IQ.Pilot Release Commit @ 0798119

tools/lateral_maneuvers/sim_maneuvers.py

@@ -0,0 +1,73 @@
+#!/usr/bin/env python3
+"""Run lateral_maneuversd against a synthetic lateral plant and write an rlog.
+
+    ./tools/lateral_maneuvers/sim_maneuvers.py --out /tmp/lat_rlog.zst
+    ./tools/lateral_maneuvers/generate_report.py /tmp/lat_rlog.zst
+"""
+import argparse
+import re
+from pathlib import Path
+
+from openpilot.common.constants import CV
+from openpilot.tools.lateral_maneuvers.lateral_maneuversd import MANEUVERS
+from openpilot.tools.longitudinal_maneuvers.sim_harness import ManeuverSim, Plant
+
+CURV_TAU = 0.05  # controlsd curvature command tracking
+RACK_WN = 8.0    # steering rack + tire natural frequency (rad/s)
+RACK_ZETA = 0.7  # underdamped, so achieved curvature overshoots like a real rack
+CRUISE_ACCEL = 1.2
+
+SET_SPEED_RE = re.compile(r"Set speed to (\d+) mph")
+
+
+class LateralPlant(Plant):
+  PLAN = 'lateralManeuverPlan'
+
+  def __init__(self):
+    super().__init__(v_ego=MANEUVERS[0].initial_speed)
+    self.sim = None
+    self._rack_rate = 0.0
+    self.target_speed = MANEUVERS[0].initial_speed
+    self._by_description = {m.description: m.initial_speed for m in MANEUVERS}
+
+  def _update_target(self):
+    if self.sim is None:
+      return
+    speed = self._by_description.get(self.sim.alert2)
+    if speed is None:
+      match = SET_SPEED_RE.search(self.sim.alert1)
+      speed = float(match.group(1)) * CV.MPH_TO_MS if match else None
+    if speed is not None:
+      self.target_speed = speed
+
+  def step(self, dt, plan):
+    self._update_target()
+
+    err = self.target_speed - self.v_ego
+    self.a_ego = max(min(err / 1.0, CRUISE_ACCEL), -CRUISE_ACCEL)
+    self.v_ego = max(self.v_ego + self.a_ego * dt, 0.0)
+
+    desired_curvature = float(plan.desiredCurvature) if plan is not None else 0.0
+    self.curvature += (dt / (CURV_TAU + dt)) * (desired_curvature - self.curvature)
+
+    self._rack_rate += dt * (RACK_WN ** 2 * (self.curvature - self.achieved_curvature) - 2 * RACK_ZETA * RACK_WN * self._rack_rate)
+    self.achieved_curvature += dt * self._rack_rate
+    self.lat_accel = self.achieved_curvature * max(self.v_ego, 1.0) ** 2
+
+
+def main():
+  parser = argparse.ArgumentParser(description=__doc__)
+  parser.add_argument("--out", type=Path, default=Path("/tmp/lateral_maneuvers_sim/rlog.zst"))
+  parser.add_argument("--max-maneuvers", type=int, default=0, help="stop after N maneuvers (0 = all)")
+  parser.add_argument("--timeout", type=float, default=900.0)
+  args = parser.parse_args()
+
+  sim = ManeuverSim("openpilot.tools.lateral_maneuvers.lateral_maneuversd", LateralPlant(),
+                    max_maneuvers=args.max_maneuvers, timeout=args.timeout)
+  out = sim.run(args.out)
+  print(f"\nmaneuvers seen: {sim.seen_maneuvers}")
+  print(f"rlog: {out} ({out.stat().st_size / 1e6:.1f} MB)")
+
+
+if __name__ == "__main__":
+  main()