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attitude.m
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attitude.m
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% Main code to simulate all different controllers
%% Store states
N = length(tfs);
omegafs = zeros(N,length(omega));
omegadfs = zeros(N,length(omega));
controlfs = zeros(N,3);
Jfs{1} = zeros(N,6);
Jfs{2} = zeros(N,6);
Jhatfs{1} = zeros(N,6);
Jhatfs{2} = zeros(N,6);
efs_att = zeros(N,7);
angfs = zeros(N,3);
angdfs = zeros(N,3);
%% Arm length profile
% uncomment this if the arm lengths change
l_max = 0.2;
l_min = 0.1;
lfs = l_max*ones(length(tfs),1);
lfs(1:30000) = l_max;
lfs(30000:60000) = l_min;
lfs(60000:100000) = l_max;
lfs(100000:150000) = l_min;
l_arm_prev = lfs(1);
%% initialize J for each config
Jdot = zeros(3,3);
Jhat{1} = zeros(3,3);
Jhat{2} = zeros(3,3);
for i = 1:no_of_configs
if i == 1
l_arm = 0.3;
cg = calculate_cg(beta,M_Sph,m_point,l_arm,h_prop);
Jbarvec = current_J(beta,M_Sph,R_Sph,m_point,l_arm,h_prop);
Jhat{i} = [Jbarvec(1) Jbarvec(4) Jbarvec(5);...
Jbarvec(4) Jbarvec(2) Jbarvec(6);...
Jbarvec(5) Jbarvec(6) Jbarvec(3)];
elseif i == 2
l_arm = 0.1;
cg = calculate_cg(beta,M_Sph,m_point,l_arm,h_prop);
Jbarvec = current_J(beta,M_Sph,R_Sph,m_point,l_arm,h_prop);
Jhat{i} = [Jbarvec(1) Jbarvec(4) Jbarvec(5);...
Jbarvec(4) Jbarvec(2) Jbarvec(6);...
Jbarvec(5) Jbarvec(6) Jbarvec(3)];
end
end
Phat{1} = (0.5*trace(Jhat{1})*eye(3)) - (Jhat{1});
Phat{2} = (0.5*trace(Jhat{2})*eye(3)) - (Jhat{2});
%% reinitialize counter and arm length for starting simulation
i = 1;
l_arm = 0.3;
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% main code begins %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% main code begins %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%% main code
while t < tend-dt
Rd = eul2rotm([0 pi*cos(t)/9 pi*sin(t)/9]);
% calculate error in R
eRvee = 0.5*(G*Rd'*R-R'*Rd*G);
eR = [eRvee(3,2) eRvee(1,3) eRvee(2,1)]';
% calculate error in omega
if i == 1
omegad = [0 0 0]';
omegad_prev = omegad;
else
omegadvee = Rd'*((Rd-Rd_prev)/dt);
omegad = [omegadvee(3,2) omegadvee(1,3) omegadvee(2,1)]';
end
% for omegadot
if i > 2
omegadotd = (omegad - omegad_prev)/dt;
else
omegadotd = [0 0 0]';
end
eOmega = omega - R'*Rd*omegad;
% Get current arm length
l_arm = lfs(i);
% Set configuration
if abs(l_arm - l_arm_prev) > 0.05
config = next_config
next_config = previous_config;
previous_config = config;
end
% Calculate J from geometry
% get vector J
cg = calculate_cg(beta,M_Sph,m_point,l_arm,h_prop);
Jbarvec = current_J(beta,M_Sph,R_Sph,m_point,l_arm,h_prop);
% organize into the symmetric matrix
if config == 1
J{1} = [Jbarvec(1) Jbarvec(4) Jbarvec(5);...
Jbarvec(4) Jbarvec(2) Jbarvec(6);...
Jbarvec(5) Jbarvec(6) Jbarvec(3)] + diag([0.2 0.2 0.4]);
elseif config == 2
J{2} = [Jbarvec(1) Jbarvec(4) Jbarvec(5);...
Jbarvec(4) Jbarvec(2) Jbarvec(6);...
Jbarvec(5) Jbarvec(6) Jbarvec(3)] + diag([0.1 0.1 0.2]);
end
% Calculate alpha_D
alpha_D = - omegahat(omega)*R'*Rd*omegad + R'*Rd*omegadotd;
% MOI Estimator
switch estimator
case 'proposed_robust_adaptive'
eA_phat = eOmega + 0.5*eR;
[Phat{config}, Jhat{config}] = calculate_Jtilde(eA_phat, omega, alpha_D, Phat{config}, dt, J_gain);
case 'conventional_robust'
Jhat{config} = Jhat{config};
end
% Controller
switch estimator
case 'proposed_robust_adaptive'
eA = eOmega + c2*Jhat{config}^-1*eR;
mu = -delta_RAd^2*eA/(delta_RAd*norm(eA)+epsilon);
tau = -kR*eR -komega*eOmega + cross(omega, Jhat{config}*omega) + Jhat{config}*alpha_D + mu;
case 'conventional_robust'
eA = eOmega + c2*Jhat{config}^-1*eR;
mu = -delta_R^2*eA/(delta_R*norm(eA)+epsilon);
tau = -kR_lee*eR -komega_lee*eOmega + cross(omega, Jhat{config}*omega) + Jhat{config}*alpha_D + mu;
end
% State propagation
states = {omega, R};
control = {tau};
[omega, R] = dynamics(states,control,J{config},Jdot,Delta_R(i));
% Store full states
angfs(i,:) = rotm2eul(R);
angdfs(i,:) = rotm2eul(Rd);
if abs(angfs(end,3)) > deg2rad(maxRoll)
angfs(end,3) = sign(angfs(end,3))*deg2rad(maxRoll);
R = eul2rotm([angfs(end,1) angfs(end,2) angfs(end,3)]);
end
if abs(angfs(end,2)) > deg2rad(maxPitch)
angfs(end,2) = sign(angfs(end,2))*deg2rad(maxPitch);
R = eul2rotm([angfs(end,1) angfs(end,2) angfs(end,3)]);
end
omegafs(i,:) = omega';
omegadfs(i,:) = omegad';
Jfs{1,config}(i,:) = [J{1,config}(1) J{1,config}(5) J{1,config}(9) J{1,config}(2) J{1,config}(3) J{1,config}(6)];
Jhatfs{1,config}(i,:) = [Jhat{1,config}(1) Jhat{1,config}(5) Jhat{1,config}(9) Jhat{1,config}(2) Jhat{1,config}(3) Jhat{1,config}(6)];
% Update previous states
Rd_prev = Rd;
omegad_prev = omegad;
Jactprev = J;
Jhat_prev = Jhat;
l_arm_prev = l_arm;
% Store control
controlfs(i,:) = tau';
% store attitude errors
Psi = 0.5*trace(G*(eye(3) - Rd'*R));
efs_att(i,:) = [eR' eOmega' Psi];
% Update time, counter
t = t + dt;
i = i +1;
end
%% plot all data
plots