diff --git a/systems_design/src/common/aircraftSystems/ATAXX.cpp b/systems_design/src/common/aircraftSystems/ATAXX.cpp
index b204c515cab3b3f795aceb9809bd6796900a52d6..6e265d2232716866074e6d09e03c5b37f9ea439d 100644
--- a/systems_design/src/common/aircraftSystems/ATAXX.cpp
+++ b/systems_design/src/common/aircraftSystems/ATAXX.cpp
@@ -23,6 +23,7 @@
/* The following statements import necessary header files */
#include "ATAXX.h" // Import of header file from src/aircraftSystems folder for ATAXX
#include <runtimeInfo/runtimeInfo.h> // Import of header file from external runtime library for using runtimeInfo
+#include <aircraftGeometry2/processing/transform.h> //Import of header file for geometry transformation operations
/* Constructor for ATAXX */
ATAXX::ATAXX(const std::string& systemName, bool systemIsOperating, std::shared_ptr<systemsIOData> data, const RuntimeIO& rtIO)
@@ -159,9 +160,8 @@ Vec3 ATAXX::getRefPoint() {
this->refPtX_cockpit = 0.0;
this->refPtX_cockpit = data_->data.Accommodation.payload_tube_x_ref;
/* Auto Flight System, Navigation & Communication: Placement in Avionics Bay */
- if (avBayLocation == 0) {
- this->refPtX_avionicsBay = data_->theWing.at(0).aerodynamicSurface.sections.front().origin[0] -
- 0.25 * data_->theWing.at(0).aerodynamicSurface.sections.front().get_chord_length(); // Initial method
+ if (avBayLocation == 0) {//Location of avionics bay at wing root
+ this->refPtX_avionicsBay = data_->theWing.at(0).position[0]; // Initial method
} else if (avBayLocation == 1) {
this->refPtX_avionicsBay = this->refPtX_cockpit * 0.25; // Location of the avionics bay in the nose for business-jet-like AC; approximation: 25% of the cockpit length
} else if (avBayLocation == 2) {
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA21.cpp b/systems_design/src/common/aircraftSystems/conventionalATA21.cpp
index cd68d60a1220052474cc7ae76aece9c88c096a86..b6d2bd070630adb4cc65482dcfdcad8f6282505d 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA21.cpp
+++ b/systems_design/src/common/aircraftSystems/conventionalATA21.cpp
@@ -51,10 +51,8 @@ conventionalATA21::~conventionalATA21() {
void conventionalATA21::readParameters(const node& config) {
std::string unit;
scaling_factor = EndnodeReadOnly<double>("/module_configuration_file/program_settings/scaling_factors/environmental_control_system").read(config).value();
- offTakeOff = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/off_on_take_off/value");
- data_->configuration.checkForValidity(offTakeOff, 0, 1, "offOnTakeOff");
- ecoMode = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/eco_mode/value");
- data_->configuration.checkForValidity(ecoMode, 0, 1, "ecoMode");
+ offTakeOff = EndnodeReadOnly<bool>("/module_configuration_file/program_settings/systems_constants/environmental_control_system/off_on_take_off").read(config).value();
+ ecoMode = EndnodeReadOnly<bool>("/module_configuration_file/program_settings/systems_constants/environmental_control_system/eco_mode").read(config).value();
airflowPerPax = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/airflow_per_pax/value");
data_->configuration.checkForValidity(airflowPerPax, 0.0, 0.02, "airflowPerPax");
Recirculation = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/recirculation/value");
@@ -65,8 +63,6 @@ void conventionalATA21::readParameters(const node& config) {
data_->configuration.checkForValidity(heatSun, 0.0, 5000.0, "heatSun");
heatPerPAX = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/heat_per_pax/value");
data_->configuration.checkForValidity(heatPerPAX, 0.0, 500.0, "heatPerPAX");
- heatPerLightLength = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/heat_per_light_length/value");
- data_->configuration.checkForValidity(heatPerLightLength, 0.0, 500.0, "heatPerLightLength");
efficiencyFactor = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/efficiency_factor/value");
data_->configuration.checkForValidity(efficiencyFactor, 0.0, 1.0, "efficiencyFactor");
heatCapacityAir = config.at("/module_configuration_file/program_settings/systems_constants/environmental_control_system/heat_capacity_air/value");
