%TR2RPY Convert a homogeneous transform to roll-pitch-yaw angles % % RPY = TR2RPY(T, options) are the roll-pitch-yaw angles expressed as a row % vector corresponding to the rotation part of a homogeneous transform T. % The 3 angles RPY=[R,P,Y] correspond to sequential rotations about % the X, Y and Z axes respectively. % % RPY = TR2RPY(R, options) are the roll-pitch-yaw angles expressed as a row % vector corresponding to the orthonormal rotation matrix R. % % If R or T represents a trajectory (has 3 dimensions), then each row of RPY % corresponds to a step of the trajectory. % % Options:: % 'deg' Compute angles in degrees (radians default) % 'zyx' Return solution for sequential rotations about Z, Y, X axes (Paul book) % % Notes:: % - There is a singularity for the case where P=pi/2 in which case R is arbitrarily % set to zero and Y is the sum (R+Y). % - Note that textbooks (Paul, Spong) use the rotation order ZYX. % % See also rpy2tr, tr2eul. % 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 . % TODO singularity for XYZ case, function rpy = tr2rpy(m, varargin) opt.deg = false; opt.zyx = false; opt = tb_optparse(opt, varargin); s = size(m); if length(s) > 2 rpy = zeros(s(3), 3); for i=1:s(3) rpy(i,:) = tr2rpy(m(:,:,i), varargin{:}); end return end rpy = zeros(1,3); if ~opt.zyx % XYZ order if abs(m(3,3)) < eps && abs(m(2,3)) < eps % singularity rpy(1) = 0; % roll is zero rpy(2) = atan2(m(1,3), m(3,3)); % pitch rpy(3) = atan2(m(2,1), m(2,2)); % yaw is sum of roll+yaw else rpy(1) = atan2(-m(2,3), m(3,3)); % roll % compute sin/cos of roll angle sr = sin(rpy(1)); cr = cos(rpy(1)); rpy(2) = atan2(m(1,3), cr * m(3,3) - sr * m(2,3)); % pitch rpy(3) = atan2(-m(1,2), m(1,1)); % yaw end else % old ZYX order (as per Paul book) if abs(m(1,1)) < eps && abs(m(2,1)) < eps % singularity rpy(1) = 0; % roll is zero rpy(2) = atan2(-m(3,1), m(1,1)); % pitch rpy(3) = atan2(-m(2,3), m(2,2)); % yaw is difference yaw-roll else rpy(1) = atan2(m(2,1), m(1,1)); sp = sin(rpy(1)); cp = cos(rpy(1)); rpy(2) = atan2(-m(3,1), cp * m(1,1) + sp * m(2,1)); rpy(3) = atan2(sp * m(1,3) - cp * m(2,3), cp*m(2,2) - sp*m(1,2)); end end if opt.deg rpy = rpy * 180/pi; end end