| |
| |
| |
| |
|
|
| from isaaclab.app import AppLauncher |
|
|
| HEADLESS = True |
|
|
| |
| simulation_app = AppLauncher(headless=HEADLESS).app |
|
|
| """Rest of imports follows""" |
|
|
| from types import SimpleNamespace |
|
|
| import pytest |
| import torch |
|
|
|
|
| def make_thruster_cfg(num_motors: int): |
| """Create a minimal Thruster-like config object for tests.""" |
| return SimpleNamespace( |
| dt=0.01, |
| num_motors=num_motors, |
| thrust_range=(0.0, 10.0), |
| max_thrust_rate=100.0, |
| thrust_const_range=(0.05, 0.1), |
| tau_inc_range=(0.01, 0.02), |
| tau_dec_range=(0.01, 0.02), |
| torque_to_thrust_ratio=0.0, |
| use_discrete_approximation=True, |
| use_rps=True, |
| integration_scheme="euler", |
| ) |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [1, 2, 4]) |
| @pytest.mark.parametrize("num_motors", [1, 2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_zero_thrust_const_is_handled(num_envs, num_motors, device): |
| """When thrust_const_range contains zeros, Thruster clamps values and compute returns finite outputs.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
| cfg.thrust_const_range = (0.0, 0.0) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
| thruster_ids = slice(None) |
| init_rps = torch.ones(num_envs, num_motors, device=device) |
|
|
| thr = Thruster(cfg, thruster_names, thruster_ids, num_envs, device, init_rps) |
|
|
| command = torch.full((num_envs, num_motors), 1.0, device=device) |
| action = SimpleNamespace(thrusts=command.clone(), thruster_indices=thruster_ids) |
|
|
| thr.compute(action) |
|
|
| assert torch.isfinite(action.thrusts).all() |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [1, 2, 4]) |
| @pytest.mark.parametrize("num_motors", [1, 2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_negative_thrust_range_results_finite(num_envs, num_motors, device): |
| """Negative configured thrust ranges are clamped and yield finite outputs after hardening.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
| cfg.thrust_range = (-5.0, -1.0) |
| cfg.thrust_const_range = (0.05, 0.05) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
| thruster_ids = slice(None) |
| init_rps = torch.ones(num_envs, num_motors, device=device) |
|
|
| thr = Thruster(cfg, thruster_names, thruster_ids, num_envs, device, init_rps) |
|
|
| command = torch.full((num_envs, num_motors), -2.0, device=device) |
| action = SimpleNamespace(thrusts=command.clone(), thruster_indices=thruster_ids) |
|
|
| thr.compute(action) |
|
|
| assert torch.isfinite(action.thrusts).all() |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [2, 3, 4]) |
| @pytest.mark.parametrize("num_motors", [2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_tensor_vs_slice_indices_and_subset_reset(num_envs, num_motors, device): |
| """Compute should accept tensor or slice thruster indices, and reset_idx should affect only specified envs.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
| |
| motor_indices = [0, min(2, num_motors - 1)] |
| thruster_ids_tensor = torch.tensor(motor_indices, dtype=torch.int64, device=device) |
| thruster_ids_slice = slice(None) |
| init_rps = torch.ones(num_envs, num_motors, device=device) |
|
|
| thr_tensor = Thruster(cfg, thruster_names, thruster_ids_tensor, num_envs, device, init_rps) |
| thr_slice = Thruster(cfg, thruster_names, thruster_ids_slice, num_envs, device, init_rps) |
|
|
| command = torch.full((num_envs, num_motors), cfg.thrust_range[1] * 0.5, device=device) |
| action_tensor = SimpleNamespace(thrusts=command.clone(), thruster_indices=thruster_ids_tensor) |
| action_slice = SimpleNamespace(thrusts=command.clone(), thruster_indices=thruster_ids_slice) |
