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: fuselageLocalCoeffInit.m
    path of file: ./repos/LADAC/aerodynamics/fuselage
    
    the code of the file until where you have to start completion: function coeff_loc = fuselageLocalCoeffInit( n_segments )
% fuselageLocalCoeffInit define and initialize fuselage local aerodynamic
% coefficients struct.
% 

    
function coeff_loc = fuselageLocalCoeffInit( n_segments )
% fuselageLocalCoeffInit define and initialize fuselage local aerodynamic
% coefficients struct.
% 
% Syntax:
%   coeff_loc = fuselageLocalCoeffInit( n_segments )
% 
% Inputs:
%   n_segments      number of segments for discretization
% 
% Outputs:
%   coeff_loc       fuselage local aerodynamic coefficient 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
coeff_loc.C_XYZ_b_i   	= zeros( 3, n_segments );

end