// 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 #include #include #include "opengc.hxx" #include #include
#include #include #include
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; 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(); 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(); //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"); 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; }