およそ５等星以上の恒星データや星座線，惑星の軌道要素などを使ってある年月日，時刻の星空を再現するプログラムをPythonで作ってみました。はじめは中野主一さんの「マイコンで解く天体の謎」（1982年）を参考にして作ったのですが，惑星や月の位置計算が500年もするとずれてくることに気づき，斉藤国治さんの「古天文学」（1989年）の計算方法を移植しています。これで紀元前の日食なども再現できるようにしました。ソースコードが1000行以上にもなってしまいました。パッケージに分けていますが，現在未完成です。ソースコードにご興味がある方は，参考にしてみてください。（2020年3月にバージョン2.0に）。恒星データは https://heasarc.gsfc.nasa.gov/W3Browse/star-catalog/hipparcos.html ，星座線や星座名のデータはAstro Commons (アストロ・コモンズ)。 http://astronomy.webcrow.jp/help/ から得ました。
下記のデータファイル「seizaData」をダウンロードして，同一ディレクトリに置いて 実行すると，ステレオ投影図法の天球に恒星と星座線，星座名および月惑星（太陽も）が表示されます。右上のinputボックスに見たい年月日や時刻を例にならって入力し（例；YYYYMMDD＝20201028→2020年10月28日）Enterキーを押してください。 デフォルトで表示されるのは，紀元628年4月10日の日本書紀に初めて記録された日食です。 緯度経度は奈良盆地です。
- 星座早見データ →こちらから seizaData
2020年3月現在，実行形式のファイル（約10MB) を作りました。Python3がインストールされていなくても，お試しいただけます。こちらからダウンロードしてください。 → 星座早見プログラムダウンロード
'''
******************************************************
星座早見プログラム（古天文学バージョン）
2019.08.18 Ver1.0から古天文学バージョンへ1.2
2020.03.13 実行ファイルも作製 Ver.2.0以降
******************************************************
'''
# 2019.08.18試作版完成 古天文学バージョンへupgrade 8/28 Ver.1.0
# 8/30 def Batch()を挿入 8/31 タプル代入に変更
# 9/11 月食計算を追加（地球の影） 9/11 元期のユリウス日が1日ずれていたことに気づき修正
# 2020.2 GUI部分をクラス化 numpyを使わないで計算するように変更。月齢を画面表示に
# 惑星位置計算などバグを修正（by pycharm)
# 2020/03/27 バージョン2.4 星座線終点をはみださないようにし，月の月齢写真を表示に
import os
import tkinter as tk
import csv
import math
# ユリウス日をグレゴリオ暦に直す計算
def JDT(jd):
Z = int(jd + 0.5)
if Z >= 2299161:
a = int((Z - 1867216.25) / 36524.25)
A = Z + 1 + a - int(a / 4)
else:
A = Z
B = A + 1524
C = int((B - 122.1) / 365.25)
K = int(365.25 * C)
E = int((B - K)/30.6001)
D = B - K - int(30.6001 * E) + (jd + 0.5) - int(jd + 0.5)
if E < 13.5:
M = E -1
else:
M = E -13
if M > 2.5:
Y = C - 4716
else:
Y = C - 4715
if M >= 13:
Y = Y + 1
M = M -12
if Y <= 0:
Y = Y -1
h = D - int(D)
D = int(D)
h = h*24
lh = round(long/15)
h = h +lh
if h >= 24.0:
h = h - 24
D = D + 1
if D >= 32:
D = D - 31
M = M + 1
if M >= 13:
Y = Y + 1
M = M - 12
h = round(h,1)
return [Y,M,D,h]
def koseji(jd,long): # 恒星時の計算
B = jd - 2415020.0
R = 366.2422/365.2422
ST = 18.6461 + 24*B*R + 3.24e-14*B*B + long/15
ST = 24*(ST/24-int(ST/24))
if ST < 0:
ST = ST + 24
return ST
def yogen_AD(arfa,drta): # 方向余弦の計算
a = math.radians(arfa)
d = math.radians(drta)
L = math.cos(a) * math.cos(d)
M = math.cos(d) * math.sin(a)
N = math.sin(d)
return [L,M,N]
def horizon(ad): # 地平座標の計算（ST;恒星時 LAT;緯度 ad;方向余弦)
sT = math.sin(math.radians(ST))
cT = math.cos(math.radians(ST))
sL = math.sin(math.radians(LAT))
cL = math.cos(math.radians(LAT))
L = sL*cT*ad[0] + sL*sT*ad[1] - cL*ad[2]
M = -sT*ad[0] + cT*ad[1]
N = cL*cT*ad[0] + cL*sT*ad[1] + sL*ad[2]
if L == 0:
L = 0.01
h = math.asin(N)
h = math.degrees(h)
A = math.atan(-M/L)
A = math.degrees(A)
if L < 0. :
A = A + 180.
