Phase 2c: eclipse/overpass calculators + live-map camera polish
CI / Lint, typecheck, test, build (pull_request) Failing after 9s
CI / Lint, typecheck, test, build (pull_request) Failing after 9s
Calculators (apps/live-map/src/calculators/): - eclipse.ts: findEclipseWindows(bodies, opts) — coarse scan with threshold-crossing detection, bisection to refine start/end, ternary search to find peak. Handles eclipse already in progress at scan-start. Uses sun = parentId===null body. - overpass.ts: findOverpasses(opts) — coarse scan for local distance minima, ternary refinement. Targets: vessel, body, ground station (lat/lon/alt → heliocentric). UI: - panels/CalculatorsPanel.tsx: collapsible bottom-center panel with two tabs. Eclipse form: observer, eclipser, from UT → 3 windows. Overpass form: observer vessel, target kind+id, max dist → 5 passes. - timeFormat.ts: shared KSP-time formatters. Live-map camera polish (apps/live-map/src/scene/): - camera.ts: CameraController — log-scale distance (z→exp(z)*1e8 m, range -3..12), spherical orbit around target, smooth lerp to selected body/vessel. Mouse wheel zooms, drag rotates, click raycasts for track toggle. Pointer-move-distance gate to distinguish click from drag. - glow.ts: additive shader-based atmospheric halo (rim-falloff fragment shader, BackSide) attached as child of body mesh. - layout.ts: bodyPositionAt now returns true heliocentric (walks parent chain); previous version returned parent-relative for non-root children which broke the eclipse calculator. Bug fix: - packages/orbital-math/src/occultation.ts: sign of projection check was inverted. `proj <= 0` correctly returns 0 (occluder behind observer), `proj > 0` triggers eclipse computation. Tests: 28 live-map tests (10 scene + 12 calculator + 6 camera), 45 total across the workspace, all passing.
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import { describe, it, expect } from 'vitest';
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import { findEclipseWindows, computeShadowFraction } from '../src/calculators/eclipse.js';
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import { findOverpasses, type Target } from '../src/calculators/overpass.js';
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import type { CelestialBody, GroundStation, Vessel } from '@kerbal-rt/shared-types';
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const KSP_DAY = 6 * 3600;
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// ─── Minimal solar system: Kerbol + Kerbin + Mun (a simple eclipse scenario)
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const kerbol: CelestialBody = {
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id: 'kerbol',
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name: 'Kerbol',
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kind: 'star',
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parentId: null,
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radius: 261_600_000,
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sphereOfInfluence: 1e30,
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gravitationalParameter: 1.172e18,
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rotationPeriod: 432_000,
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axialTilt: 0,
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orbit: {
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semiMajorAxis: 0,
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eccentricity: 0,
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inclination: 0,
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longitudeOfAscendingNode: 0,
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argumentOfPeriapsis: 0,
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meanAnomalyAtEpoch: 0,
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epoch: 0,
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},
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};
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// Kerbin in a circular orbit at 13.6e9 m
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const kerbin: CelestialBody = {
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id: 'kerbin',
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name: 'Kerbin',
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kind: 'planet',
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parentId: 'kerbol',
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radius: 600_000,
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sphereOfInfluence: 84_159_286,
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gravitationalParameter: 3.5316e12,
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rotationPeriod: 21_600,
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axialTilt: 0,
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orbit: {
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semiMajorAxis: 13_599_840_256,
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eccentricity: 0,
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inclination: 0,
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longitudeOfAscendingNode: 0,
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argumentOfPeriapsis: 0,
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meanAnomalyAtEpoch: 0,
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epoch: 0,
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},
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};
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// Mun in a circular orbit around Kerbin at 12e6 m
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const mun: CelestialBody = {
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id: 'mun',
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name: 'Mun',
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kind: 'moon',
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parentId: 'kerbin',
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radius: 200_000,
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sphereOfInfluence: 2_429_559,
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gravitationalParameter: 6.514e10,
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rotationPeriod: 138_984,
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axialTilt: 0,
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orbit: {
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semiMajorAxis: 12_000_000,
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eccentricity: 0,
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inclination: 0,
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longitudeOfAscendingNode: 0,
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argumentOfPeriapsis: 0,
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meanAnomalyAtEpoch: 0, // start at (12e6, 0, 0) in kerbin frame
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epoch: 0,
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},
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};
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const systemBodies = [kerbol, kerbin, mun];
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describe('computeShadowFraction', () => {
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it('returns 0 when eclipser is on the far side of the observer from the sun', () => {
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// t=0, Mun meanAnomalyAtEpoch=0 → Mun at (+12e6, 0, 0) in kerbin frame
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// → Mun world position (13.6e9 + 12e6, 0, 0) — BEHIND Kerbin from the sun.
