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flightgear/src/Network/opengc.cxx

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// opengc.cxx - Network interface program to send data to display processor over LAN
//
// Created by: J. Wojnaroski -- castle@mminternet.com
// Date: 21 Nov 2001
//
// Extended from original network code developed by C. Olson
//
// Modified 12/02/01 - Update engine structure for multi-engine models
// - Added data preamble to id msg types
//
// Modified 01/23/02 - Converted portions of the Engine and Gear accesssors to properties
// - Removed data from navigation functions. OpenGC provides own nav functions
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License as
// published by the Free Software Foundation; either version 2 of the
// License, or (at your option) any later version.
//
// This program is distributed in the hope that it will be useful, but
// WITHOUT ANY WARRANTY; without even the implied warranty of
// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
// General Public License for more details.
//
// You should have received a copy of the GNU General Public License
// along with this program; if not, write to the Free Software
// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
//
#include <simgear/debug/logstream.hxx>
#include <simgear/io/iochannel.hxx>
#include <vector>
#include "opengc.hxx"
#include <FDM/flight.hxx>
#include <Main/globals.hxx>
#include <Cockpit/radiostack.hxx>
#include <Controls/controls.hxx>
#include <Main/fg_props.hxx>
SG_USING_STD(vector);
FGOpenGC::FGOpenGC() :
press_node(fgGetNode("/environment/pressure-inhg", true)),
temp_node(fgGetNode("/environment/temperature-degc", true)),
wind_dir_node(fgGetNode("/environment/wind-from-heading-deg", true)),
wind_speed_node(fgGetNode("/environment/wind-speed-kt", true)),
p_left_aileron(fgGetNode("surface-positions/left-aileron-pos-norm", true)),
p_right_aileron(fgGetNode("surface-positions/right-aileron-pos-norm", true)),
p_elevator(fgGetNode("surface-positions/elevator-pos-norm", true)),
p_elevator_trim(fgGetNode("surface-positions/elevator_trim-pos-norm", true)),
p_rudder(fgGetNode("surface-positions/rudder-pos-norm", true)),
p_flaps(fgGetNode("surface-positions/flap-pos-norm", true)),
p_flaps_cmd(fgGetNode("/controls/flight/flaps", true)),
p_alphadot(fgGetNode("/fdm/jsbsim/aero/alphadot-radsec", true)),
p_betadot(fgGetNode("/fdm/jsbsim/aero/betadot-radsec", true))
{
}
FGOpenGC::~FGOpenGC() {
}
// open hailing frequencies
bool FGOpenGC::open() {
if ( is_enabled() ) {
SG_LOG( SG_IO, SG_ALERT, "This shouldn't happen, but the channel "
<< "is already in use, ignoring" );
return false;
}
SGIOChannel *io = get_io_channel();
if ( ! io->open( get_direction() ) ) {
SG_LOG( SG_IO, SG_ALERT, "Error opening channel communication layer." );
return false;
}
set_enabled( true );
return true;
}
//static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
void FGOpenGC::collect_data( const FGInterface *fdm, ogcFGData *data ) {
data->version_id = OGC_VERSION;
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data->longitude = cur_fdm_state->get_Longitude_deg();
data->latitude = cur_fdm_state->get_Latitude_deg();
data->magvar = globals->get_mag()->get_magvar();
data->pitch = cur_fdm_state->get_Theta_deg();
data->bank = cur_fdm_state->get_Phi_deg();
data->heading = cur_fdm_state->get_Psi_deg();
data->altitude = cur_fdm_state->get_Altitude();
data->altitude_agl = cur_fdm_state->get_Altitude_AGL();
data->v_kcas = cur_fdm_state->get_V_calibrated_kts();
data->vvi = cur_fdm_state->get_Climb_Rate();
data->mach = cur_fdm_state->get_Mach_number();
data->groundspeed = cur_fdm_state->get_V_ground_speed();
data->v_keas = cur_fdm_state->get_V_equiv_kts();
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data->phi_dot = cur_fdm_state->get_Phi_dot();
data->theta_dot = cur_fdm_state->get_Theta_dot();
data->psi_dot = cur_fdm_state->get_Psi_dot();
data->alpha = cur_fdm_state->get_Alpha();
data->beta = cur_fdm_state->get_Beta();
data->alpha_dot = p_alphadot->getDoubleValue();
data->beta_dot = p_betadot->getDoubleValue();
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//data->rudder_trim = p_Controls->get_rudder_trim();