return [h,A]
def proper_move(RA,DC,V1,V2): # 固有運動
T = Cent - 1
RA = RA + V1*T/3600000/math.cos(math.radians(DC))
DC = DC + V2*T/3600000
return [RA , DC]
def saisa_hosei(ad): # 歳差補正
t = Cent - 1
f = 0.640616 * t + 0.0000839* t*t + 0.000005*t**3
z = 0.640616 * t + 0.000304 * t*t + 0.00000506*t**3
s = 0.556753 * t - 0.000119 * t*t - 0.0000116*t**3
sF = math.sin(math.radians(f))
cF = math.cos(math.radians(f))
sZ = math.sin(math.radians(z))
cZ = math.cos(math.radians(z))
sS = math.sin(math.radians(s))
cS = math.cos(math.radians(s))
L = (sZ*sF + cZ*cS*cF)*ad[0] + (sZ*cF - cZ*cS*sF)*ad[1] - cZ*sS*ad[2]
M = (cZ*sF - sZ*cS*cF)*ad[0] + (cZ*cF + sZ*cS*sF)*ad[1] + sZ*sS*ad[2]
N = sS*cF*ad[0] - sS*sF*ad[1] + cS*ad[2]
return [L, M, N]
def dispXY(hh, AA):
dot = 580 # 画面のパラメータ 中心座標（600,450)
r = dot * math.sin(math.radians((90-hh)/2))
x = r * math.sin(math.radians(AA)) + 600
y = r * math.cos(math.radians(AA)) + 450
return [x, y]
# 太陽の位置計算
def solar_Pos():
#print("Solar")
sml = 280.6824 + 36000.769325 * Cent + 7.22222e-04*Cent*Cent
sml = 360*(sml/360 - int(sml/360))
if sml < 0:
sml = sml + 360 # 平均黄経
sec = 0.0167498 - 4.258e-5*Cent - 1.37e-7*Cent*Cent # 離心率
spl = 281.2206 + 1.717697*Cent + 4.83333e-4*Cent*Cent + 2.77777e-6*Cent*Cent*Cent
spl = 360*(spl/360 -int(spl/360))
if spl < 0:
spl = spl + 360 # 近日点黄経
sma = sml - spl
if sma < 0:
sma = sma + 360
sma = math.radians(sma) # 平均近点角
smpg = 1.91946 * math.sin(sma) + 2.00939e-2*math.sin(2*sma) \
- 4.78889e-3*math.sin(sma)*Cent - 1.44444e-5*math.sin(sma)*Cent*Cent
sl = sml + smpg # 太陽黄経
sta = sl -spl # 真近点角
if sta < 0:
sta = sta + 360
sax = 1.00000129 # 軌道長半径
srr = sax*(1 - sec*sec)/(1 + sec*math.cos(math.radians(sta))) #地球-太陽距離
ss = 0.2666/srr # 視半径
sx = srr*(math.cos(math.radians(sl)))
sy = srr*(math.sin(math.radians(sl)))
sz = 0
return [srr,sx,sy,sz,sl,ss]
#水星の軌道要素
def Mercury(C):
#print("Mercury")
ml = 182.27175 + 149474.07244*C + 2.01944e-3*C*C # 平均黄径
if ml > 360:
ml = 360*(ml/360 - int(ml/360))
pnl = 75.89717 + 1.553469*C + 3.08639e-4*C*C # 近日点黄径
omg = 47.144736 + 1.18476*C + 2.23194e-4*C*C # 昇降点黄径Ω
inc = 7.003014 + 1.73833e-3*C - 1.55555e-5*C*C # 軌道傾斜角
ec = 0.20561494 + 0.0203e-3*C - 0.04e-6*C*C # 離心率
ax = 0.3870984 # 軌道長半径
return [ml,pnl,omg,inc,ec,ax]
#金星の軌道要素
def Venus(C):
#print("Venus")
ml = 344.36936 + 58519.2126*C + 9.8055e-4*C*C #平均黄径
if ml > 360:
ml = 360*(ml/360 - int(ml/360))
pnl = 130.14057 + 1.3723*C - 1.6472e-3*C*C #近日点黄径
omg = 75.7881 + 0.91403*C + 4.189e-4*C*C #昇降点黄径Ω
inc = 3.3936 + 1.2522e-3*C - 4.333e-6*C*C #軌道傾斜角