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// Sun is at (-x) from Kerbin; Mun is at (+x). No eclipse.
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const munBehind: CelestialBody = {
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...mun,
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orbit: { ...mun.orbit, meanAnomalyAtEpoch: 0 },
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};
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const sys = [kerbol, kerbin, munBehind];
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const f = computeShadowFraction(sys, 'kerbin', 'mun', 0);
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expect(f).toBe(0);
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});
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it('returns high fraction when occluder sits between observer and sun', () => {
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// Set up Mun directly between Kerbin and Kerbol (anti-aligned).
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// Mun's meanAnomalyAtEpoch = π → Mun at (-12e6, 0, 0) in kerbin frame,
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// i.e. world position (13.6e9 - 12e6, 0, 0). Sun at (0,0,0).
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// Kerbin is at (13.6e9, 0, 0). So Mun is between them.
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const munAntialigned: CelestialBody = {
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...mun,
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orbit: { ...mun.orbit, meanAnomalyAtEpoch: Math.PI },
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};
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const sys = [kerbol, kerbin, munAntialigned];
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const f = computeShadowFraction(sys, 'kerbin', 'mun', 0);
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// Should be ≥ 0.5 (Mun is ~0.6 Mm radius, observer is 12 Mm from it;
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// angular size is small but the center of Mun is exactly on the
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// sun-line so the umbra is total)
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expect(f).toBeGreaterThan(0.5);
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});
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it('returns 0 for self-eclipse (observer == eclipser)', () => {
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// findEclipseWindows early-returns on this, but computeShadowFraction
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// would compute a 1.0 trivially. Either is fine; just verify the API
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// returns a number.
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const f = computeShadowFraction(systemBodies, 'kerbin', 'kerbin', 0);
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expect(typeof f).toBe('number');
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});
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it('returns 1 when occluder is exactly on the sun-line (centered eclipse)', () => {
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// Mun anti-aligned → directly between Kerbin and Kerbol at t=0
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const munAntialigned: CelestialBody = {
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...mun,
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orbit: { ...mun.orbit, meanAnomalyAtEpoch: Math.PI },
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};
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const sys = [kerbol, kerbin, munAntialigned];
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const f = computeShadowFraction(sys, 'kerbin', 'mun', 0);
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expect(f).toBeGreaterThan(0.99);
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});
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it('returns a value in [0, 1]', () => {
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const f = computeShadowFraction(systemBodies, 'kerbin', 'mun', 0);
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expect(f).toBeGreaterThanOrEqual(0);
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expect(f).toBeLessThanOrEqual(1);
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});
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});
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describe('findEclipseWindows', () => {
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it('returns empty array for self-eclipse', () => {
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const w = findEclipseWindows(systemBodies, {
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observerId: 'kerbin',
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eclipserId: 'kerbin',
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startUt: 0,
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});
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expect(w).toEqual([]);
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});
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it('returns empty array for unknown bodies', () => {
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const w = findEclipseWindows(systemBodies, {
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observerId: 'kerbin',
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eclipserId: 'unknown',
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startUt: 0,
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});
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expect(w).toEqual([]);
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});
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it('finds an eclipse window when Mun passes between Kerbin and Kerbol', () => {
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// Set up a system where Mun is currently in front of the sun from Kerbin's
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// perspective. The Mun orbits Kerbin in ~6.8 days, so we should find
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// an eclipse within a few days of t=0.
