Right pane tabs Jobs/Planes market + 5 new plane types with tech-spec panels + sell-plane cargo guard (ISS-047 part A)
CI / build + unit + e2e (pull_request) Successful in 8m56s

This commit is contained in:
2026-09-20 13:57:52 +00:00
parent 4f182a22b6
commit 7524f943d2
13 changed files with 287 additions and 2 deletions
+22
View File
@@ -5,6 +5,7 @@ import {
burnRateConstant,
FUEL_DENSITY_KG_PER_L,
fuelAtWeighted,
maxRangeKm,
positionAt,
progressAt,
requiredFuelFor,
@@ -164,3 +165,24 @@ describe('weighted burn model (v0.16.0)', () => {
expect(fuelAtWeighted(TANK, BURN, WE, TANK, KM, progressAt(DEP, KM, SPEED, clock))).toBeGreaterThan(0);
});
});
describe('maxRangeKm (v0.28.0)', () => {
it('ATR 72-600 full tank ≈ 4439 km (±5%)', () => {
const r = maxRangeKm(BURN, WE, TANK);
expect(r).toBeGreaterThan(4439 * 0.95);
expect(r).toBeLessThan(4439 * 1.05);
});
it('increases with tank size and decreases with burn rate', () => {
expect(maxRangeKm(BURN, WE, TANK * 2)).toBeGreaterThan(maxRangeKm(BURN, WE, TANK));
expect(maxRangeKm(3, WE, TANK)).toBeLessThan(maxRangeKm(BURN, WE, TANK));
});
it('zero fuel → zero range', () => {
expect(maxRangeKm(BURN, WE, 0)).toBe(0);
});
it('rejects a non-positive empty weight', () => {
expect(() => maxRangeKm(BURN, 0, TANK)).toThrow();
});
});
+10
View File
@@ -118,3 +118,13 @@ export function requiredFuelFor(
const rho = FUEL_DENSITY_KG_PER_L;
return (emptyWeightKg / rho) * (Math.exp(k * rho * distanceKm) - 1);
}
// Max range from a FULL tank under the weighted model — solve requiredFuelFor(d) = maxFuel for d:
// (We/ρ)(e^{kρd} − 1) = F → d = ln(1 + ρF/We) · (We + ρF)/(ρ·burnPerKm).
// Returns raw km (call sites round); zero fuel gives exactly 0. Pure — display-only, the sim
// itself does not model range exhaustion (see fuelAtWeighted).
export function maxRangeKm(burnPerKm: number, emptyWeightKg: number, maxFuel: number): number {
if (!(emptyWeightKg > 0)) throw new Error('emptyWeightKg must be > 0');
const rho = FUEL_DENSITY_KG_PER_L;
return Math.log(1 + (rho * maxFuel) / emptyWeightKg) * ((emptyWeightKg + rho * maxFuel) / (rho * burnPerKm));
}