ec = 0.00681636 - 0.5384e-4*C + 0.126e-6*C*C #離心率
ax = 0.72333015 #軌道長半径
return [ml,pnl,omg,inc,ec,ax]
#火星の軌道要素
def Mars(C):
#print("Mars")
ml = 294.26478 + 19141.69625*C + 3.15028e-4*C*C #平均黄径
if ml > 360:
ml = 360*(ml/360 - int(ml/360))
pnl = 334.21833 + 1.840394*C + 3.35917e-4*C*C #近日点黄径
omg = 48.78670 + 0.776944*C - 6.02778e-4*C*C #昇降点黄径Ω
inc = 1.85030 - 6.49028e-4*C + 2.625e-5*C*C #軌道傾斜角
ec = 0.0933088 + 0.095284e-3*C - 0.122e-6*C*C #離心率
ax = 1.5236781 #軌道長半径
return [ml,pnl,omg,inc,ec,ax]
# 木星の軌道要素
def Jupiter(C,Y,JD):
#print("Jupiter")
ml = 238.132386 + 3036.301986*C + 3.34683e-4*C*C - 1.64889e-6*C**3 #平均黄径
if ml > 360:
ml = 360*(ml/360 - int(ml/360))
T = Y/1000
A = 0.42 - 0.075*T + 0.015*T*T - 0.003*T**3
L7 = A*math.sin(math.radians((T-0.62)*360/0.925)) #摂動補正（長周期）
eta = 86.1 + 0.033459*(JD - 1721057)
eta = 360*(eta/360 - int(eta/360))
if eta < 0:
eta = eta + 360
zeta = 89.1 + 0.04963*(JD - 1721057)
zeta = 360*(zeta/360-int(zeta/360))
if zeta < 0:
zeta = zeta +360
#print("eta = ",eta," zeta = ",zeta) #短周期
#L8 = input("input> L8 =")
L8 = -.02#float(L8)
ml = ml + L7 + L8
pnl = 12.720972 + 1.6099617*C + 1.05627e-3*C*C - 3.4333e-6*C**3 #近日点黄径
pnl = 360*(pnl/360 - int(pnl/360))
if pnl < 0:
pnl = pnl + 360
PS7 = 0.02*math.sin(math.radians((T + 0.1)*360/0.925))
#print(" input> PS8 ")
#PS8 = input("=")
PS8 = .0#float(PS8)
PH = 2.58 + 0.1*T
pnl = pnl + (PS7 + PS8)/math.sin(math.radians(PH))
ec = 0.0483348 + 0.16418e-3*C - 0.4676e-6*C*C - 1.7e-9*C**3 # 離心率
PH7 = 0.03*math.sin(math.radians((T + 0.36)*360/0.925))
# print(" input> PH8 ")
# PH8 = input("=")
PH8 = .4 # float(PH8)
ec = math.sin(math.radians(PH + PH7 + PH8))
omg = 99.443414 + 1.01053*C + 3.52222e-4*C*C - 8.351111e-6*C**3 # 昇降点黄径Ω
inc = 1.308736 - 5.69611e-3*C + 3.88889e-6*C*C # 軌道傾斜角
ax = 5.202805 # 軌道長半径
return [ml,pnl,omg,inc,ec,ax]
# 土星の軌道要素
def Saturn(C,Y,JD):
#print("Saturn")
ax = 9.554747 # 軌道長半径
ml = 266.597875 + 1223.50988*C + 3.24542e-4*C*C - 5.83333e-7*C**3 #平均黄径
if ml > 360:
ml = 360*(ml/360 - int(ml/360))
T = Y/1000
A = 0.88 - 0.0633*T + 0.03*T*T - 0.006*T**3
L7 = -0.5 + A*math.sin(math.radians((T-0.145)*360/0.95)) #摂動補正（長周期）
# 短周期
# L8 = input("input> L8=")
L8 = .3 # float(L8)
ml = ml + L7 + L8
pnl = 91.09821 + 1.958416*C + 8.26361e-4*C*C + 4.61111e-6*C**3 #近日点黄径
pnl = 360*(pnl/360 - int(pnl/360))
if pnl < 0:
pnl = pnl + 360
B = 0.1 - 0.005*T
PS7 = -0.5 + B*math.sin(math.radians((T - 0.54)*360/0.95))
# print(" input> PS8 ")
# PS8 = input("=")
PS8 = .4 # float(PS8)