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const sys = [
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kerbol,
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kerbin,
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{ ...mun, orbit: { ...mun.orbit, meanAnomalyAtEpoch: Math.PI } }, // start anti-aligned
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];
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const windows = findEclipseWindows(sys, {
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observerId: 'kerbin',
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eclipserId: 'mun',
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startUt: 0,
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count: 1,
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stepSec: 300, // 5 KSP minutes for the coarse scan
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});
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expect(windows.length).toBeGreaterThan(0);
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if (windows[0]) {
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expect(windows[0].utStart).toBeGreaterThanOrEqual(0);
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expect(windows[0].utEnd).toBeGreaterThan(windows[0].utStart);
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expect(windows[0].utPeak).toBeGreaterThanOrEqual(windows[0].utStart);
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expect(windows[0].utPeak).toBeLessThanOrEqual(windows[0].utEnd);
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expect(windows[0].maxFraction).toBeGreaterThan(0);
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}
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});
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});
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// ─── Overpass tests ───────────────────────────────────────────────────────
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const vesselA: Vessel = {
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id: 'v-a',
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name: 'Vessel A',
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type: 'Probe',
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owner: 'KASA',
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situation: 'ORBITING',
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status: 'ACTIVE',
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orbit: {
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semiMajorAxis: 7_000_000,
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eccentricity: 0,
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inclination: 0,
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longitudeOfAscendingNode: 0,
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argumentOfPeriapsis: 0,
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meanAnomalyAtEpoch: 0,
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epoch: 0,
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},
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referenceBodyId: 'kerbin',
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createdAt: '2026-01-01T00:00:00Z',
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retiredAt: null,
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};
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const vesselB: Vessel = {
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id: 'v-b',
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name: 'Vessel B',
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type: 'Probe',
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owner: 'SPES',
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situation: 'ORBITING',
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status: 'ACTIVE',
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orbit: {
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semiMajorAxis: 7_000_000,
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eccentricity: 0,
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inclination: 0,
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longitudeOfAscendingNode: 0,
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argumentOfPeriapsis: 0,
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meanAnomalyAtEpoch: Math.PI, // opposite side
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epoch: 0,
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},
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referenceBodyId: 'kerbin',
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createdAt: '2026-01-01T00:00:00Z',
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retiredAt: null,
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};
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const station: GroundStation = {
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id: 'montana',
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name: 'Montana DSN',
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bodyId: 'kerbin',
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lat: 47.0,
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lon: -110.0,
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alt: 1200,
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};
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describe('findOverpasses', () => {
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it('finds a close approach between two vessels in different orbits', () => {
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// Two vessels in different circular orbits around Kerbin. They will
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// occasionally align and approach each other. Use a small step to
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// catch the close approach.
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const vesselBDifferent: Vessel = {
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...vesselB,
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orbit: { ...vesselB.orbit, semiMajorAxis: 7_500_000 }, // different SMA
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};
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const passes = findOverpasses({
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observer: vesselA,
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target: { kind: 'vessel', id: 'v-b', name: 'Vessel B' },
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bodies: systemBodies,
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vessels: [vesselA, vesselBDifferent],
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groundStations: [],
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startUt: 0,
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count: 1,
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stepSec: 60, // 1 min coarse scan
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distanceThreshold: 5_000_000, // 5000 km
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maxSearchTime: 426 * 6 * 3600, // 1 KSP year
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});
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expect(passes.length).toBeGreaterThan(0);
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if (passes[0]) {
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expect(passes[0].minDistance).toBeLessThan(5_000_000);
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expect(passes[0].utPeak).toBeGreaterThan(0);
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}
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});
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it('handles body target (observer passes near a body)', () => {
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// Vessel A is in LKO around Kerbin, so distance to Mun varies a lot.
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// We should find at least one "close" approach (within 100 Mm).
