 - 255)
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// straight && level == (128, 128)
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int roll = (int)( (roll_deg+180.0) * 255.0 / 360.0) + 1;
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int pitch = (int)( (pitch_deg+180.0) * 255.0 / 360.0) + 1;
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sprintf( rul, "p%c%c\n", roll, pitch);
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|
|
|
FG_LOG( FG_SERIAL, FG_INFO, "p " << roll << " " << pitch );
|
|
|
|
string rul_sentence = rul;
|
|
p->port.write_port(rul_sentence);
|
|
}
|
|
|
|
|
|
// one more level of indirection ...
|
|
static void process_port( fgIOCHANNEL *p ) {
|
|
if ( p->kind == fgIOCHANNEL::FG_SERIAL_NMEA_OUT ) {
|
|
send_nmea_out(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_NMEA_IN ) {
|
|
read_nmea_in(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_GARMIN_OUT ) {
|
|
send_garmin_out(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_GARMIN_IN ) {
|
|
read_garmin_in(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_FGFS_OUT ) {
|
|
send_fgfs_out(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_FGFS_IN ) {
|
|
read_fgfs_in(p);
|
|
} else if ( p->kind == fgIOCHANNEL::FG_SERIAL_RUL_OUT ) {
|
|
send_rul_out(p);
|
|
}
|
|
}
|
|
|
|
|
|
// process any serial port work
|
|
void fgSerialProcess() {
|
|
fgIOCHANNEL *port;
|
|
|
|
io_iterator current = port_list.begin();
|
|
io_iterator last = port_list.end();
|
|
|
|
for ( ; current != last; ++current ) {
|
|
port = current;
|
|
if ( port->kind != fgIOCHANNEL::FG_SERIAL_DISABLED ) {
|
|
process_port ( port );
|
|
}
|
|
}
|
|
}
|