PH = 3.56 + 0.175*T - 0.005*T*T
pnl = pnl + (PS7 + PS8)/math.sin(math.radians(PH))
ec = 0.05589231 - 3.455e-4*C - 7.28e-7*C*C + 7.4e-10*C**3 # 離心率
F = 0.1 -0.005*T
PH7 = -0.5 + F*math.sin(math.radians((T - 0.32)*360/0.95))
# print(" input> PH8 ")
# PH8 = input("=")
PH8 = .5 # float(PH8)
ec = math.sin(math.radians(PH + PH7 + PH8))
G = 0.004 - 0.0005*T
AX7 = -0.05 + G*math.sin(math.radians((T - 0.35)*360/0.95))
# print(" input> AX8 ")
# AX8 = input("=")
AX8 = .04 # float(AX8)
ax = ax + AX7 + AX8
omg = 112.790414 + 0.873195*C - 1.52181e-4*C*C - 5.30555e-6*C**3 # 昇降点黄径Ω
inc = 2.49252 - 3.91889e-3*C - 1.54889e-5*C*C + 4.44444e-8*C**3 # 軌道傾斜角
return [ml,pnl,omg,inc,ec,ax]
def pl_position(el): # 惑星の位置計算
ml = el[0] ; pnl=el[1] ; omg=el[2] ; inc=el[3] ; ec=el[4] ; ax=el[5]
ma = ml -pnl # 平均近点角(Mean Anomaly)
ma = 360*(ma/360 - int(ma/360))
if ma < 0:
ma = ma + 360
# print(" ma=",ma)
mar = math.radians(ma)
mpg = (2*ec-(ec*ec*ec)/4)*math.sin(mar) + 1.25*math.sin(2*mar)*ec*ec \
+ (13/12)*math.sin(3*mar)*ec**3
mpg = math.degrees(mpg)
# print(" ml=",ml)
ta = ma + mpg # 真近点角(Ture Anomaly)
uu = ta + pnl - omg
if uu < 0:
uu = uu + 360
aa = math.cos(math.radians(inc))*math.tan(math.radians(uu))
cc = math.atan(aa)
cc = math.degrees(cc)
if uu > 90 and uu < 270:
cc = cc + 180
if uu > 270:
cc = cc + 360
bb = math.tan(math.radians(inc))*math.sin(math.radians(cc))
ll = cc + omg # 日心黄径
if ll > 360:
ll = ll - 360
# print(" ll =",ll)
tb = math.atan(bb)
tb = math.degrees(tb) # 日心黄緯
rr = ax*(1 - ec*ec)/(1 + ec*math.cos(math.radians(ta))) # 動径
xx = rr*(math.cos(math.radians(uu))*math.cos(math.radians(omg)) \
- math.sin(math.radians(uu))*math.sin(math.radians(omg))*math.cos(math.radians(inc)))
yy = rr*(math.cos(math.radians(uu))*math.sin(math.radians(omg)) \
+ math.sin(math.radians(uu))*math.cos(math.radians(omg))*math.cos(math.radians(inc)))
zz = rr*(math.sin(math.radians(uu))*math.sin(math.radians(inc)))
# tt = math.sqrt(xx**2 + yy**2 + zz**2) # 太陽との距離＝動径
# print(" rr=",rr)
return [rr,xx,yy,zz,ll,tb]
def sekido(): # 赤道・黄道の描画
sekiR = [0.0]*182
A = [0.0]*182
hh = [0.0]*182
xl = [0.0]*182
yl = [0.0]*182
sekiD = [0.0]*182
kodoD = [0.0]*182
for i in range(0,181):
sekiR[i] = i*2
sekiD[i] = 0
kodoD[i] = 23.4392*math.sin(math.radians(i*2))
n = 0
for i in range(182):
ad = yogen_AD(sekiR[i],sekiD[i])
h = horizon(ad)
if h[0] < 0.2:
continue
hh[n],A[n] = h
n += 1
for i in range(n):
xy= dispXY(hh[i],A[i])
xl[i] ,yl[i]= xy
for i in range(n-1):
if xl[i+1] - xl[i] > 50:
continue