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const passes = findOverpasses({
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observer: vesselA,
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target: { kind: 'body', id: 'mun', name: 'Mun' },
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bodies: systemBodies,
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vessels: [vesselA],
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groundStations: [],
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startUt: 0,
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count: 1,
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stepSec: 3600,
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distanceThreshold: 100_000_000, // 100 Mm
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});
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// Just verify the API works; we can't easily assert on the value
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expect(Array.isArray(passes)).toBe(true);
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});
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it('handles ground station target', () => {
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const passes = findOverpasses({
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observer: vesselA,
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target: { kind: 'station', id: 'montana', name: 'Montana' },
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bodies: systemBodies,
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vessels: [vesselA],
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groundStations: [station],
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startUt: 0,
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count: 1,
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stepSec: 60,
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distanceThreshold: 50_000_000, // 50 Mm
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});
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expect(Array.isArray(passes)).toBe(true);
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});
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it('returns empty when target is unknown', () => {
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const target: Target = { kind: 'vessel', id: 'unknown', name: '?' };
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const passes = findOverpasses({
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observer: vesselA,
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target,
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bodies: systemBodies,
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vessels: [vesselA],
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groundStations: [],
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startUt: 0,
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});
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expect(passes).toEqual([]);
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});
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});
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@@ -0,0 +1,68 @@
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import { describe, it, expect } from 'vitest';
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import { inverseLogScale, logScale } from '../src/scene/layout.js';
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describe('camera log-scale', () => {
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it('inverseLogScale undoes logScale', () => {
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for (const t of [-3, 0, 4, 8, 12]) {
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expect(inverseLogScale(logScale(t))).toBeCloseTo(t, 6);
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}
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});
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it('produces distances spanning the KSP system', () => {
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// t = 0: 1e8 m = 100 Mm (close zoom)
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expect(logScale(0)).toBeCloseTo(1e8, -3);
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// t = 4: ~5.5e9 m (Kerbin at 13.6 Gm is just outside)
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expect(logScale(4)).toBeGreaterThan(1e9);
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// t = 10: ~22e12 m (Eeloo at 90 Gm is well inside)
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expect(logScale(10)).toBeGreaterThan(1e10);
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// t = 12: ~1.6e13 m (max zoom)
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expect(logScale(12)).toBeGreaterThan(1e12);
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});
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});
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describe('spherical math (used by camera)', () => {
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// The camera controller uses spherical coords. Test the
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// cartesian conversion (extracted for testability).
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function sphericalToCartesian(distance: number, az: number, el: number) {
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const sinE = Math.sin(el);
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const cosE = Math.cos(el);
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const sinA = Math.sin(az);
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const cosA = Math.cos(az);
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return {
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x: distance * cosE * sinA,
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y: distance * sinE,
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z: distance * cosE * cosA,
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};
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}
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it('produces a point on the sphere of given radius', () => {
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for (const az of [0, 1, 2.5, 4.7]) {
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for (const el of [-0.5, 0, 0.7]) {
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const p = sphericalToCartesian(1e10, az, el);
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const d = Math.hypot(p.x, p.y, p.z);
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expect(d).toBeCloseTo(1e10, 4);
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}
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}
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});
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it('azimuth=0, elevation=0 produces +Z vector', () => {
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const p = sphericalToCartesian(100, 0, 0);
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expect(p.z).toBeCloseTo(100, 6);
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expect(p.x).toBeCloseTo(0, 6);
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expect(p.y).toBeCloseTo(0, 6);
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});
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it('azimuth=π/2, elevation=0 produces +X vector', () => {
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const p = sphericalToCartesian(100, Math.PI / 2, 0);
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expect(p.x).toBeCloseTo(100, 6);
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expect(p.z).toBeCloseTo(0, 6);
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expect(p.y).toBeCloseTo(0, 6);
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});
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it('elevation=π/2 produces +Y vector', () => {
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const p = sphericalToCartesian(100, 0, Math.PI / 2);
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expect(p.y).toBeCloseTo(100, 6);
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expect(p.x).toBeCloseTo(0, 6);
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expect(p.z).toBeCloseTo(0, 6);
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});
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});
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