net->elevator_trim = node->getDoubleValue( "elevator-trim" );
net->rudder = node->getDoubleValue( "rudder" );
net->flaps = node->getDoubleValue( "flaps" );
- node = fgGetNode("/controls", true);
net->flaps_power
- = node->getDoubleValue( "/systems/electrical/outputs/flaps",
- 1.0 ) >= 1.0;
+ = fgGetDouble( "/systems/electrical/outputs/flaps", 1.0 ) >= 1.0;
+ net->flap_motor_ok = node->getBoolValue( "flaps-serviceable" );
+
net->num_engines = FGNetCtrls::FG_MAX_ENGINES;
for ( i = 0; i < FGNetCtrls::FG_MAX_ENGINES; ++i ) {
// Controls
tempnode = fgGetNode("/controls/gear", true);
for ( i = 0; i < FGNetCtrls::FG_MAX_WHEELS; ++i ) {
node = fgGetNode("/controls/gear/wheel", i);
- if ( node->getChild("brake") != NULL ) {
+ if ( node != NULL && node->getChild("brake") != NULL ) {
if ( tempnode->getChild("parking-brake")->getDoubleValue() > 0.0 ) {
net->brake[i] = 1.0;
} else {
net->turbulence_norm =
fgGetDouble("/environment/turbulence/magnitude-norm");
+ net->temp_c = fgGetDouble("/environment/temperature-degc");
+ net->press_inhg = fgGetDouble("/environment/pressure-sea-level-inhg");
+
// cur_fdm_state->get_ground_elev_ft() is what we want ... this
// reports the altitude of the aircraft.
// "/environment/ground-elevation-m" reports the ground elevation
htond(net->rudder);
htond(net->flaps);
net->flaps_power = htonl(net->flaps_power);
+ net->flap_motor_ok = htonl(net->flap_motor_ok);
for ( i = 0; i < FGNetCtrls::FG_MAX_ENGINES; ++i ) {
net->magnetos[i] = htonl(net->magnetos[i]);
net->starter_power[i] = htonl(net->starter_power[i]);
htond(net->wind_speed_kt);
htond(net->wind_dir_deg);
htond(net->turbulence_norm);
- htond(net->hground);
+ htond(net->temp_c);
+ htond(net->press_inhg);
+ htond(net->hground);
htond(net->magvar);
net->speedup = htonl(net->speedup);
net->freeze = htonl(net->freeze);
htond(net->rudder);
htond(net->flaps);
net->flaps_power = htonl(net->flaps_power);
+ net->flap_motor_ok = htonl(net->flap_motor_ok);
net->num_engines = htonl(net->num_engines);
for ( i = 0; i < net->num_engines; ++i ) {
net->magnetos[i] = htonl(net->magnetos[i]);
htond(net->wind_speed_kt);
htond(net->wind_dir_deg);
htond(net->turbulence_norm);
+ htond(net->temp_c);
+ htond(net->press_inhg);
htond(net->hground);
htond(net->magvar);
net->speedup = htonl(net->speedup);
node->setDoubleValue( "elevator-trim", net->elevator_trim );
node->setDoubleValue( "rudder", net->rudder );
node->setDoubleValue( "flaps", net->flaps );
-
fgSetBool( "/systems/electrical/outputs/flaps", net->flaps_power );
+ node->setBoolValue( "flaps-serviceable", net->flap_motor_ok );
for ( i = 0; i < FGNetCtrls::FG_MAX_ENGINES; ++i ) {
// Controls
}
for ( i = 0; i < FGNetCtrls::FG_MAX_WHEELS; ++i ) {
node = fgGetNode( "/controls/gear/wheel", i );
- node->getChild( "brake" )->setDoubleValue( net->brake[i] );
+ if ( node != NULL ) {
+ node->getChild( "brake" )->setDoubleValue( net->brake[i] );
+ }
}
node = fgGetNode( "/controls/gear", true );
node->setDoubleValue( "turbulence/magnitude-norm", net->turbulence_norm );
node->setBoolValue( "magnetic-variation-deg", net->magvar );
+ node->setDoubleValue( "/environment/temperature-degc",
+ net->temp_c );
+ node->setDoubleValue( "/environment/pressure-sea-level-inhg",
+ net->press_inhg );
+
// ground elevation ???
fgSetInt( "/sim/speed-up", net->speedup );