app.co_line(xl[i], yl[i], xl[i+1], yl[i+1], '#710071')
n = 0
for i in range(182):
ad = yogen_AD(sekiR[i], kodoD[i])
# ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] < 0.2:
continue
hh[n],A[n] = h
n += 1
for i in range(n):
xy= dispXY(hh[i],A[i])
xl[i] ,yl[i] = xy
for i in range(n-1):
if xl[i+1] - xl[i] > 50 :
continue
app.co_line(xl[i], yl[i], xl[i+1], yl[i+1], '#969600')
def star_color(CL): # 恒星の色 CL：color index
if CL < -0.16:
c = "#a09eff"
elif CL < 0.15:
c = "#a0d7ff"
elif CL < 0.45:
c = "#d7e8ff"
elif CL < 0.68:
c = "#ffffff"
elif CL < 1.15:
c = "#ffffdc"
elif CL < 1.6:
c = "#ffe6aa"
else:
c = "#ffd7b1"
return c
def magnitude(m): #等級を星の大きさに
if m < 0.0:
rd = 7
elif m < 1.0:
rd = 6
elif m < 2.0:
rd = 5
elif m < 3.0:
rd = 4
elif m < 4.0:
rd = 3
else:
rd = 2
return rd
class Conline: # 星座線クラス
def __init__(self):
self.lcnum = 0
self.linRas = 0
self.linDcs = 0
self.linV1s = 0
self.linV2s = 0
self.linRae = 0
self.linDce = 0
self.linV1e = 0
self.linV2e = 0
class Star: # 星クラス
def __init__(self):
self.stnum = 0
self.stV1 = 0
self.stV2 = 0
self.stRA = 0
self.stDC = 0
self.stMg = 0
self.stCL = 0
class Constelation: # 星座クラス
def __init__(self):
self.con_name = ""
self.con_Ra = 0
self.con_Dc = 0
class Planetarium: # プラネタリウムクラス
# 惑星表示のための変数
ex = [0.0]*5
ey = [0.0]*5
ez = [0.0]*5
xq = [0.0]*5
yq = [0.0]*5
zq = [0.0]*5
dd = [0.0]*5
lam = [0.0]*5
bet = [0.0]*5
ii = [0.0]*5
R = [0.0]*5
pmag = [0.0] * 5
pl_RA = [0.0] * 5
pl_DC = [0.0] * 5
ph = [0.0] * 5
pA = [0.0] * 5
pname = [''] * 5
pelm = [0.0, 0.0, 0.0, 0.0, 0.0, 0.0] * 5
xp = [0.0] * 5
yp = [0.0] * 5
br = [0.0] * 5
xyz = [0.0, 0.0, 0.0, 0.0, 0.0, 0.0] * 5
plane_counter = 0
# 星表示のための変数
XX = [0.0] * 1000
YY = [0.0] * 1000
hh = [0.0] * 1000
AA = [0.0] * 1000
MG = [0.0] * 1000
CLs = [0.0] * 1000
rd = [0] * 1000
hLs = [0.0] * 500
hLe = [0.0] * 500
ALs = [0.0] * 500
ALe = [0.0] * 500
x1 = [0.0] * 500
y1 = [0.0] * 500
x2 = [0.0] * 500
y2 = [0.0] * 500
nh = [0.0] * 60
nA = [0.0] * 60
xn = [0.0] * 60
yn = [0.0] * 60
coname = [""] * 60
star_counter = 0
line_counter = 0
con_counter = 0
def __init__(self):
# 星、星座線リストを作る
self.star_list = list()
self.conline_list = list()
self.conste_list = list()
for i in range(1263):
self.star_list.append(Star())
for i in range(673):
self.conline_list.append(Conline())
for i in range(89):
self.conste_list.append(Constelation())
# データ読み込み
with open("starData1263.csv", "r") as f: # 恒星ファイル読み込み
stDATA = csv.reader(f, delimiter=",")
i = 0
for row in stDATA:
self.star_list[i].stnum = int(row[4]) #No.
