lwr_server/lwrserv/matlab/rvctools/simulink/quadrotor_plot.m

% Copyright (C) 1993-2011, by Peter I. Corke
%
% This file is part of The Robotics Toolbox for Matlab (RTB).
% 
% RTB is free software: you can redistribute it and/or modify
% it under the terms of the GNU Lesser General Public License as published by
% the Free Software Foundation, either version 3 of the License, or
% (at your option) any later version.
% 
% RTB is distributed in the hope that it will be useful,
% but WITHOUT ANY WARRANTY; without even the implied warranty of
% MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
% GNU Lesser General Public License for more details.
% 
% You should have received a copy of the GNU Leser General Public License
% along with RTB.  If not, see <http://www.gnu.org/licenses/>.
function [sys,x0,str,ts] = flyerplot3(t,x,u,flag,s,plot,enable)
% Flyer plot, lovingly coded by Paul Pounds, first coded 17/4/02
% version 2 2004 added scaling and ground display
% version 3 2010 improved rotor rendering and fixed mirroring bug
%
% Displays X-4 flyer position and attitude in a 3D plot.
% GREEN ROTOR POINTS NORTH
% BLUE ROTOR POINTS EAST

% PARAMETERS
% s defines the plot size in meters
% swi controls flyer attitude plot; 1 = on, otherwise off.

% INPUTS
% 1 Center X position
% 2 Center Y position
% 3 Center Z position
% 4 Yaw angle in rad
% 5 Pitch angle in rad
% 6 Roll angle in rad

% OUTPUTS
%   None
ts = [-1 0];

switch flag,
  case 0
    [sys,x0,str,ts] = mdlInitializeSizes(ts,plot,enable); % Initialization
  case 3
    sys = mdlOutputs(t,u,s,plot,enable); % Calculate outputs
  case {1,2, 4, 9} % Unused flags
    sys = [];
  otherwise
    error(['unhandled flag = ',num2str(flag)]); % Error handling
end


% Initialize
function [sys,x0,str,ts] = mdlInitializeSizes(ts,plot,enable)
% Call simsizes for a sizes structure, fill it in, and convert it 
% to a sizes array.
sizes = simsizes;
sizes.NumContStates  = 0;
sizes.NumDiscStates  = 0;
sizes.NumOutputs     = 0;
sizes.NumInputs      = 6;
sizes.DirFeedthrough = 1;
sizes.NumSampleTimes = 1;
sys = simsizes(sizes); 
x0  = [];
str = [];          % Set str to an empty matrix.
ts = [0.05 0];

if enable == 1
    figure(plot);
    clf;
    %colordef(1,'none');
end
% End of mdlInitializeSizes.


function sys = mdlOutputs(t,u,s,plot,enable)
global a1s b1s

    name = strcat('flyer_movie',num2str((t/0.125)*2+1),'r.bmp'); %odds
    %name = strcat('flyer_movie',num2str(160-(t/0.125)*2),'l.bmp'); %evens


if size(a1s) == [0 0];
    a1s = [0 0 0 0];
    b1s = [0 0 0 0];
end

d = 0.315; %Hub displacement from COG
r = 0.165; %Rotor radius
N = 1;
S = 2;
E = 3;
W = 4;
D(:,N) = [d;0;0]; %displacements
D(:,S) = [-d;0;0];
D(:,E) = [0;d;0];
D(:,W) = [0;-d;0];
C(:,N) = [s(1)/4;0;0]; %Attitude center displacements
C(:,S) = [-s(1)/4;0;0];
C(:,E) = [0;s(1)/4;0];
C(:,W) = [0;-s(1)/4;0];

if enable == 1
    %draw ground
    figure(plot);
    clf;
    if length(s) == 1
        axis([-s s -s s 0 s]);
    else
        axis([-s(1) s(1) -s(1) s(1) 0 s(2)])
        s = s(1);
    end
    hold on;

    plot3([-s -s],[s -s],[0 0],'-b')
    plot3([-s s],[s s],[0 0],'-b')
    plot3([s -s],[-s -s],[0 0],'-b')
    plot3([s s],[s -s],[0 0],'-b')
    plot3([s -s],[-s s],[0 0],'-b')
    plot3([-s s],[-s s],[0 0],'-b')

