You are an expert in writing code in many different languages. Your goal is to perform code completion for the following code, keeping in mind the rest of the code and the file meta data.
    Metadata details:
    filename: fuselageLocalInflowInit.m
    path of file: ./repos/LADAC/aerodynamics/fuselage
    
    the code of the file until where you have to start completion: function local_inflow = fuselageLocalInflowInit( n_segments )
% fuselageLocalInflowInit define and initialize fuselage local inflow
% states struct.
% 
% Inputs:
%   n_segments      number of segments for discretization

    
function local_inflow = fuselageLocalInflowInit( n_segments )
% fuselageLocalInflowInit define and initialize fuselage local inflow
% states struct.
% 
% Inputs:
%   n_segments      number of segments for discretization
% 
% Outputs:
%   local_inflow    fuselage local inflow state struct (as defined by this
%                   function)
% 
% See also:
%   fuselageInit, fuselageStateInit
% 

% Disclamer:
%   SPDX-License-Identifier: GPL-3.0-only
% 
%   Copyright (C) 2020-2022 Yannic Beyer
%   Copyright (C) 2022 TU Braunschweig, Institute of Flight Guidance
% *************************************************************************

% airspeed at control point at the center line in body frame, in m/s
local_inflow.V      = zeros( 3, n_segments );
% local angle of attack at each border at the center line, in rad
local_inflow.alpha  = zeros( 1, n_segments + 1 );
% local sideslip angle at each border at the center line, in rad
local_inflow.beta   = zeros( 1, n_segments + 1 );

end