```matlab
% Prompt the user to specify flight conditions
density = input('Enter the air density: ');
speed = input('Enter the airspeed: ');
altitude = input('Enter the altitude: ');
% Prompt the user to specify the body axis or wind axis
axis_choice = input('Enter the axis choice (body/wind): ');
% Prompt the user to enter system parameters
mass = input('Enter the mass: ');
inertia = input('Enter the inertia: ');
stability_derivatives = input('Enter the stability derivatives: ');
control_derivatives = input('Enter the control derivatives: ');
% Compute transfer functions for longitudinal and lateral-directional motions
if axis_choice == 'body'
% Compute longitudinal transfer functions
% ...
% Compute lateral-directional transfer functions
% ...
elseif axis_choice == 'wind'
% Compute longitudinal transfer functions
% ...
% Compute lateral-directional transfer functions
% ...
end
% Prompt the user to specify the transfer function to be displayed
tf_choice = input('Enter the transfer function to display: ');
% Display the selected transfer function
if tf_choice == 'longitudinal'
% Display longitudinal transfer function
% ...
elseif tf_choice == 'lateral-directional'
% Display lateral-directional transfer function
% ...
else
disp('Invalid transfer function choice.');
end
```