@@ -251,7 +247,7 @@ void conventionalATA21::getPower(std::vector<double> existingHeatLoads) {
heatLoad.missionPower.at(i).baseLoad = (1. - efficiencyFactor) * (P_ACP
+ 0.1 * myElectricSum.missionPower.at(i).baseLoad);
//Switching off the air condition during takeoff
- if (offTakeOff == true && data_->mission.Steps.at(i).rating == "TO" && data_->mission.Steps.at(i).configuration == "TakeOff") {
+ if (offTakeOff == true && data_->mission.Steps.at(i).rating == "takeoff" && data_->mission.Steps.at(i).configuration == "takeoff") {
bleedAir.missionPower.at(i).baseLoad = 0.0;
heatLoad.missionPower.at(i).baseLoad = 0.0;
}
@@ -306,9 +302,9 @@ double conventionalATA21::getMass(double massFlowECS) {
/* Determination of the reference point */
Vec3 conventionalATA21::getRefPoint() {
/* Assumption: ECS is located in the belly fairing */
- return Vec3(data_->theWing.back().aerodynamicSurface.origin[0] +
+ return Vec3(data_->theWing.back().position[0] +
0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
- data_->theWing.back().aerodynamicSurface.origin[1], data_->theWing.back().aerodynamicSurface.origin[2]);
+ data_->theWing.back().position[1], data_->theWing.back().position[2]);
}
/* Determination of the heat flux for ACP */
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA21.h b/systems_design/src/common/aircraftSystems/conventionalATA21.h
index 48bd4637cea0887bf9760b0e97af866386aa6de8..24cc1a08d76725ccedc972b1db7804c0f4e15b2a 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA21.h
+++ b/systems_design/src/common/aircraftSystems/conventionalATA21.h
@@ -62,7 +62,6 @@ class conventionalATA21: public aircraftSystem {
double heatSun; /**< [W/m^2] heat from the sun **/
double windowArea; /**< [m^2] window area **/
double heatPerPAX; /**< [W] heat from each PAX **/
- double heatPerLightLength; /**< [W/m] heat per meter of lighting **/
double efficiencyFactor; /**< [---] efficiency factor of the ECS **/
double heatCapacityAir; /**< [J/(kg*K)] heat capacity of the air **/
bool offTakeOff; /**< switch if ECS is off during takeoff */
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA27.cpp b/systems_design/src/common/aircraftSystems/conventionalATA27.cpp
index 61ab640ac8a9360d80b216d4d717ab686696b571..55b8c338bec2aca0cdc647d9b15dc0e8f536d078 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA27.cpp
+++ b/systems_design/src/common/aircraftSystems/conventionalATA27.cpp
@@ -146,11 +146,11 @@ void conventionalATA27::readParameters(const node& config) {
myRuntimeInfo->err << "--> Abort!" << std::endl;
exit(1);
}
- flightControl.defaultAileronActuator = EndnodeReadOnly<bool>(flightControlConfig + "/ailerons/default_actuator_architecture").read(config).value();
- flightControl.defaultSpoilerActuator = EndnodeReadOnly<bool>(flightControlConfig + "/spoilers/default_actuator_architecture").read(config).value();
- flightControl.defaultElevatorActuator = EndnodeReadOnly<bool>(flightControlConfig + "/elevators/default_actuator_architecture").read(config).value();
- flightControl.defaultRudderActuator = EndnodeReadOnly<bool>(flightControlConfig + "/rudders/default_actuator_architecture").read(config).value();
- flightControl.defaultTHSAActuator = EndnodeReadOnly<bool>(flightControlConfig + "/trimmable_horizontal_stabilizer/default_actuator_architecture").read(config).value();
+ flightControl.defaultAileronActuator = EndnodeReadOnly<bool>(flightControlConfig + "/ailerons/default_actuator_architecture_switch").read(config).value();
+ flightControl.defaultSpoilerActuator = EndnodeReadOnly<bool>(flightControlConfig + "/spoilers/default_actuator_architecture_switch").read(config).value();
+ flightControl.defaultElevatorActuator = EndnodeReadOnly<bool>(flightControlConfig + "/elevators/default_actuator_architecture_switch").read(config).value();
+ flightControl.defaultRudderActuator = EndnodeReadOnly<bool>(flightControlConfig + "/rudders/default_actuator_architecture_switch").read(config).value();
+ flightControl.defaultTHSAActuator = EndnodeReadOnly<bool>(flightControlConfig + "/trimmable_horizontal_stabilizer/default_actuator_architecture_switch").read(config).value();
