Index

A

add_aircraft() (machupX.Scene method) aero_center() (machupX.Scene method)

airfoil (airfoil_db.DatabaseBoundsError attribute) airfoil_db (module)

C

control_derivatives() (machupX.Scene method)

D

damping_derivatives() (machupX.Scene method) DatabaseBoundsError (class in airfoil_db) derivatives() (machupX.Scene method)

display_planform() (machupX.Scene method) display_wireframe() (machupX.Scene method) distributions() (machupX.Scene method)

E

exception_indices (airfoil_db.DatabaseBoundsError attribute) export_dxf() (machupX.Scene method) export_pylot_model() (machupX.Scene method)

export_stl() (machupX.Scene method) export_stp() (machupX.Scene method) export_vtk() (machupX.Scene method)

G

get_aircraft_reference_geometry() (machupX.Scene method)

get_max_bound_vortex_length() (machupX.Scene method)

I

inputs_dict (airfoil_db.DatabaseBoundsError attribute)

M

MAC() (machupX.Scene method)

machupX (module), [1] message (airfoil_db.DatabaseBoundsError attribute)

O

out_gamma() (machupX.Scene method)

P

pitch_trim() (machupX.Scene method)

pitch_trim_using_orientation() (machupX.Scene method)

R

remove_aircraft() (machupX.Scene method)

S

Scene (class in machupX) set_aircraft_control_state() (machupX.Scene method) set_aircraft_state() (machupX.Scene method) set_err_state() (machupX.Scene method)

solve_forces() (machupX.Scene method) SolverNotConvergedError (class in machupX) stability_derivatives() (machupX.Scene method) state_derivatives() (machupX.Scene method)

T

target_CL() (machupX.Scene method)