data->left_aileron = p_left_aileron->getDoubleValue();
data->right_aileron = p_right_aileron->getDoubleValue();
data->elevator = p_elevator->getDoubleValue();
data->elevator_trim = p_elevator_trim->getDoubleValue();
data->rudder = p_rudder->getDoubleValue();
data->flaps = p_flaps->getDoubleValue();
data->flaps_cmd = p_flaps_cmd->getDoubleValue();
data->gear_nose = fgGetDouble("gear/gear[0]/position-norm");
data->gear_nose = fgGetDouble("gear/gear[1]/position-norm");
data->gear_nose = fgGetDouble("gear/gear[2]/position-norm");
data->gear_nose = fgGetDouble("gear/gear[3]/position-norm");
data->gear_nose = fgGetDouble("gear/gear[4]/position-norm");
data->rpm[0] = fgGetDouble("/engines/engine[0]/rpm");
data->rpm[1] = fgGetDouble("/engines/engine[1]/rpm");
data->epr[0] = fgGetDouble("/engines/engine[0]/epr");
data->epr[1] = fgGetDouble("/engines/engine[1]/epr");
data->epr[2] = fgGetDouble("/engines/engine[2]/epr");
data->epr[3] = fgGetDouble("/engines/engine[3]/epr");
data->egt[0] = (fgGetDouble("/engines/engine[0]/egt-degf") - 32.0) * 0.555;
data->egt[1] = (fgGetDouble("/engines/engine[1]/egt-degf") - 32.0) * 0.555;
data->egt[2] = (fgGetDouble("/engines/engine[2]/egt-degf") - 32.0) * 0.555;
data->egt[3] = (fgGetDouble("/engines/engine[3]/egt-degf") - 32.0) * 0.555;
data->n2_turbine[0] = fgGetDouble("/engines/engine[0]/n2");
data->n2_turbine[1] = fgGetDouble("/engines/engine[1]/n2");
data->n2_turbine[2] = fgGetDouble("/engines/engine[2]/n2");
data->n2_turbine[3] = fgGetDouble("/engines/engine[3]/n2");
data->n1_turbine[0] = fgGetDouble("/engines/engine[0]/n1");
data->n1_turbine[1] = fgGetDouble("/engines/engine[1]/n1");
data->n1_turbine[2] = fgGetDouble("/engines/engine[2]/n1");
data->n1_turbine[3] = fgGetDouble("/engines/engine[3]/n1");
// Convert gph to pph for turbine engines
data->fuel_flow[0] = fgGetDouble("/engines/engine[0]/fuel-flow-gph") * 6.5;
data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph") * 6.5;
data->fuel_flow[2] = fgGetDouble("/engines/engine[2]/fuel-flow-gph") * 6.5;
data->fuel_flow[3] = fgGetDouble("/engines/engine[3]/fuel-flow-gph") * 6.5;
data->oil_pressure[0] = fgGetDouble("/engines/engine[0]/oil-pressure-psi");
data->oil_pressure[1] = fgGetDouble("/engines/engine[1]/oil-pressure-psi");
data->oil_pressure[2] = fgGetDouble("/engines/engine[2]/oil-pressure-psi");
data->oil_pressure[3] = fgGetDouble("/engines/engine[3]/oil-pressure-psi");
// Just a few test numbers to test interface and drive EICAS displayss
for (int j=0; j<4; j++) data->oil_pressure[j] = 100.4 + 2.3*j;
data->man_pressure[0] = fgGetDouble("/engines/engine[0]/mp-osi");
data->man_pressure[1] = fgGetDouble("/engines/engine[1]/mp-osi");
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data->total_temperature = cur_fdm_state->get_Total_temperature();
data->total_pressure = cur_fdm_state->get_Total_pressure();
data->dynamic_pressure = cur_fdm_state->get_Dynamic_pressure();
data->static_pressure = press_node->getDoubleValue();
data->static_temperature = temp_node->getDoubleValue();
data->wind = wind_speed_node->getDoubleValue();
data->wind_dir = wind_dir_node->getDoubleValue();
}
static void distribute_data( const ogcFGData *data, FGInterface *chunk ) {
// just a place holder until the CDU is developed
}
// process work for this port
bool FGOpenGC::process() {
SGIOChannel *io = get_io_channel();
int length = sizeof(buf);
if ( get_direction() == SG_IO_OUT ) {
collect_data( cur_fdm_state, &buf );
//collect_data( &buf );
if ( ! io->write( (char *)(& buf), length ) ) {
SG_LOG( SG_IO, SG_ALERT, "Error writing data." );
return false;
}
} else if ( get_direction() == SG_IO_IN ) {
if ( io->get_type() == sgFileType ) {
if ( io->read( (char *)(& buf), length ) == length ) {
SG_LOG( SG_IO, SG_DEBUG, "Success reading data." );
distribute_data( &buf, cur_fdm_state );
}
} else {
while ( io->read( (char *)(& buf), length ) == length ) {
SG_LOG( SG_IO, SG_DEBUG, "Success reading data." );
distribute_data( &buf, cur_fdm_state );
}
}
}
return true;
}
// close the channel
bool FGOpenGC::close() {
SGIOChannel *io = get_io_channel();
set_enabled( false );
if ( ! io->close() ) {
return false;
}
return true;
}