    %READ STATE
    z = [u(1);u(2);u(3)];
    n = [u(4);u(5);u(6)];
    
    %PREPROCESS ROTATION MATRIX
    phi = n(1);    %Euler angles
    the = n(2);
    psi = n(3);

    R = [cos(the)*cos(phi) sin(psi)*sin(the)*cos(phi)-cos(psi)*sin(phi) cos(psi)*sin(the)*cos(phi)+sin(psi)*sin(phi);   %BBF > Inertial rotation matrix
         cos(the)*sin(phi) sin(psi)*sin(the)*sin(phi)+cos(psi)*cos(phi) cos(psi)*sin(the)*sin(phi)-sin(psi)*cos(phi);
         -sin(the)         sin(psi)*cos(the)                            cos(psi)*cos(the)];

        %Manual Construction
        %Q3 = [cos(psi) -sin(psi) 0;sin(psi) cos(psi) 0;0 0 1];   %Rotation mappings
        %Q2 = [cos(the) 0 sin(the);0 1 0;-sin(the) 0 cos(the)];
        %Q1 = [1 0 0;0 cos(phi) -sin(phi);0 sin(phi) cos(phi)];
        %R = Q3*Q2*Q1;    %Rotation matrix
        
    %CALCULATE FLYER TIP POSITONS USING COORDINATE FRAME ROTATION
    F = [1 0 0;0 -1 0;0 0 -1];

    %Draw flyer rotors
    t = [0:pi/8:2*pi];
    for j = 1:length(t)
        circle(:,j) = [r*sin(t(j));r*cos(t(j));0];
    end
    
    for i = [N S E W]
        hub(:,i) = F*(z + R*D(:,i)); %points in the inertial frame
        
        q = 1; %Flapping angle scaling for output display - makes it easier to see what flapping is occurring
        Rr = [cos(q*a1s(i))  sin(q*b1s(i))*sin(q*a1s(i)) cos(q*b1s(i))*sin(q*a1s(i));   %Rotor > Plot frame
              0              cos(q*b1s(i))               -sin(q*b1s(i));
              -sin(q*a1s(i)) sin(q*b1s(i))*cos(q*a1s(i)) cos(q*b1s(i))*cos(q*a1s(i))];
       
        tippath(:,:,i) = F*R*Rr*circle;
        plot3([hub(1,i)+tippath(1,:,i)],[hub(2,i)+tippath(2,:,i)],[hub(3,i)+tippath(3,:,i)],'b-')
    end
     
 
    
    
    
    
    
    
    %     %Draw flyer
    plot3([hub(1,N) hub(1,S)],[hub(2,N) hub(2,S)],[hub(3,N) hub(3,S)],'-b')
    plot3([hub(1,E) hub(1,W)],[hub(2,E) hub(2,W)],[hub(3,E) hub(3,W)],'-b')
    plot3([hub(1,N)],[hub(2,N)],[hub(3,N)],'og')
    plot3([hub(1,S)],[hub(2,S)],[hub(3,S)],'or')
    plot3([hub(1,E)],[hub(2,E)],[hub(3,E)],'oc')
    plot3([hub(1,W)],[hub(2,W)],[hub(3,W)],'or')
    
   
    %Tracking lines
    plot3([z(1) 0],[-z(2) 0],[0 0],'--k')
    plot3([z(1)],[-z(2)],[0],'xk')
%    plot3([-s -s],[s s],[-z(3) 0],'--r')
%    plot3([-s],[s],[-z(3)],'xr')
    xlabel('x');
    ylabel('y');
    zlabel('z (height above ground)');
end
    
%saveas(1,name);

sys = [];
% End of mdlOutputs.