this->getAilerons(config);
this->getSpoilers(config);
@@ -1716,9 +1716,9 @@ Vec3 conventionalATA27::getRefPoint() {
// return Vec3(x_cg_ATA27, 0., z_cg_ATA27);
//alte Annahme: Schwerpunkt bei 45% Rumpflaenge
// return Vec3(fuselageRef[0]+0.45*fuselageLength, fuselageRef[1], fuselageRef[2]);
- return Vec3(data_->theWing.back().aerodynamicSurface.origin[0] +
+ return Vec3(data_->theWing.back().position[0] +
0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
- data_->theWing.back().aerodynamicSurface.origin[1], data_->theWing.back().aerodynamicSurface.origin[2]);
+ data_->theWing.back().position[1], data_->theWing.back().position[2]);
}
double conventionalATA27::getMaxDeflection(double minDeflection, double maxDeflection) {
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA29.cpp b/systems_design/src/common/aircraftSystems/conventionalATA29.cpp
index 5b96a288febb74c57b8d6aa9c7df462e2f3acc0c..f341520168e234a6ee52bc095ffdd3659816afb6 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA29.cpp
+++ b/systems_design/src/common/aircraftSystems/conventionalATA29.cpp
@@ -54,18 +54,6 @@ void conventionalATA29::readParameters(const node& config) {
scaling_factor = EndnodeReadOnly<double>("/module_configuration_file/program_settings/scaling_factors/hydraulic_system").read(config).value();
std::string unit;
std::string hydraulicSystemConfig = "/module_configuration_file/program_settings/systems_constants/hydraulic_system";
- unit = std::string(config.at(hydraulicSystemConfig + "/pressure/unit"));
- if (unit == "psi") {
- Pressure = 6894.76 * config.at(hydraulicSystemConfig + "/pressure/value");
- } else if (unit == "Pa") {
- Pressure = config.at(hydraulicSystemConfig + "/pressure/value");
- } else {
- Pressure = config.at(hydraulicSystemConfig + "/pressure/value");
- myRuntimeInfo->err << "The unit of hydraulic pressure is not known.!" << std::endl;
- myRuntimeInfo->err << "hydraulic pressure: " << Pressure << " " << unit << std::endl;
- exit(1);
- }
- data_->configuration.checkForValidity(Pressure, 6894.76 * 2500, 6894.76 * 10000, "Hydraulic.Pressure");
efficiencyFactorHydraulicSystem = config.at(hydraulicSystemConfig + "/efficiency_factor_hydraulic_system/value");
data_->configuration.checkForValidity(efficiencyFactorHydraulicSystem, 0.0, 1.0, "Hydraulic.efficiencyFactorHydraulicSystem");
maxRelPower = config.at(hydraulicSystemConfig + "/rel_max_power/value");
@@ -358,11 +346,6 @@ double conventionalATA29::getDuctingLength(const geom2::MultisectionSurface<geom
/* Determination of the reference point */
Vec3 conventionalATA29::getRefPoint() {
/* Assumption: hydraulic system is located in the belly fairing */
- return Vec3(data_->theWing.back().aerodynamicSurface.origin[0] + 0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
- data_->theWing.back().aerodynamicSurface.origin[1], data_->theWing.back().aerodynamicSurface.origin[2]);
-}
-
-/* Determination of hydraulic volume flow */
-double conventionalATA29::getHydraulicVolumeFlow(double Power, double Pressure) {
- return (Power / Pressure * (60 / 0.001));
+ return Vec3(data_->theWing.back().position[0] + 0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
+ data_->theWing.back().position[1], data_->theWing.back().position[2]);
}
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA29.h b/systems_design/src/common/aircraftSystems/conventionalATA29.h
index 00a9472ad3b1fcce0b39e35e56c7f5d63c80dddb..7c7591b3008c3c00ac0df6e2af5aeb8fb9e20758 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA29.h
+++ b/systems_design/src/common/aircraftSystems/conventionalATA29.h
@@ -55,7 +55,6 @@ class conventionalATA29: public aircraftSystem {
double lengthDucting; /**<[m] length of the ducting */
- double Pressure; /**< [Pa] Pressure of the hydraulic System **/
double efficiencyFactorHydraulicSystem;/**< [-] efficiency factor of the hydraulic system */
double maxRelPower;
double specificDuctingMass; /**< [kg/m] specific mass of hydraulic ducting */
@@ -117,13 +116,6 @@ class conventionalATA29: public aircraftSystem {
*/
Vec3 getRefPoint();
- /** \brief calculates the volume flow of the hydraulic system. UNUSED FUNCTION!
