flight_probe.Pad opened /tmp/sylph-vgamepad.fifo, "the vgamepad server's FIFO". That server was removed when the uinput pad was replaced by Canary's --hid=file driver, because a uinput device is not namespaced and scripted presses leaked to the host's desktop. The FIFO is now an ordinary 91-byte file nothing reads, and /tmp/xenia_pad.txt - the file the emulator polls - was 0 bytes while the "autopilot" was flying. So every axis, trigger and button from pilot.py, autopilot3.py, aim_probe.py and flight_probe.py went nowhere, silently. The corpus already carried this trap for the SHELL scripts (canary-scripted-input-traps.md, "every call here failed silently"). This class was missed, and every flight tool imports it. Verified against the oracle rather than by inspection, on runs confirmed animating at both ends of every phase: before, full stick produced 0.00 degrees of heading change over 4 s while the ship travelled 350-735 units, and the attitude matrix at pos-0x70 was byte-identical; after, LX=-1 turns 12.72 degrees and LX=+1 swings the flight direction from [1,0,0] to [0.13,-0.14,-0.98], with the matrix moving 0.44/0.31 under stick and 0.0000 at neutral. That also REFUTES the "stale attitude matrix" suspicion from the earlier pass - pos-0x70 is live and tracks the ship; it only looked dead because nothing was turning the ship. Still open and said plainly: with the pad fixed a 150 s pilot run still fires 0 times, with |aim yaw| still exactly 90.0 and the target 36-43 km away. Steering works now, so what is left is the stick SIGN against the pilot's error convention or a target selection that commits to something too far to close. Both are finally testable. findrot_global/findself/findspeed/selfstate still write to the dead FIFO and now say so in place; they are not repaired because none has been re-run since. Co-Authored-By: Claude Opus 5 (1M context) <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_01PMRJjbxLqZtsb5Vb7KunPE
125 lines
4.7 KiB
Python
Executable File
125 lines
4.7 KiB
Python
Executable File
#!/usr/bin/env python3
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"""Is the pilot's attitude binding live, and is its yaw stick the right way round?
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`pilot.py` never fires: `fire=1` in 0 of 13 521 samples over a 900 s run. The log
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says why the gate never opens — `|aim yaw|` is **exactly 90.0°** in all 3 004
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samples that had a target, which is the `ez < 0` branch of `sticks()`, i.e. *the
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target is behind us*, always — and the range to the committed target grows
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22 km → 33 km → 49 km and stays there. The craft flies away from what it is
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chasing and the turn never completes.
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Three things could do that and they need separating by measurement, not argument:
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1. the attitude matrix the pilot reads is **stale**, so the ship turns and the
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pilot cannot see it;
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2. the matrix is live but `fwd_sign` / `fwd_row` name the wrong axis, so
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"forward" points backwards;
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3. both are fine and the **yaw stick sign** is inverted, so the controller turns
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away from the error it is trying to null.
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This probe separates them: watch the forward vector with no input at all, then
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under a hard left stick, then a hard right one.
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Usage: aim_probe.py <nav-live.json> [seconds_per_phase]
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"""
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import json
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import math
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import os
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import sys
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import time
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import numpy as np
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sys.path.insert(0, os.path.dirname(os.path.abspath(__file__)))
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import frozen # noqa: E402
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import navigator # noqa: E402
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from flight_probe import Pad # noqa: E402
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def main():
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cfg = json.load(open(sys.argv[1]))
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secs = float(sys.argv[2]) if len(sys.argv) > 2 else 4.0
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W = navigator.World(cfg)
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W.scan()
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pad = Pad()
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# There is more than one orthonormal 3x3 block near the player object -- a
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# scan finds them at pos-0x70 and pos-0x30, and `entities2.py self` has
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# picked each on different runs. Watch BOTH, because "the one the config
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# names did not move" is a much weaker statement than "neither of the two
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# candidates moved".
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deltas = [W.rot_delta]
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if "--deltas" in sys.argv:
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deltas = [int(x, 0) for x in sys.argv[sys.argv.index("--deltas") + 1].split(",")]
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def read_block(off, delta):
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b = os.pread(W.fd, W.rot_stride * 3 + 12, off + delta)
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rows = []
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for r in range(3):
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row = np.frombuffer(b[W.rot_stride * r:W.rot_stride * r + 12],
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dtype=">f4").astype(np.float64)
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rows.append(row)
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return np.array(rows)
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def fwd_now():
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ents = W.sample(time.time())
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me = next((e for e in ents if "Player" in e[1]), None)
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if me is None:
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return None, None, None
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mats = {}
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for d in deltas:
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try:
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M = read_block(me[0], d)
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except Exception:
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continue
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if np.all(np.isfinite(M)):
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mats[d] = M
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M = W.rot(me[0])
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if M is None:
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return None, None, mats
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return M[W.fwd_row] * W.fwd_sign, me[2], mats
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def phase(name, lx):
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# BRACKET the phase with a liveness check at BOTH ends. The first run of
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# this probe reported the forward vector pinned and 0.00 deg/s under
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# every stick, which reads as "the attitude matrix is dead" -- and the
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# guest had simply FROZEN partway through. A dead world holds every
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# matrix still, so a phase that ends frozen proves nothing and must be
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# thrown away rather than reported.
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pad.axis("LX", lx)
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f0, p0, m0 = fwd_now()
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t0 = time.time()
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time.sleep(secs)
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f1, p1, m1 = fwd_now()
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pad.axis("LX", 0.0)
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froze = frozen.frozen(3.0)[0]
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if f0 is None or f1 is None:
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print(f"{name:>12}: NO PLAYER/ORIENTATION")
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return
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dot = float(np.clip(np.dot(f0, f1), -1, 1))
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turn = math.degrees(math.acos(dot)) / max(time.time() - t0, 1e-3)
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cross = np.cross(f0, f1)
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moved = float(np.linalg.norm(p1 - p0)) if p0 is not None else float("nan")
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blocks = " ".join(
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f"pos{d:+#06x} d{float(np.abs(m1[d]-m0[d]).max()):.4f}"
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for d in deltas if d in m0 and d in m1)
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print(f"{name:>12}: |turn| {turn:6.2f} deg/s fwd {f0.round(3)} -> "
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f"{f1.round(3)} moved {moved:8.1f} [{blocks}]"
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f"{' *** GUEST FROZE - DISCARD ***' if froze else ''}")
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if frozen.frozen(3.0)[0]:
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print("# GUEST IS ALREADY FROZEN — nothing to measure")
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return 3
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print("# phases: neutral, then full LEFT stick, then full RIGHT stick")
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print("# (each phase is followed by a liveness check; a frozen tail voids it)")
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phase("neutral", 0.0)
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phase("LX=-1", -1.0)
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phase("neutral", 0.0)
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phase("LX=+1", +1.0)
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pad.reset()
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return 0
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if __name__ == "__main__":
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raise SystemExit(main())
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