configJetControlParams.m

%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%                                                                         %
%               COEFFICIENTS FOR JET CONTROL MODELS                       %
%                                                                         %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

%% TURBINE MODEL COEFFICIENTS %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%
% ẋ  = F(x) + G(x)*u
%
% xdot(1,:) = Tdot;
% xdot(2,:) = K_T*T + K_TT*T^2 + K_D*Tdot + ... $x^2+e^{\pi i}$
%             K_DD*Tdot^2 + K_TD*T*Tdot + ...
%            (B_U + B_T*T + B_D*Tdot)*(u + B_UU*u^2) + c;

% Diesel parameters
%                      K_T        K_TT       K_D       K_DD      K_TD      Bᵤ        Bₜ         B_d       Bᵤᵤ        c
% Config.jetC_P160 = [-1.496760, -0.045206, -2.433030, 0.020352, 0.064188, 0.589177, 0.016715, -0.021258, 0.013878, -19.926756];
% Config.jetC_P220 = [-0.482993, -0.013562,  1.292093, 0.055923, 0.006887, 0.130662, 0.022564, -0.052168, 0.004485, -5.436267];

% Kerosene parameters
%                    K_T        K_TT       K_D       K_DD       K_TD      Bᵤ        Bₜ         B_d       Bᵤᵤ        c
Config.jetC_P100 = [-1.497225, -0.059093, -2.429288, 0.107146,  0.124828, 0.520267, 0.018470,  -0.046559,  0.014813, -19.928301];
Config.jetC_P160 = [ 0.306530, -0.024867, -0.973422, 0.055786,  0.022618, 0.688710, 0.038025,  -0.089879, -0.001393, -0.958953];
Config.jetC_P220 = [ 0.237755, -0.012799, -0.860374, 0.023606,  0.008599, 1.139026, 0.019914,  -0.050257,  0.000302, -0.692913 ];