matlab-基于模糊控制器的UAV行驶轨迹控制matlab仿真-源码

classdef QuadPlot < handle %QUADPLOT Visualization class for quad properties (SetAccess = public) k = 0; qn; % quad number time = 0; % time state; % state rot; % rotation matrix body to world color; % color of quad wingspan; % wingspan height; % height of quad motor; % motor position state_hist; % position history time_hist; % time history max_iter; % max iteration end properties (SetAccess = private) h_3d h_m13; % motor 1 and 3 handle h_m24; % motor 2 and 4 handle h_qz; % z axis of quad handle h_qn; % quad number handle h_pos_hist; % position history handle text_dist; % distance of quad number to quad end methods % Constructor function Q = QuadPlot(qn, state, wingspan, height, color, max_iter, h_3d) Q.qn = qn; Q.state = state; Q.wingspan = wingspan; Q.color = color; Q.height = height; Q.rot = QuatToRot(Q.state(7:10)); Q.motor = quad_pos(Q.state(1:3), Q.rot, Q.wingspan, Q.height); Q.text_dist = Q.wingspan / 3; Q.max_iter = max_iter; Q.state_hist = zeros(6, max_iter); Q.time_hist = zeros(1, max_iter); % Initialize plot handle if nargin < 7, h_3d = gca; end Q.h_3d = h_3d; hold(Q.h_3d, 'on') Q.h_pos_hist = plot3(Q.h_3d, Q.state(1), Q.state(2), Q.state(3), 'r.'); Q.h_m13 = plot3(Q.h_3d, ... Q.motor(1,[1 3]), ... Q.motor(2,[1 3]), ... Q.motor(3,[1 3]), ... '-ko', 'MarkerFaceColor', Q.color, 'MarkerSize', 5); Q.h_m24 = plot3(Q.h_3d, ... Q.motor(1,[2 4]), ... Q.motor(2,[2 4]), ... Q.motor(3,[2 4]), ... '-ko', 'MarkerFaceColor', Q.color, 'MarkerSize', 5); Q.h_qz = plot3(Q.h_3d, ... Q.motor(1,[5 6]), ... Q.motor(2,[5 6]), ... Q.motor(3,[5 6]), ... 'Color', Q.color, 'LineWidth', 2); Q.h_qn = text(... Q.motor(1,5) + Q.text_dist, ... Q.motor(2,5) + Q.text_dist, ... Q.motor(3,5) + Q.text_dist, num2str(qn)); hold(Q.h_3d, 'off') end % Update quad state function UpdateQuadState(Q, state, time) Q.state = state; Q.time = time; Q.rot = QuatToRot(state(7:10))'; % Q.rot needs to be body-to-world end % Update quad history function UpdateQuadHist(Q) Q.k = Q.k + 1; Q.time_hist(Q.k) = Q.time; Q.state_hist(:,Q.k) = Q.state(1:6); end % Update motor position function UpdateMotorPos(Q) Q.motor = quad_pos(Q.state(1:3), Q.rot, Q.wingspan, Q.height); end % Truncate history function TruncateHist(Q) Q.time_hist = Q.time_hist(1:Q.k); Q.state_hist = Q.state_hist(:, 1:Q.k); end % Update quad plot function UpdateQuadPlot(Q, state, time) Q.UpdateQuadState(state, time); Q.UpdateQuadHist(); Q.UpdateMotorPos(); set(Q.h_m13, ... 'XData', Q.motor(1,[1 3]), ... 'YData', Q.motor(2,[1 3]), ... 'ZData', Q.motor(3,[1 3])); set(Q.h_m24, ... 'XData', Q.motor(1,[2 4]), ... 'YData', Q.motor(2,[2 4]), ... 'ZData', Q.motor(3,[2 4])); set(Q.h_qz, ... 'XData', Q.motor(1,[5 6]), ... 'YData', Q.motor(2,[5 6]), ... 'ZData', Q.motor(3,[5 6])) set(Q.h_qn, 'Position', ... [Q.motor(1,5) + Q.text_dist, ... Q.motor(2,5) + Q.text_dist, ... Q.motor(3,5) + Q.text_dist]); set(Q.h_pos_hist, ... 'XData', Q.state_hist(1,1:Q.k), ... 'YData', Q.state_hist(2,1:Q.k), ... 'ZData', Q.state_hist(3,1:Q.k)); drawnow; end end end