import numpy as np from openpilot.common.constants import ACCELERATION_DUE_TO_GRAVITY from openpilot.common.realtime import DT_CTRL, DT_MDL MIN_SPEED = 1.0 CONTROL_N = 17 CAR_ROTATION_RADIUS = 0.0 # This is a turn radius smaller than most cars can achieve MAX_CURVATURE = 0.4 MAX_VEL_ERR = 5.0 # m/s MAX_LATERAL_JERK = 5.0 # m/s^3 MAX_LATERAL_ACCEL_NO_ROLL = 3.0 # m/s^2 MAX_LATERAL_ACCEL_NO_ROLL_OVERRIDE = 5.0 # m/s^2 DEFAULT_STOPPING_SPEED = 0.25 # m/s def should_stop(v_ego: float, a_target: float, stopping_speed: float = DEFAULT_STOPPING_SPEED) -> bool: return bool(v_ego < stopping_speed and a_target < 0.1) def clamp(val, min_val, max_val): clamped_val = float(np.clip(val, min_val, max_val)) return clamped_val, clamped_val != val def smooth_value(val, prev_val, tau, dt=DT_MDL): alpha = 1 - np.exp(-dt/tau) if tau > 0 else 1 return alpha * val + (1 - alpha) * prev_val # "Model smoothing": when the policy's own predicted uncertainty (plan_stds) for the # 1s-ahead lateral position spikes, temporarily lengthen the desiredCurvature smoothing # time constant so a noisy/uncertain model output doesn't jerk the wheel. MODEL_SMOOTHING_STD_LOW = 0.15 # m, plan y_std at 1s below which no extra smoothing is added MODEL_SMOOTHING_STD_HIGH = 0.25 # m, plan y_std at 1s at/above which the full max_extra_seconds is added MODEL_SMOOTHING_MAX_TOTAL_SEC = 0.60 # hard ceiling on base + dynamic lat smoothing seconds def dynamic_lat_smooth_extra_seconds(y_std_1s: float, max_extra_seconds: float) -> float: if max_extra_seconds <= 0.0: return 0.0 return float(np.interp(y_std_1s, [MODEL_SMOOTHING_STD_LOW, MODEL_SMOOTHING_STD_HIGH], [0.0, max_extra_seconds])) def clip_curvature(v_ego, prev_curvature, new_curvature, roll, override=False) -> tuple[float, bool]: # This function respects ISO lateral jerk and acceleration limits + a max curvature v_ego = max(v_ego, MIN_SPEED) max_curvature_rate = MAX_LATERAL_JERK / (v_ego ** 2) # inexact calculation, check https://github.com/commaai/openpilot/pull/24755 new_curvature = np.clip(new_curvature, prev_curvature - max_curvature_rate * DT_CTRL, prev_curvature + max_curvature_rate * DT_CTRL) max_lat_accel_no_roll = MAX_LATERAL_ACCEL_NO_ROLL_OVERRIDE if override else MAX_LATERAL_ACCEL_NO_ROLL roll_compensation = roll * ACCELERATION_DUE_TO_GRAVITY max_lat_accel = max_lat_accel_no_roll + roll_compensation min_lat_accel = -max_lat_accel_no_roll + roll_compensation new_curvature, limited_accel = clamp(new_curvature, min_lat_accel / v_ego ** 2, max_lat_accel / v_ego ** 2) new_curvature, limited_max_curv = clamp(new_curvature, -MAX_CURVATURE, MAX_CURVATURE) return float(new_curvature), limited_accel or limited_max_curv def get_accel_from_plan(speeds, accels, t_idxs, action_t=DT_MDL, stopping_speed=DEFAULT_STOPPING_SPEED): if len(speeds) == len(t_idxs): v_now = speeds[0] a_now = accels[0] v_target = np.interp(action_t, t_idxs, speeds) a_target = 2 * (v_target - v_now) / (action_t) - a_now else: v_now = 0.0 v_target = 0.0 a_target = 0.0 return a_target, should_stop(v_now, a_target, stopping_speed) def curv_from_psis(psi_target, psi_rate, vego, action_t): vego = np.clip(vego, MIN_SPEED, np.inf) curv_from_psi = psi_target / (vego * action_t) return 2*curv_from_psi - psi_rate / vego def get_curvature_from_plan(yaws, yaw_rates, t_idxs, vego, action_t): psi_target = np.interp(action_t, t_idxs, yaws) psi_rate = yaw_rates[0] return curv_from_psis(psi_target, psi_rate, vego, action_t)