- * \param Power double: [W]
- * \param Pressure double: [N/m^2]
- * \return double: volume flow [kg/s]
- */
- double getHydraulicVolumeFlow(double Power, double Pressure); /** < Return of the volume flow [l/min] */
-
/** \brief Constructor of the hydraulic system
* \param systemName string
* \param systemIsOperating bool: Switch whether system is operating (1) or not (0)
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA32.cpp b/systems_design/src/common/aircraftSystems/conventionalATA32.cpp
index 6faed3a438f2906cb3ccbb4204a5cdd6029e0760..54b63e64d1a843d6d8c315096759ced291348cbc 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA32.cpp
+++ b/systems_design/src/common/aircraftSystems/conventionalATA32.cpp
@@ -40,7 +40,6 @@ conventionalATA32::~conventionalATA32() {
/* Reading system specific parameters of configuration xml file */
void conventionalATA32::readParameters(const node& config) {
- scaling_factor = EndnodeReadOnly<double>("/module_configuration_file/program_settings/scaling_factors/landing_gear_system").read(config).value();
efficiencyFactor = config.at("/module_configuration_file/program_settings/systems_constants/gear/efficiency_factor/value");
retractionTime = config.at("/module_configuration_file/program_settings/systems_constants/gear/retraction_time/value");
extensionTime = config.at("/module_configuration_file/program_settings/systems_constants/gear/extension_time/value");
@@ -99,6 +98,7 @@ void conventionalATA32::calculateSinkMass(const powerProfile& sourceBleed,
UNUSED(sourceElectric);
UNUSED(sourceHydraulic);
/* Calculate Systems Mass */
+ //landing gear mass is required for power calculation. It is not considered in total system mass since it is accounted for in landing_gear_design
if (data_->data.Mass.Gear > 0.0) {
Mass = data_->data.Mass.Gear;
refPoint = data_->data.CofG.landingGear;
@@ -191,7 +191,7 @@ void conventionalATA32::getPower() {
cleanPowerPeaks(&bleedAir);
}
double conventionalATA32::getMass() {
- //TODO(seabrooke): check that this is the landing gear actuation mass
+ //landing gear mass is required for power calculation but not considered for total system mass
return static_cast<double>(0.00271 * pow(data_->data.Mass.MLM, 1.24));
}
diff --git a/systems_design/src/common/aircraftSystems/conventionalATA36.cpp b/systems_design/src/common/aircraftSystems/conventionalATA36.cpp
index c2a4e9fb02ae92213840be37464a8fc5077d8761..b90bacade05342e09fe5075b465b1ea1a5d81176 100644
--- a/systems_design/src/common/aircraftSystems/conventionalATA36.cpp
+++ b/systems_design/src/common/aircraftSystems/conventionalATA36.cpp
@@ -175,7 +175,7 @@ double conventionalATA36::getMass() {
Vec3 conventionalATA36::getRefPoint() {
/* Assumption: the bleed air system is located in the belly fairing **/
- return Vec3(data_->theWing.back().aerodynamicSurface.origin[0] + 0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
- data_->theWing.back().aerodynamicSurface.origin[1],
- data_->theWing.back().aerodynamicSurface.origin[2]);
+ return Vec3(data_->theWing.back().position[0] + 0.5 * data_->theWing.back().aerodynamicSurface.sections.at(0).get_chord_length(),
+ data_->theWing.back().position[1],
+ data_->theWing.back().position[2]);
}
diff --git a/systems_design/src/common/systemsIOData.cpp b/systems_design/src/common/systemsIOData.cpp
index 2d7fd2eec9eeec804dfd6f78766269bdeb286798..8aa1cc810d5d06674ec8f6290539f08c9c1c88c2 100644
--- a/systems_design/src/common/systemsIOData.cpp
+++ b/systems_design/src/common/systemsIOData.cpp
@@ -95,6 +95,9 @@ void systemsIOData::readWing(const node& acxml, const std::string& airfoilDir) {
geom2::WingFactory theWingfactory{ACXML, airfoilDir}; // wing factory
for (size_t i = 0; i < wingVector.size(); i++) {
Wing newWing;
+ newWing.position[0] = EndnodeReadOnly<double>("aircraft_exchange_file/component_design/wing/position/x").read(acxml).value();
+ newWing.position[1] = EndnodeReadOnly<double>("aircraft_exchange_file/component_design/wing/position/y").read(acxml).value();
+ newWing.position[2] = EndnodeReadOnly<double>("aircraft_exchange_file/component_design/wing/position/z").read(acxml).value();
newWing.aerodynamicSurface = theWingfactory.create("wing/specific/geometry/aerodynamic_surface@0");
