Luận án Nghiên cứu hệ thống xây dựng bản đồ, lập quỹ đạo và điều khiển bám quỹ đạo cho robot tự hành bốn bánh đa hướng

Đối với robot tự hành, chuyển động được đặt trên hệ toạ độ Đề-các Oxy, số bậc
tự do tối đa là 3 bậc bao gồm di chuyển tịnh tiến theo phương dọc, phương ngang và
theo góc quay của robot. Robot tự hành dạng phi holonom thông thường chỉ xét đến
2 bậc tự do điều khiển được là bậc tự do theo phương di chuyển tịnh tiến theo phương
dọc và di chuyển theo góc. Ngược lại robot tự hành dạng holonom xét đến đầy đủ cả
3 phương di chuyển, do đó nó tăng tính linh hoạt trong chuyển động của robot. Đặc
biệt, robot có thể di chuyển tức thời theo bất cứ phương nào mà không phụ thuộc vào
góc quay. Khác với các loại robot sử dụng bánh truyền thống (bánh tiêu chuẩn), robot
tự hành sử dụng bánh đa hướng có thêm các ưu điểm vượt trội như: khả năng thay
đổi vị trí và định hướng linh hoạt bởi chúng có khả năng tịnh tiến và quay đồng thời
hoặc độc lập (Hình 1.1).
Thông thường bánh xe được bố trí dọc theo trục của robot, nhưng đối với OMR
các bánh xe được bố trí theo một đường tròn ngoại tiếp robot để tận dụng các bậc tự
do của bánh đa hướng. Trong kỹ thuật điều khiển chuyển động của OMR, vấn đề điều
khiển bám quỹ đạo và tác động nhanh khi thay đổi tránh va chạm với vật cản là yêu
cầu cần thiết.
Ngoài ra, do có khả năng chuyển động linh hoạt nên OMR có khả năng tiết kiệm
năng lượng hơn so với robot sử dụng bánh xe thông thường. Nhờ những tính năng
vượt trội như vậy, OMR được ứng dụng ngày càng nhiều nhằm thay thế các loại robot
tự hành kiểu phi holonom truyền thống, nó được sử dụng nhiều trong các cần cẩu
nâng hạ, vận chuyển trong các kho bãi, robot tích hợp tay máy di chuyển trong các
nhà xưởng, robot thám hiểm, robot phục vụ lễ tân, robot y tế, robot quân sự … 
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  7. PL-2 [World.y, lmks_visible] = sen_rf.constrainMeasurement(World.y); enough_correlations = 0; last_scan_good = this_scan_good; pose_last_scan = pose_this_scan; this_scan_good = 0; % Initialise this_scan_good for this iteration scan_ref = World.scan_data; World.scan_data = -ones(3, numSegments * (round(sen.fov/sen.angular_res) + 1)); scan_ndx = 1; for i = 1:length(Obstacles) scan_data = Obstacles(i).getMeasured(sen, rob); if ~isempty(scan_data) World.scan_data(:, scan_ndx:scan_ndx+size(scan_data, 2)-1) = scan_data; scan_ndx = scan_ndx + size(scan_data, 2); end end World.scan_data = World.scan_data(:, World.scan_data(2, :) ~= -1); World.scan_data = removeDuplicateLasers(World.scan_data); World.scan_data = World.scan_data(2:3, :); % Remove index row v = repmat(sen.noise, 1, size(World.scan_data, 2)) .* randn(2,size(World.scan_data, 2)); World.scan_data = World.scan_data + v; if ~isempty(World.scan_data) obstaclesDetected = 1; World.scan_data = getInvMeasurement(World.scan_data); if size(World.scan_data, 2) > World.scan_corr_tolerance this_scan_good = 1; end else obstaclesDetected = 0; World.scan_global = []; end if last_scan_good && this_scan_good n = rob.q .* randn(2,1); % Noise in odometry measurement [R, T, correl, icp_var] = doICP(scan_ref, World.scan_data, 1, rob.u + n); if length(correl) > World.scan_corr_tolerance enough_correlations = 1;