|
|
| thr_tensor.compute(action_tensor) |
| thr_slice.compute(action_slice) |
|
|
| assert action_tensor.thrusts.shape == (num_envs, num_motors) |
| assert action_slice.thrusts.shape == (num_envs, num_motors) |
|
|
| |
| env_to_reset = num_envs - 1 |
| prev = thr_tensor.curr_thrust.clone() |
| thr_tensor.reset_idx(torch.tensor([env_to_reset], dtype=torch.int64, device=device)) |
| assert not torch.allclose(prev[env_to_reset], thr_tensor.curr_thrust[env_to_reset]) |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [1, 2, 4]) |
| @pytest.mark.parametrize("num_motors", [1, 2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_mixing_and_integration_modes(num_envs, num_motors, device): |
| """Verify mixing factor selection and integration kernel choice reflect the config.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
|
|
| |
| cfg.use_discrete_approximation = True |
| cfg.integration_scheme = "euler" |
| thr_d = Thruster( |
| cfg, thruster_names, slice(None), num_envs, device, torch.ones(num_envs, num_motors, device=device) |
| ) |
| |
| assert getattr(thr_d.mixing_factor_function, "__func__", None) is Thruster.discrete_mixing_factor |
| assert getattr(thr_d._step_thrust, "__func__", None) is Thruster.compute_thrust_with_rpm_time_constant |
|
|
| |
| cfg.use_discrete_approximation = False |
| cfg.integration_scheme = "rk4" |
| thr_c = Thruster( |
| cfg, thruster_names, slice(None), num_envs, device, torch.ones(num_envs, num_motors, device=device) |
| ) |
| assert getattr(thr_c.mixing_factor_function, "__func__", None) is Thruster.continuous_mixing_factor |
| assert getattr(thr_c._step_thrust, "__func__", None) is Thruster.compute_thrust_with_rpm_time_constant_rk4 |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [1, 2, 4]) |
| @pytest.mark.parametrize("num_motors", [1, 2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_thruster_compute_clamps_and_shapes(num_envs, num_motors, device): |
| """Thruster.compute should return thrusts with correct shape and within clamp bounds.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
| thruster_ids = slice(None) |
| init_rps = torch.ones(num_envs, num_motors, device=device) |
|
|
| thr = Thruster(cfg, thruster_names, thruster_ids, num_envs, device, init_rps) |
|
|
| |
| command = torch.full((num_envs, num_motors), cfg.thrust_range[1] * 2.0, device=device) |
| action = SimpleNamespace(thrusts=command.clone(), thruster_indices=thruster_ids) |
|
|
| out = thr.compute(action) |
|
|
| assert out.thrusts.shape == (num_envs, num_motors) |
| |
| assert torch.all(out.thrusts <= cfg.thrust_range[1] + 1e-6) |
| assert torch.all(out.thrusts >= cfg.thrust_range[0] - 1e-6) |
|
|
|
|
| @pytest.mark.parametrize("num_envs", [1, 2, 4]) |
| @pytest.mark.parametrize("num_motors", [1, 2, 4]) |
| @pytest.mark.parametrize("device", ["cpu", "cuda"]) |
| def test_thruster_reset_idx_changes_state(num_envs, num_motors, device): |
| """reset_idx should re-sample parameters for specific env indices.""" |
| from isaaclab_contrib.actuators import Thruster |
|
|
| cfg = make_thruster_cfg(num_motors) |
|
|
| thruster_names = [f"t{i}" for i in range(num_motors)] |
| thruster_ids = slice(None) |
| init_rps = torch.ones(num_envs, num_motors, device=device) |
|
|
| thr = Thruster(cfg, thruster_names, thruster_ids, num_envs, device, init_rps) |
|
|
| |
| thr.tau_inc_s[0, 0] = thr.tau_inc_s[0, 0] + 1.0 |
| prev_val = thr.tau_inc_s[0, 0].item() |
|
|
| |
| thr.reset_idx(torch.tensor([0], dtype=torch.int64, device=device)) |
|
|
| |
| assert not torch.isclose(torch.tensor(prev_val, device=device), thr.tau_inc_s[0, 0]) |
|
|