theWing.push_back(newWing);
myRuntimeInfo->out << "Create: " << theWing.at(i).aerodynamicSurface.name << " ..." << std::endl;
@@ -172,7 +175,7 @@ void systemsIOData::readFuselages(const node& acxml, const std::string& geometry
myRuntimeInfo->out << "Create: " << theFuselage.at(i).name << " ..." << std::endl;
/* Point between cockpit and cabin is needed for cable length / avionics positioning */
// current implementation only for TAW aircraft with one payload tube
- data.Accommodation.payload_tube_x_ref = fuselageVector[i]->at("/fuselage_accommodation/payload_tube@0/payload_tube_reference_points/front_reference_points/x/value");
+ data.Accommodation.payload_tube_x_ref = fuselageVector[i]->at("/fuselage_accommodation/position/x/value");
}
}
diff --git a/systems_design/src/common/systemsIOData.h b/systems_design/src/common/systemsIOData.h
index fe7c073d46129099d6854ae0fd9a6bcdca961f13..eaed585ed1178e9716bb3bb724ad9fdf8e40b84c 100644
--- a/systems_design/src/common/systemsIOData.h
+++ b/systems_design/src/common/systemsIOData.h
@@ -75,6 +75,7 @@ class systemsIOData {
class Wing {
public:
geom2::MultisectionSurface<geom2::AirfoilSection> aerodynamicSurface;/** aerodynamic surface of the wing*/
+ Vec3 position;/**[m] Wing root position*/
std::vector<geom2::MultisectionSurface<geom2::PolygonSection>> controlSurface;/** control surface of the wing*/
std::vector<double> controlDevicePosDeflection;/**[°] maximum pos. deflection of the control device*/
std::vector<double> controlDeviceNegDeflection;/**[°] maximum neg. deflection of the control device*/
diff --git a/systems_design/systems_design_conf.xml b/systems_design/systems_design_conf.xml
index 1c067f9c832284db5ef4c6dc0b005ef343ae95ef..d1a942dd840d560689845cb93afe84089ee40483 100644
--- a/systems_design/systems_design_conf.xml
+++ b/systems_design/systems_design_conf.xml
@@ -1,4 +1,4 @@
-<?xml version="1.0" encoding="utf-8" ?>
+<?xml version="1.0" encoding="utf-8" ?>
<module_configuration_file name="systems_design_conf.xml">
<control_settings description="General control settings for this tool">
<aircraft_exchange_file_name description="Specify the name of the exchange file">
@@ -105,13 +105,6 @@
<upper_boundary>inf</upper_boundary>
<default>1</default>
</ice_rain_protection_system>
- <landing_gear_system description="Scaling factor for the landing gear actuation.">
- <value>1</value>
- <unit>1</unit>
- <lower_boundary>0</lower_boundary>
- <upper_boundary>inf</upper_boundary>
- <default>1</default>
- </landing_gear_system>
<lighting_system description="Scaling factor for the lighting system.">
<value>1</value>
<unit>1</unit>
@@ -457,15 +450,12 @@
<unit>W</unit>
<default>75</default>
</heat_per_pax>
- <heat_per_light_length description="Heat emission per light specific cabin length">
- <value>40</value>
- <unit>W/m</unit>
- <default>40</default>
- </heat_per_light_length>
<efficiency_factor description="Efficiency of the ACP">
<value>0.7</value>
<unit>1</unit>
<default>0.7</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor>
<heat_capacity_air description="Heat capacity of air">
<value>1005.0</value>
@@ -473,14 +463,14 @@
<default>1005.0</default>
</heat_capacity_air>
<off_on_take_off description="Switch off ACP during take off (Airbus Getting Grips on Fuel Savings). Switch: true (ACP off during take off) / false (ACP always on)">
- <value>1</value>
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</off_on_take_off>
<eco_mode description="ECO Mode switch: 25% reduction in bleed air withdrawal (Airbus Getting Grips on Fuel Savings). Switch : true (ECO Mode) / false (normal mode)">
- <value>1</value>
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</eco_mode>
<shaft_power_sources description="Sources for possible existing shaft power consumption">
<number_of_power_sources description="Number of power sources">
@@ -618,6 +608,8 @@
<value>0.8</value>
<unit>1</unit>
<default>0.8</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor_electro_thermic_anti_icing>
<shaft_power_sources description="Sources for possible existing shaft power consumption">
<number_of_power_sources description="Number of power sources">
@@ -720,6 +712,8 @@
<value>0.95</value>
<unit>1</unit>
