Getting Started
AEIC Modules
PerformanceModel
PerformanceModel.create_performance_table()
PerformanceModel.initialize_performance()
PerformanceModel.read_performance_data()
config
missions
ac_params
engine_model
LTO_data
model_info
performance_table
performance_table_cols
performance_table_colnames
MATLAB
Bada3EngineModel
Bada3EngineModel.calculate_descent_thrust_app()
Bada3EngineModel.calculate_descent_thrust_high()
Bada3EngineModel.calculate_descent_thrust_land()
Bada3EngineModel.calculate_descent_thrust_low()
Bada3EngineModel.calculate_max_climb_thrust()
Bada3EngineModel.calculate_max_cruise_thrust()
Bada3JetEngineModel
Bada3JetEngineModel.calculate_cruise_fuel_flow()
Bada3JetEngineModel.calculate_max_climb_thrust_isa()
Bada3JetEngineModel.calculate_nominal_fuel_flow()
Bada3JetEngineModel.calculate_specific_fuel_consumption()
Bada3TurbopropEngineModel
Bada3TurbopropEngineModel.calculate_cruise_fuel_flow()
Bada3TurbopropEngineModel.calculate_max_climb_thrust_isa()
Bada3TurbopropEngineModel.calculate_nominal_fuel_flow()
Bada3TurbopropEngineModel.calculate_specific_fuel_consumption()
Bada3PistonEngineModel
Bada3PistonEngineModel.calculate_cruise_fuel_flow()
Bada3PistonEngineModel.calculate_max_climb_thrust_isa()
Bada3PistonEngineModel.calculate_nominal_fuel_flow()
Bada3PistonEngineModel.calculate_specific_fuel_consumption()
Bada3FuelBurnModel
Bada3FuelBurnModel.calculate_cd()
Bada3FuelBurnModel.calculate_cl()
Bada3FuelBurnModel.calculate_drag()
Bada3FuelBurnModel.calculate_specific_ground_range()
Bada3FuelBurnModel.calculate_thrust()
Bada3FuelBurnModel.calculate_thrust_by_total_energy()
Bada3FuelBurnModel.iterate_flight_simulation_constant_final_mass()
Bada3FuelBurnModel.iterate_flight_simulation_constant_initial_mass()
Bada3FuelBurnModel.iterate_flight_simulation_fuel_burn_dependent_initial_mass_rf_fraction()
Bada3FuelBurnModel.iterate_flight_simulation_fuel_burn_dependent_initial_mass_rf_value()
Bada3AircraftParameters
Bada3AircraftParameters.assign_parameters_fromdict()
Bada3AircraftParameters.get_params_asdict()
BaseAircraftParameters
BaseFuelBurnModel