use use function combine_se3_exp(w, ABt) = construct_Rt(rodrigues_so3_exp(w, ABt[0], ABt[1]), ABt[2]); // [A,B,t] function se3_exp_1(t,w) = concat( so3_exp_1(w*w), [t + 0.5 * cross(w,t)] ); function se3_exp_2(t,w) = se3_exp_2_0(t,w,w*w); function se3_exp_2_0(t,w,theta_sq) = se3_exp_23( so3_exp_2(theta_sq), C = (1.0 - theta_sq/20) / 6, t=t,w=w); function se3_exp_3(t,w) = se3_exp_3_0(t,w,sqrt(w*w)*180/PI,1/sqrt(w*w)); function se3_exp_3_0(t,w,theta_deg,inv_theta) = se3_exp_23( so3_exp_3_0(theta_deg = theta_deg, inv_theta = inv_theta), C = (1 - sin(theta_deg) * inv_theta) * (inv_theta * inv_theta), t=t,w=w); function se3_exp_23(AB,C,t,w) = [AB[0], AB[1], t + AB[1] * cross(w,t) + C * cross(w,cross(w,t)) ]; function se3_exp(mu) = se3_exp_0(t=take3(mu),w=tail3(mu)/180*PI); function se3_exp_0(t,w) = combine_se3_exp(w, // Evaluate by Taylor expansion when near 0 w*w < 1e-8 ? se3_exp_1(t,w) : w*w < 1e-6 ? se3_exp_2(t,w) : se3_exp_3(t,w) ); function se3_ln(m) = se3_ln_to_deg(se3_ln_rad(m)); function se3_ln_to_deg(v) = concat(take3(v),tail3(v)*180/PI); function se3_ln_rad(m) = se3_ln_0(m, rot = so3_ln_rad(rotation_part(m))); function se3_ln_0(m,rot) = se3_ln_1(m,rot, theta = sqrt(rot*rot)); function se3_ln_1(m,rot,theta) = se3_ln_2(m,rot,theta, shtot = theta > 0.00001 ? sin(theta/2*180/PI)/theta : 0.5, halfrotator = so3_exp_rad(rot * -.5)); function se3_ln_2(m,rot,theta,shtot,halfrotator) = concat( (halfrotator * translation_part(m) - (theta > 0.001 ? rot * ((translation_part(m) * rot) * (1-2*shtot) / (rot*rot)) : rot * ((translation_part(m) * rot)/24) )) / (2 * shtot), rot); __se3_test = [20,-40,60,-80,100,-120]; echo(UNITTEST_se3=norm(__se3_test-se3_ln(se3_exp(__se3_test))) < 1e-8);