inc_rock.m

导弹控制系统的鲁棒控制设计实例

function x0 = inc_rock
%
% Initial conditions for simulation of the rocket stabilization system.
t = 14;    % s
sol_rock
%
% Unperturbed motion
%   x(1) = V
%   x(2) = H
%   x(3) = Theta
%
% Perturbed motion
%   x(1)  = V
%   x(2)  = H
%   x(3)  = Theta
%   x(4)  = Psi
%   x(5)  = omega_x
%   x(6)  = omega_y
%   x(7)  = omega_z
%   x(8)  = psi
%   x(9)  = theta
%   x(10) = gamma 
%
%     1    2    3    4   5   6   7   8   9  10
x0 = [V    H  Theta  0   0   0   0   0   0  0]';