self.star_list[i].stV1 = float(row[1]) #固有運動RA
self.star_list[i].stV2 = float(row[2]) # DC
self.star_list[i].stRA = float(row[6]) #赤経
self.star_list[i].stDC = float(row[7]) #赤緯
self.star_list[i].stMg = float(row[5]) #光度
self.star_list[i].stCL = float(row[8]) #色指数
i += 1
with open("cons_lineData.csv", "r") as f: #星座線ファイル読み込み
szL=csv.reader(f,delimiter=",")
i = 0
for row in szL:
self.conline_list[i].lcnum = str(row[0]) #星座コード
self.conline_list[i].linRas = float(row[1]) #始点
self.conline_list[i].linDcs = float(row[2])
self.conline_list[i].linV1s = float(row[3])
self.conline_list[i].linV2s = float(row[4])
self.conline_list[i].linRae = float(row[5]) #終点
self.conline_list[i].linDce = float(row[6])
self.conline_list[i].linV1e = float(row[7])
self.conline_list[i].linV2e = float(row[8])
i += 1
with open("cons_nameData.csv", "r") as f: # 星座名ファイル読み込み
szM=csv.reader(f,delimiter=",")
i = 0
for row in szM:
self.conste_list[i].con_name = str(row[0]) # 星座名
self.conste_list[i].con_Ra = float(int(row[1])*15+int(row[2])*0.25)
self.conste_list[i].con_Dc = float(row[3])
i += 1
def star_culc(self): # 恒星表示メソッド
for lin in self.conline_list: #固有運動の補正
ads = proper_move(lin.linRas,lin.linDcs,lin.linV1s,lin.linV2s)
lin.linRas = ads[0]
lin.linDcs = ads[1]
ade = proper_move(lin.linRae,lin.linDce,lin.linV1e,lin.linV2e)
lin.linRae = ade[0]
lin.linDce = ade[1]
m = 0 # 星座線の地平座標計算
for line in self.conline_list:
ad = yogen_AD(line.linRas,line.linDcs)
ad = saisa_hosei(ad)
hs = horizon(ad)
if hs[0] < 0.0:
continue
ad = yogen_AD(line.linRae,line.linDce)
ad = saisa_hosei(ad)
he = horizon(ad)
if he[0] < 0.0:
continue
self.hLs[m],self.ALs[m] = hs
self.hLe[m],self.ALe[m] = he
m += 1
self.line_counter = m
i = 0
for i in range( self.line_counter): # 画面上の座標
xy= dispXY(self.hLs[i],self.ALs[i])
self.x1[i] ,self.y1[i] = xy
xy= dispXY(self.hLe[i],self.ALe[i])
self.x2[i] ,self.y2[i] = xy
for star in self.star_list: # 固有運動の補正
ad = proper_move(star.stRA,star.stDC,star.stV1,star.stV2)
star.stRA = ad[0]
star.stDC = ad[1]
n = 0 # 恒星の地平座標計算
for star in self.star_list:
ad = yogen_AD(star.stRA,star.stDC)
ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] < 0.0:
continue
self.hh[n],self.AA[n] = h
self.MG[n] = star.stMg
self.CLs[n] = star.stCL
n += 1
self.star_counter = n
for i in range(self.star_counter):
xy= dispXY(self.hh[i],self.AA[i])
self.XX[i] ,self.YY[i] = xy
n = 0 #星座名表示の地平座標計算
for c in self.conste_list:
ad = yogen_AD(c.con_Ra,c.con_Dc)
ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] < 0.0:
continue