  8. PL-4 weight_scan = 1; weight_odo = 0; end rob.r = weight_odo * dr_odo + weight_scan * dr_scan + rob.r; World.x(r) = rob.r; P_rr = World.P(r,r); World.P(r,:) = R_r * World.P(r,:); World.P(:,r) = World.P(r,:)'; World.P(r,r) = R_r * P_rr * R_r' + weight_scan * cov_scan + weight_odo * cov_odo; r_old = rob.r; lmks_visible_known = find(World.l(1,lmks_visible)); lids = lmks_visible(lmks_visible_known); for lid = lids [e, E_r, E_l] = scanPoint(rob.r, World.x(World.l(:,lid))); E_rl = [E_r E_l]; rl = [r World.l(:,lid)']; E = E_rl * World.P(rl,rl) * E_rl'; yi = World.y(:,lid); z = yi - e; z(2) = getPiToPi(z(2)); Z = World.M + E; K = World.P(:, rl) * E_rl' * Z^-1; World.x = World.x + K * z; World.P = World.P - K * Z * K'; rob.r = World.x(r); end lmks_visible_unknown = find(World.l(1,lmks_visible)==0); lids = lmks_visible(lmks_visible_unknown); if ~isempty(lids) for lid = lids s = find(World.mapspace, 2); if ~isempty(s) World.mapspace(s) = 0; World.l(:,lid) = s'; % Measurement yi = World.y(:,lid); [World.x(World.l(:,lid)), L_r, L_y] = invScanPoint(rob.r, yi);
  9. PL-6 odo_error = abs(dr_odo-dr_true); odo_error(3) = abs(getPiToPi(odo_error(3))); odo_error(1) = pdist([0 0; odo_error(1) odo_error(2)]); odo_error(2) = []; World.scan_error_hist(:, t) = scan_error; World.odo_error_hist(:, t) = odo_error; World.turning_hist(t) = rob.u(2); World.weight_scan_hist(t) = weight_scan; World.weight_odo_hist(t) = weight_odo; Graphics.lmks_all = lmks_all; Graphics.lmks_visible = lmks_visible; doGraphics(rob, World, Graphics, Obstacles(movingObstacles), AxesDir); end set(Graphics.R_hist, 'xdata', World.R_hist(1,:), 'ydata', World.R_hist(2, :)) set(Graphics.r_hist, 'xdata', World.r_hist(1,:), 'ydata', World.r_hist(2, :)) figure('color', 'white') subplot(2, 1, 1) plot(1:World.tend, World.error_hist) title('EKF SLAM: position error over time') xlabel('Time (s)'), ylabel('Position Error (m)') subplot(2, 1, 2) plot(1:World.tend, sqrt(World.Pr_hist(1, :)), 'r', 1:World.tend, sqrt(World.Pr_hist(2, :)), 'b') title('EKF SLAM: position uncertainty over time') xlabel('Time (s)'), ylabel('Standard Deviation (m)') legend('St. Dev. in x', 'St. Dev. in y') figure('color', 'white') subplot(4, 1, 1) AX = plotyy(1:World.tend, World.scan_error_hist(1,:), 1:World.tend, World.scan_error_hist(2,:), 'plot'); set(get(AX(1),'Ylabel'),'String',['Position' char(10) 'Error (m)']) set(get(AX(2),'Ylabel'),'String',['Angular' char(10) 'Error (rad)']) title('Scan errors over time') xlabel('Time (s)') subplot(4, 1, 2) AX2 = plotyy(1:World.tend, World.odo_error_hist(1,:), 1:World.tend, World.odo_error_hist(2,:), 'plot'); set(get(AX2(1),'Ylabel'),'String',['Position' char(10) 'Error (m)'])
  10. PL-8 f = Function('f',{states,controls},{rhs}); % Nonlinear mapping function f(x,u) U = SX.sym('U',n_controls,N); % Control variables P = SX.sym('P',n_states + N*(n_states + n_controls)); X = SX.sym('X',n_states,(N+1)); obj = 0; % Objective function g = []; % constraints vector st = X(:,1); % Initial state g = [g;st-P(1:3)]; % Initial condition constraints % Euler discretization for k = 1:N st = X(:,k); con = U(:,k); obj = obj+(st-P(6*k-2:6*k+0))'*Q*(st-P(6*k-2:6*k+0)) + (con-P(6*k+1:6*k+3))'*R*(con-P(6*k+1:6*k+3)) ; % calculate obj % The number 6 is (n_states+n_controls) st_next = X(:,k+1); f_value = f(st,con); st_next_euler = st+ (T*f_value); g = [g;st_next-st_next_euler]; % compute constraints end % Make the decision variable one column vector OPT_variables = [reshape(X,3*(N+1),1);reshape(U,3*N,1)]; nlp_prob = struct('f', obj, 'x', OPT_variables, 'g', g, 'p', P); opts = struct; opts.ipopt.max_iter = 2000; opts.ipopt.print_level =0;%0,3 opts.print_time = 0; opts.ipopt.acceptable_tol =1e-8; opts.ipopt.acceptable_obj_change_tol = 1e-6; solver = nlpsol('solver', 'ipopt', nlp_prob, opts); args = struct; args.lbg(1:3*(N+1)) = 0; % Equality constraints args.ubg(1:3*(N+1)) = 0; % Equality constraints args.lbx(1:3:3*(N+1),1) = x_min; % State x lower bound
