Fix/system issues from parameter studies
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Fix issues discovered in systems_design through parameter studies
Fixes several small issues discovered through the parameter studies:
N.A.
Setting | Expected Result |
---|---|
/module_configuration_file/program_settings/systems_constants/environmental_control_system/off_on_take_off/value |
If set to true , the bleed air power requirement during the take-off segments of the mission (segment one) should be 0. Check in this file: ../reporting/plots/csv_files/systems_design_design_mission_power_ATA-21_plot.csv
|
/module_configuration_file/program_settings/systems_constants/flight_controls/ailerons/default_actuator_architecture_switch/value |
If set to true , changing values in /module_configuration_file/program_settings/systems_constants/flight_controls/ailerons/default_actuator_architecture will affect the mass of ATA27 (flight control system: /aircraft_exchange_file/component_design/systems/specific/geometry/mass_properties/flight_controls/value ) in the acxml. If it is set to false , changes in the default actuator architecture will have no effect. |
/module_configuration_file/program_settings/systems_constants/avionics/location_of_aviationics_bay/value |
Changing the avionics bay location will move the systems center of gravity slightly (systems CoG moves forward with setting 0->2->1). |