Run and export to CSV
This commit is contained in:
parent
cbc770f340
commit
104ec50dcd
3 changed files with 44 additions and 14 deletions
23
app/Main.hs
23
app/Main.hs
|
@ -2,5 +2,26 @@ module Main where
|
|||
|
||||
import Lib
|
||||
|
||||
import Linear.Affine
|
||||
import Linear.V3
|
||||
|
||||
csvFromPoint :: Point V3 Double -> String
|
||||
csvFromPoint (P (V3 x y z)) =
|
||||
show x ++ "," ++ show y ++ "," ++ show z
|
||||
|
||||
csvFromBodies :: [Body] -> [String]
|
||||
csvFromBodies [] = []
|
||||
csvFromBodies (x:xs) =
|
||||
(bodyName x ++ ","
|
||||
++ (show $ bodyMass x) ++ ","
|
||||
++ (csvFromPoint $ bodyPosition x) ++ "\n")
|
||||
:(csvFromBodies xs)
|
||||
|
||||
steps :: Int -> Double -> [Body] -> IO ()
|
||||
steps 0 _ _ = return ()
|
||||
steps n dt bodies = do
|
||||
putStr . concat $ map ((++) (show n ++ ",")) $ csvFromBodies bodies
|
||||
steps (n-1) dt (updateAll dt bodies)
|
||||
|
||||
main :: IO ()
|
||||
main = putStrLn "Hello"
|
||||
main = steps 1000000 10 [sun, earth, moon]
|
||||
|
|
|
@ -26,6 +26,7 @@ executable orbit-exe
|
|||
ghc-options: -threaded -rtsopts -with-rtsopts=-N
|
||||
build-depends: base
|
||||
, orbit
|
||||
, linear
|
||||
default-language: Haskell2010
|
||||
|
||||
test-suite orbit-test
|
||||
|
|
34
src/Lib.hs
34
src/Lib.hs
|
@ -1,11 +1,17 @@
|
|||
module Lib (
|
||||
gravity,
|
||||
Body,
|
||||
bodyName,
|
||||
bodyMass,
|
||||
bodyPosition,
|
||||
bodySpeed,
|
||||
bodyDistance,
|
||||
field,
|
||||
acceleration,
|
||||
update,
|
||||
b1, b2, b3
|
||||
updateAll,
|
||||
b1, b2, b3,
|
||||
au, sun, earth, moon
|
||||
) where
|
||||
|
||||
import Linear.Vector
|
||||
|
@ -27,9 +33,10 @@ gravity = 6.67408e-11
|
|||
|
||||
-- Body
|
||||
data Body = Body {
|
||||
bodyMass :: Double,
|
||||
bodyPosition :: Point V3 Double,
|
||||
bodySpeed :: V3 Double
|
||||
bodyName :: String,
|
||||
bodyMass :: Double, -- [kg]
|
||||
bodyPosition :: Point V3 Double, -- [m]
|
||||
bodySpeed :: V3 Double -- [m/s]
|
||||
} deriving (Show, Eq)
|
||||
|
||||
|
||||
|
@ -64,9 +71,9 @@ acceleration body = foldr f (fromInteger 0)
|
|||
|
||||
-- Update speed and position with using a timestep dt
|
||||
update :: Double -> Body -> [Body] -> Body
|
||||
update dt (Body m pos speed) neighbours =
|
||||
Body m newpos newspeed
|
||||
where accel = acceleration (Body m pos speed) neighbours
|
||||
update dt (Body name m pos speed) neighbours =
|
||||
Body name m newpos newspeed
|
||||
where accel = acceleration (Body name m pos speed) neighbours
|
||||
newspeed = speed + dt *^ accel
|
||||
newpos = pos + dt *^ P newspeed
|
||||
|
||||
|
@ -85,13 +92,14 @@ updateAll dt bodies = aux [] [] bodies
|
|||
-- EXAMPLES
|
||||
--------------------------------------------------------------------------------
|
||||
|
||||
b1 = Body 42 (P $ V3 0 0 0) (V3 0 0 0)
|
||||
b2 = Body 11 (P $ V3 1 2 3) (V3 0 0 0)
|
||||
b3 = Body 5 (P $ V3 5 2 1) (V3 0 0 0)
|
||||
b1 = Body "b1" 42e12 (P $ V3 0 0 0) (V3 0 0 0)
|
||||
b2 = Body "b2" 11e12 (P $ V3 1 2 3) (V3 0 3e3 0)
|
||||
b3 = Body "b3" 5e12 (P $ V3 5 2 1) (V3 3e3 1e3 0)
|
||||
|
||||
-- Astronomical Unit
|
||||
-- Astronomical Unit [m]
|
||||
au :: Double
|
||||
au = 149597870700
|
||||
|
||||
sun = Body 1.98855e30 (P $ V3 0 0 0) (V3 0 0 0)
|
||||
earth = Body 8.97237e24 (P $ V3 au 0 0) (V3 0 29.78e3 0)
|
||||
sun = Body "Sun" 1.98855e30 (P $ V3 0 0 0) (V3 0 0 0)
|
||||
earth = Body "Earth" 8.97237e24 (P $ V3 au 0 0) (V3 0 29.78e3 0)
|
||||
moon = Body "Moon" 7.342e22 (P $ V3 (au+384399e3) 0 0) (V3 0 (29.78e3+1022) 0)
|
||||
|
|
Loading…
Add table
Add a link
Reference in a new issue