  11. PL-10 u = reshape(full(sol.x(3*(N+1)+1:end))',3,N)'; y = u(1,:); end
  12. PL-12 #define Ts 0.1 // sampling time #define Lf 1.0 /* Global variables used by the solver. */ ACADOvariables acadoVariables; ACADOworkspace acadoWorkspace; // MPC init functions vector > init_acado(); void init_weight(); vector > run_mpc_acado(vector states, vector ref_states, vector > previous_u); vector calculate_ref_states(const vector &ref_x, const vector &ref_y, const vector &ref_q, const double &reference_vx, const double &reference_vy, const double &reference_w); vector motion_prediction(const vector &cur_states, const vector > &prev_u); vector update_states(vector state, double vx_cmd, double vy_cmd, double w_cmd); /* ROS PARAMS*/ double weight_x, weight_y, weight_q, weight_vx, weight_vy, weight_w; nav_msgs::Odometry odom; void stateCallback(const nav_msgs::Odometry& msg) { odom = msg; } nav_msgs::Path path; void pathCallback(const nav_msgs::Path& msg) { path = msg; } bool is_target(nav_msgs::Odometry cur, double goal_x, double goal_y) {
  13. PL-14 nav_msgs::Path odom_path; odom_path.header.frame_id = "/odom"; odom_path.header.stamp = ros::Time::now(); vector > control_output; control_output = init_acado(); // cout cur_state = {px, py, pq}; // Update odom path geometry_msgs::PoseStamped cur_pose; cur_pose.header = odom_path.header; cur_pose.pose.position.x = px; cur_pose.pose.position.y = py; cur_pose.pose.orientation.w = 1.0;
  14. PL-16 nav_msgs::Path predict_path; predict_path.header.frame_id = "/odom"; predict_path.header.stamp = ros::Time::now(); for (int i = 0; i = path.poses.size(); if(goal) { vel.linear.x = 0; vel.linear.y = 0; vel.angular.z = 0; // cout << "Done!" << endl; } else { vel.linear.x = control_output[0][0]; vel.linear.y = control_output[1][0]; vel.angular.z = control_output[2][0]; } vel_pub.publish(vel); ros::spinOnce(); r.sleep(); count++; } return 0; } void init_weight() { for (int i = 0; i < N; i++) { // Setup diagonal entries
  15. PL-18 else if(j == 1 ) { control_output_vy.push_back(acadoVariables.u[i * ACADO_NU + j]); } else { control_output_w.push_back(acadoVariables.u[i * ACADO_NU + j]); } } } init_weight(); return {control_output_vx, control_output_vy, control_output_w}; } vector > run_mpc_acado(vector states, vector ref_states, vector > previous_u) { /* Some temporary variables. */ int i, iter; acado_timer t; /* Initialize the states and controls. */ for (i = 0; i < NX * (N + 1); ++i) { acadoVariables.x[ i ] = (real_t) states[i]; } for (i = 0; i < NX; ++i) { acadoVariables.x0[i] = (real_t)states[i]; } /* Initialize the measurements/reference. */ for (i = 0; i < NY * N; ++i) { acadoVariables.y[i] = (real_t)ref_states[i]; } for (i = 0; i < NYN; ++i) { acadoVariables.yN[i] = (real_t)ref_states[NY * (N - 1) + i]; }
  16. PL-20 /* Read the elapsed time. */ real_t te = acado_toc(&t); vector control_output_vx; vector control_output_vy; vector control_output_w; real_t *u = acado_getVariablesU(); for (int i = 0; i calculate_ref_states(const vector &ref_x, const vector &ref_y, const vector &ref_q, const double &reference_vx, const double &reference_vy, const double &reference_w) { vector result;
  17. PL-22 if (cur_state[3] next_state = update_states(cur_state, old_vx_cmd[i], old_vy_cmd[i], old_w_cmd[i]); predicted_states.push_back(next_state); } vector result; for (int i = 0; i < (ACADO_N + 1); ++i) { for (int j = 0; j < NX; ++j) { result.push_back(predicted_states[i][j]); } } return result; }