<default>0.95</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor>
<retraction_time description="Time to retract the landing gear">
<value>10.0</value>
@@ -780,6 +774,9 @@
<efficiency description="Actuator efficiency in average operation">
<value>0.85</value>
<default>0.85</default>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.</value>
@@ -797,10 +794,10 @@
<value>0.25</value>
<default>0.5</default>
</electric_flight_control_system_weight_factor>
- <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: 1 (true) / 0 (false)">
- <value>1</value>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: true / false">
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</default_actuator_architecture_switch>
<default_actuator_architecture description="Definition of the default actuator architecture">
<number_of_actuators_per_control_surface description="Number of actuators per control surface">
@@ -853,6 +850,8 @@
<value>0.85</value>
<unit>1</unit>
<default>0.85</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -883,6 +882,8 @@
<value>0.85</value>
<unit>1</unit>
<default>0.85</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -930,6 +931,8 @@
<value>0.85</value>
<unit>1</unit>
<default>0.85</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -960,6 +963,8 @@
<value>0.85</value>
<unit>1</unit>
<default>0.85</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -981,15 +986,15 @@
<value>0.25</value>
<default>0.5</default>
</electric_flight_control_system_weight_factor>
- <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: 1 (true) / 0 (false)">
- <value>1</value>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: true / false">
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</default_actuator_architecture_switch>
<default_actuator_architecture description="Definition of the default actuator architecture">
<number_of_actuators_per_control_surface description="Number of actuators per control surface">
<value>3</value>
- <unit></unit>
+ <unit>1</unit>
<default>3</default>
</number_of_actuators_per_control_surface>
<default_deflection_speed description="Deflection speed">
@@ -1033,6 +1038,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1062,6 +1069,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1091,6 +1100,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1120,6 +1131,8 @@
<value>1.</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1149,6 +1162,8 @@
<value>1.</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1171,10 +1186,10 @@
<unit></unit>
<default>0.5</default>
</electric_flight_control_system_weight_factor>
- <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: 1 (true) / 0 (false)">
- <value>1</value>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: true / false">
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</default_actuator_architecture_switch>
<default_actuator_architecture description="Definition of the default actuator architecture">
<number_of_actuators_per_control_surface description="Number of actuators per control surface">
@@ -1223,6 +1238,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1252,6 +1269,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1296,6 +1315,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1325,6 +1346,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1347,10 +1370,10 @@
<unit></unit>
<default>0.5</default>
</electric_flight_control_system_weight_factor>
- <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: 1 (true) / 0 (false)">
- <value>1</value>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: true / false">
+ <value>true</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</default_actuator_architecture_switch>
<default_actuator_architecture description="Definition of the default actuator architecture">
<number_of_actuators_per_control_surface description="Number of actuators per control surface">
@@ -1399,6 +1422,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1443,6 +1468,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1487,6 +1514,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1531,6 +1560,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1575,6 +1606,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1619,6 +1652,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1663,6 +1698,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1707,6 +1744,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1751,6 +1790,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1795,6 +1836,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1821,10 +1864,10 @@
