local bench = script and require(script.Parent.bench_support) or require("bench_support") local PI = 3.141592653589793 local SOLAR_MASS = 4 * PI * PI local DAYS_PER_YEAR = 365.24 local Body = {} Body.__index = Body function Body.new(x, y, z, vx, vy, vz, mass) local self = {} self.x = x self.y = y self.z = z self.vx = vx self.vy = vy self.vz = vz self.mass = mass return setmetatable(self, Body) end function Body:offsetMomentum(px, py, pz) self.vx = -px / SOLAR_MASS self.vy = -py / SOLAR_MASS self.vz = -pz / SOLAR_MASS return self end local function Jupiter() return Body.new( 4.841431442464721e0, -1.1603200440274284e0, -1.036220444711231e-1, 1.660076642744037e-3 * DAYS_PER_YEAR, 7.6990111841974045e-3 * DAYS_PER_YEAR, -6.90460016972063e-5 * DAYS_PER_YEAR, 9.547919384243267e-4 * SOLAR_MASS ) end local function Saturn() return Body.new(8.34336671824458e0, 4.124798564124305e0, -4.035234171143213e-1, -2.767425107268624e-3 * DAYS_PER_YEAR, 4.998528012349173e-3 * DAYS_PER_YEAR, 2.3041729757376395e-5 * DAYS_PER_YEAR, 2.8588598066613082e-4 * SOLAR_MASS) end local function Uranus() return Body.new(1.2894369562139132e1, -1.511115140169863e1, -2.2330757889265573e-1, 2.964601375647616e-3 * DAYS_PER_YEAR, 2.3784717395948096e-3 * DAYS_PER_YEAR, -2.9658956854023755e-5 * DAYS_PER_YEAR, 4.366244043351563e-5 * SOLAR_MASS) end local function Neptune() return Body.new(1.5379697114850917e1, -2.5919314609987962e1, 1.7925877295037118e-1, 2.680677724903893e-3 * DAYS_PER_YEAR, 1.628241700382423e-3 * DAYS_PER_YEAR, -9.515922545197158e-5 * DAYS_PER_YEAR, 5.151389020466114e-5 * SOLAR_MASS) end local function Sun() return Body.new(0, 0, 0, 0, 0, 0, SOLAR_MASS) end local NBodySystem = {} NBodySystem.__index = NBodySystem function NBodySystem.new(bodies) local self = {} self.bodies = bodies local px = 0 local py = 0 local pz = 0 local size = #self.bodies for i=1, size do local b = self.bodies[i] local m = b.mass px = px + b.vx * m py = py + b.vy * m pz = pz + b.vz * m end self.bodies[1]:offsetMomentum(px, py, pz) return setmetatable(self, NBodySystem) end function NBodySystem:advance(dt) local dx, dy, dz, distance, mag local size = #self.bodies for i=1, size do local bodyi = self.bodies[i] for j=i+1, size do local bodyj = self.bodies[j] dx = bodyi.x - bodyj.x dy = bodyi.y - bodyj.y dz = bodyi.z - bodyj.z distance = math.sqrt(dx*dx + dy*dy + dz*dz) mag = dt / (distance * distance * distance) bodyi.vx -= dx * bodyj.mass * mag bodyi.vy -= dy * bodyj.mass * mag bodyi.vz -= dz * bodyj.mass * mag bodyj.vx += dx * bodyi.mass * mag bodyj.vy += dy * bodyi.mass * mag bodyj.vz += dz * bodyi.mass * mag end end for i=1, size do local body = self.bodies[i] body.x = body.x + dt * body.vx body.y = body.y + dt * body.vy body.z = body.z + dt * body.vz end end function NBodySystem:energy() local dx, dy, dz, distance local e = 0.0 local size = #self.bodies for i=1, size do local bodyi = self.bodies[i] e = e + 0.5 * bodyi.mass * (bodyi.vx * bodyi.vx + bodyi.vy * bodyi.vy + bodyi.vz * bodyi.vz) for j=i+1, size do local bodyj = self.bodies[j] dx = bodyi.x - bodyj.x dy = bodyi.y - bodyj.y dz = bodyi.z - bodyj.z distance = math.sqrt(dx*dx + dy*dy + dz*dz) e -= (bodyi.mass * bodyj.mass) / distance end end return e end local function run() local ret = 0 local n = 3 while n <= 24 do (function() local bodies = NBodySystem.new({ Sun(),Jupiter(),Saturn(),Uranus(),Neptune() }) local max = n * 100 ret += bodies:energy() for i=1, max do bodies:advance(0.01) end ret += bodies:energy() end)() n *= 2 end local expected = -1.3524862408537381 if ret ~= expected then error('ERROR: bad result: expected ' .. expected .. ' but got ' .. ret) end end function runIteration() for i=1, 5 do run() end end bench.runCode(runIteration, "n-body-oop")