RCAIDE.Library.Methods.Performance.compute_load_and_trim_diagram

compute_load_and_trim_diagram

compute_load_and_trim_diagram(mission=None, cruise_segment_tag='cruise', discretization=5)

Computes the loading dragram of an aircraft

Notes

# total number of sumulations = 2 * discretization ^ N # where 2: is for the loading and unloading cases # and N is the number of object types i.e cabin,cargo and fuel

compute_aircraft_load_data_point(vehicle, cruise_segment_tag, RES, counter, total_sims, neutral_point, percent_pax, percent_cargo, percent_fuel, f_o, p_i, c_i, f_i)

compute_aircraft_trim_data_point(vehicle, cruise_segment_tag, RES, counter, total_sims, neutral_point, w_i, c_g_i)