<unit></unit>
<default>0.5</default>
</electric_flight_control_system_weight_factor>
- <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: 1 (true) / 0 (false)">
- <value>1</value>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture. Switch: true / false">
+ <value>ture</value>
<unit>1</unit>
- <default>1</default>
+ <default>true</default>
</default_actuator_architecture_switch>
<default_actuator_architecture description="Definition of the default actuator architecture">
<number_of_actuators_per_control_surface description="Number of actuators per control surface">
@@ -1872,6 +1915,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -1901,6 +1946,8 @@
<value>0.85</value>
<unit>1</unit>
<default>1.</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<standby_power description="Average basic power in standby operation (e.g. due to leakage)">
<value>0.0</value>
@@ -2131,20 +2178,19 @@
</specific_ducting_mass>
</bleed_air>
<hydraulic_system>
- <pressure description="Nominal pressure of the hydraulic system">
- <value>20684000</value>
- <unit>Pa</unit>
- <default>20684000</default>
- </pressure>
<efficiency_factor_hydraulic_system description="Efficiency of the hydraulic system, e.g. leakage losses">
<value>0.95</value>
<unit>1</unit>
<default>0.95</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor_hydraulic_system>
<rel_max_power description="Ratio of maximum permanent power and maximum required power of all pumps">
<value>1.0</value>
<unit>1</unit>
<default>1.0</default>
+ <lower_boundary>1.0</lower_boundary>
+ <upper_boundary>10.0</upper_boundary>
</rel_max_power>
<specific_ducting_mass description="Specific weight of hydraulic lines">
<value>2.5</value>
@@ -2204,6 +2250,8 @@
<value>0.85</value>
<unit>1</unit>
<default>0.85</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<operation_factor description="Percentage of total pump power in normal operation (value must be between">
<value>0.8</value>
@@ -2231,6 +2279,8 @@
<value>0.7</value>
<unit>1</unit>
<default>0.95</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency>
<operation_factor description="Percentage of total pump power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
<value>0.2</value>
@@ -2278,11 +2328,15 @@
<value>1.0</value>
<unit>1</unit>
<default>1.0</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor_electric_system>
<rel_max_power description="Ratio of maximum permanent power and maximum required power of all generators">
<value>1.0</value>
<unit>1</unit>
<default>1.0</default>
+ <lower_boundary>1.0</lower_boundary>
+ <upper_boundary>10.0</upper_boundary>
</rel_max_power>
<specific_cable_mass description="Specific weight of electrical wiring">
<value>6.5</value>
@@ -2314,6 +2368,8 @@
<value>0.665</value>
<unit>1</unit>
<default>0.665</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</generator_efficiency>
<operation_factor description="Share of total power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
<value>1</value>
@@ -2360,6 +2416,8 @@
<value>0.95</value>
<unit>1</unit>
<default>0.95</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor_bleed_air>
</propulsion_system>
<auxiliary_power_unit>
@@ -2387,6 +2445,8 @@
<value>0.90</value>
<unit>1</unit>
<default>0.90</default>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
</efficiency_factor_bleed_air>
<installation_factor description="Installation factor for attached parts such as fire protection, noise protection, etc.">
<value>1.5</value>
@@ -2412,8 +2472,8 @@
</design_loads>
</auxiliary_power_unit>
<avionics description="Components grouped inside ATAXX">
- <location_of_aviationics_bay description="0: Wing root, 1: Nose, 2: Behind cockpit">
- <value>0</value>
+ <location_of_aviationics_bay description="Selector: 0 (Wing root) / 1 (Nose) / 2 (Behind cockpit)">
+ <value>1</value>
<unit>1</unit>
<default>0</default>
</location_of_aviationics_bay>