wyj
f7380cbf75
Replace the position capture cutoff with a camera-relative dark threshold shared by every backend, and carry explicit outcome/reason provenance through the ray, RayPool, adaptive mesh, lens-map and replay paths. - eval/eval_slab return SpacetimePointStatus; remove SPACETIME_RAY_CAPTURED and the Schwarzschild capture radius; decouple observer construction from ray position. - RayEndpoint stores RayOutcome/RayReason plus the last trusted state; budget exhaustion is retryable UNRESOLVED, data/integration failures are INCOMPLETE. - Normal dark terminal is L - L0 >= --dark-threshold (default 8), with L0 taken at the camera event and kept distinct from the worldtube entry energy; photon energy and frequency ratio are never reset. - Implement E/D/U triangle decisions with merged budget retries, persistent probe witnesses promoted in place by vertex identity, conformity settling, and approximate-black boundary provenance with achieved-scale statistics. - Add RayPool continuation state and per-ray step budgets. - Bump lens-map to v2 with explicit end/outcome/reason, approx_black, threshold/retry/geometry provenance and per-frame retry counts; reject v1. - Gate production output on incomplete/error results, overridable with --allow-incomplete. - Update AGENTS.md, the design document and usage docs; add the termination oracle and regression coverage. make -B -j4 BUILD_TYPE=Debug test passes with bit-identical reference HDRs.
78 lines
3.2 KiB
C
78 lines
3.2 KiB
C
#include "geodesic.h"
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#include "observer_track.h"
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#include <math.h>
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#include <stdio.h>
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static int nearly_equal(double a, double b) { return fabs(a - b) < 1e-12; }
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static int check_ray(const SpacetimeSource *source,
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const ObserverState *observer,
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const double local_direction[3],
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const double expected[3]) {
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const GeodesicTraceConfig config = {.coordinate_time_step = 0.25,
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.max_steps = 100};
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RayEndpoint ray =
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geodesic_trace_past(source, observer, local_direction, &config);
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if (ray.outcome != RAY_OUTCOME_ESCAPED ||
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!nearly_equal(ray.frequency_ratio, 1.0) ||
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!nearly_equal(ray.n_infinity[0], expected[0]) ||
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!nearly_equal(ray.n_infinity[1], expected[1]) ||
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!nearly_equal(ray.n_infinity[2], expected[2])) {
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fprintf(stderr, "flat-space geodesic regression failed\n");
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return 1;
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}
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return 0;
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}
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int main(void) {
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SpacetimeSource source = {0};
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MetricSlab *slab = NULL;
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MetricData metric;
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const ObserverState observer = observer_fixed_at_origin();
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if (spacetime_create_minkowski(&source, 10.0) ||
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spacetime_load_slab(&source, 0.0, -1.0, &slab) ||
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spacetime_slab_eval(slab, -0.5, (double[]){0.0, 0.0, 0.0}, &metric) ||
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metric.alpha != 1.0 ||
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!spacetime_slab_eval(slab, 0.25, (double[]){0.0, 0.0, 0.0}, &metric))
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return 1;
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int result = check_ray(&source, &observer, (double[]){1.0, 0.0, 0.0},
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(double[]){0.0, 0.0, -1.0}) ||
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check_ray(&source, &observer, (double[]){0.0, 0.0, 1.0},
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(double[]){1.0, 0.0, 0.0});
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const ObserverState look_at_ra_zero =
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observer_fixed_at_origin_look_at(0.0, 0.0);
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result = result || check_ray(&source, &look_at_ra_zero,
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(double[]){1.0, 0.0, 0.0},
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(double[]){1.0, 0.0, 0.0});
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/* Standard ICRS has +Z at the north celestial pole and +Y at increasing
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* RA. A right-handed north-up camera consequently has west to its right. */
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result = result || check_ray(&source, &look_at_ra_zero,
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(double[]){0.0, 1.0, 0.0},
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(double[]){0.0, 0.0, 1.0}) ||
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check_ray(&source, &look_at_ra_zero,
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(double[]){0.0, 0.0, 1.0},
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(double[]){0.0, -1.0, 0.0});
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ObserverTrack accelerated = {0};
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ObserverState final_observer;
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if (observer_track_generate_minkowski_acceleration(&accelerated, 1.52, 2.0,
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1.0 / 30.0) ||
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observer_track_interpolate(&accelerated, 2.0, &final_observer, NULL)) {
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result = 1;
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} else {
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const RayEndpoint forward = geodesic_trace_past(
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&source, &final_observer, (double[]){1.0, 0.0, 0.0},
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&(GeodesicTraceConfig){.coordinate_time_step = 0.25, .max_steps = 100});
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const double expected_g = sqrt(1.0 + 3.04 * 3.04) + 3.04;
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if (forward.outcome != RAY_OUTCOME_ESCAPED ||
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!nearly_equal(forward.frequency_ratio, expected_g)) {
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fputs("accelerated-observer Doppler regression failed\n", stderr);
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result = 1;
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}
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}
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observer_track_destroy(&accelerated);
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spacetime_free_slab(slab);
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spacetime_destroy(&source);
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return result;
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}
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