Closed pavanvyn closed 3 years ago
Version b1aa18219634329d0c3092c5a9b7d9487ed81f89
configuration = "[2,2]" N_bodies = 4 masses = [5.7460828788155265, 8.357801422681348, 1.4648323385777384, 0.975317498667244] metallicities = [0.02997867474838753, 0.02997867474838753, 0.02997867474838753, 0.02997867474838753] semimajor_axes = [0.2818201949248253, 0.12278006722826543, 10.450979239812405] eccentricities = [0.23547098492944143, 0.5780702156414276, 0.5829107575734138] inclinations = [1.0951374930164222, 1.9667019164797899, 2.269031514165921] arguments_of_pericentre = [2.959631886126624, 2.7891867643123223, 2.5693711806875448] longitudes_of_ascending_node = [2.073510581755221, 4.465879312867095, 3.865192290024434] tend = 1.400000E+10 N_steps = 1000 stellar_types = [1, 1, 1, 1] object_types = [1, 1, 1, 1]
Error:
stellar_evolution.cpp -- compute_spin_angular_momentum_from_spin_frequency -- ERROR: quantity S is NaN nbody_evolution.cpp -- create_mstar_instance_of_system -- R->gbs_tolerance 1e-10 R->stopping_condition_tolerance 1e-10 R->output_time_tolerance 1e-06 nbody_evolution.cpp -- analyze_mstar_system -- starting integration U not finite.
The program does not return control to the terminal, but stalls after this point.
The problem was related to invalid spins being assigned in collision.cpp as a result of formally unbound initial collision/CE orbits that could occur in N-body mode. Should be fixed in 768c69b.
Version b1aa18219634329d0c3092c5a9b7d9487ed81f89
Error:
The program does not return control to the terminal, but stalls after this point.