SG_USING_STD(vector);
-FGOpenGC::FGOpenGC() {
+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/flaps", true)),
+ p_alphadot(fgGetNode("/fdm/jsbsim/aero/alphadot-radsec", true)),
+ p_betadot(fgGetNode("/fdm/jsbsim/aero/betadot-radsec", true))
+{
}
FGOpenGC::~FGOpenGC() {
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;
-static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
-
- data->version_id = 0x0012;
-
- data->longitude = fdm->get_Longitude_deg();
+ data->longitude = cur_fdm_state->get_Longitude_deg();
data->latitude = cur_fdm_state->get_Latitude_deg();
data->magvar = globals->get_mag()->get_magvar();
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_tas = cur_fdm_state->get_V_equiv_kts();
+ 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 = cur_fdm_state->get_Alpha_dot();
- data->beta_dot = cur_fdm_state->get_Beta_dot();
-
- data->static_temperature = cur_fdm_state->get_Static_temperature();
- data->total_temperature = cur_fdm_state->get_Total_temperature();
-
- data->static_pressure = cur_fdm_state->get_Static_pressure();
- data->total_pressure = cur_fdm_state->get_Total_pressure();
- data->dynamic_pressure = cur_fdm_state->get_Dynamic_pressure();
-
+ 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[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");
- data->egt[1] = fgGetDouble("/engines/engine[1]/egt-degf");
- data->egt[2] = fgGetDouble("/engines/engine[2]/egt-degf");
- data->egt[3] = fgGetDouble("/engines/engine[3]/egt-degf");
+
+ 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->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");
-
- data->fuel_flow[0] = fgGetDouble("/engines/engine[0]/fuel-flow-gph");
- data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph");
- data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph");
- data->fuel_flow[2] = fgGetDouble("/engines/engine[2]/fuel-flow-gph");
+// 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->gear_nose = p_gear[0]->GetPosition();
- //data->gear_left = p_gear[1]->GetPosition();
- //data->gear_right = p_gear[2]->GetPosition();
+ 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->aileron = globals->get_controls()->get_aileron();
- //data->aileron_trim = p_Controls->get_aileron_trim();
- data->elevator = globals->get_controls()->get_elevator();
- data->elevator_trim = globals->get_controls()->get_elevator_trim();
- data->rudder = globals->get_controls()->get_rudder();
- //data->rudder_trim = p_Controls->get_rudder_trim();
- //data->flaps = fgGetDouble("/controls/flaps");
- data->flaps = globals->get_controls()->get_flaps();
+ 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 ) {