self.nh[n] ,self.nA[n] = h
self.coname[n] = c.con_name
n += 1
self.con_counter = n
for i in range(self.con_counter):
xy= dispXY(self.nh[i],self.nA[i])
self.xn[i] ,self.yn[i] = xy
def star_display(self):
# 星座線を引く
for i in range( self.line_counter):
app.co_line(self.x1[i], self.y1[i], self.x2[i], self.y2[i], 'blue')
# 星のプロット
for i in range(self.star_counter):
self.rd[i] = magnitude(self.MG[i])
color = star_color(self.CLs[i])
app.point_star(self.XX[i], self.YY[i], self.rd[i]/2, color)
#星座名の表示
for i in range(self.con_counter):
app.text_in(self.xn[i], self.yn[i], self.coname[i], 'red')
def coordinate_Planet(self): # 惑星の位置計算
#
sxyz = solar_Pos()
sx = sxyz[1] ; sy = sxyz[2] ; sz = sxyz[3] ; srr = sxyz[0] ; sl = sxyz[4]
T = (YY - 1900)/100
obl = 23.4523 - 1.30125e-2*T # 黄道傾斜角
cos = math.cos(math.radians(obl))
sin = math.sin(math.radians(obl))
for ip in range(5):
if ip == 0:
self.pelm[0] = Mercury(Cent)
self.pname[0] ="Mercury"
if ip == 1:
self.pelm[1] = Venus(Cent)
self.pname[1] ="Venus"
if ip == 2:
self.pelm[2] = Mars(Cent)
self.pname[2] ="Mars"
if ip == 3:
self.pelm[3] = Jupiter(Cent,YY,JD)
self.pname[3] ="Jupiter"
if ip == 4:
self.pelm[4] = Saturn(Cent,YY,JD)
self.pname[4] ="Saturn"
self.xyz = pl_position(self.pelm[ip])
self.ex[ip] = self.xyz[1] + sx # 黄道地心座標
self.ey[ip] = self.xyz[2] + sy
self.ez[ip] = self.xyz[3] + sz
self.dd[ip] = math.sqrt(self.ex[ip]**2 + self.ey[ip]**2 + self.ez[ip]**2) # 地心距離
# 赤道地心座標に変換
self.xq[ip] = self.ex[ip]
self.yq[ip] = self.ey[ip]*cos - self.ez[ip]*sin
self.zq[ip] = self.ey[ip]*sin + self.ez[ip]*cos
self.R[ip] = math.sqrt(self.xq[ip]**2 + self.yq[ip]**2 + self.zq[ip]**2)
self.pl_RA[ip] = math.degrees(math.atan(self.yq[ip] / self.xq[ip]))
if self.xq[ip] <= 0.0:
self.pl_RA[ip] = self.pl_RA[ip] + 180
self.pl_DC[ip] = math.degrees(math.asin(self.zq[ip] / self.R[ip]))
# 位相角の計算
self.lam[ip] = self.ey[ip] / self.ex[ip]
self.bet[ip] = self.ez[ip] / self.dd[ip]
self.bet[ip] = math.asin(self.bet[ip])
self.bet[ip] = math.degrees(self.bet[ip]) #地心黄緯
self.lam[ip] = math.atan(self.lam[ip])
self.lam[ip] = math.degrees(self.lam[ip]) #地心黄径
if self.ex[ip] < 0:
self.lam[ip] = self.lam[ip] + 180
if self.ex[ip] > 0 and self.ey[ip] < 0:
self.lam[ip] = self.lam[ip] + 360
# print("lam = ",self.lam[ip]," bet= ",self.bet[ip])
# elo = self.lam[ip] - sl #太陽との離隔
# print(" elo=",elo)
hl = self.xyz[4] - sl
if hl < -180:
hl = hl + 360
d2 = math.sqrt(self.xyz[0]**2 + srr**2 + 2*self.xyz[0]*srr*math.cos(math.radians(hl)))
# print("d2=",d2," rr=",xyz[0])
self.ii[ip] = (self.xyz[0]**2 + d2*d2 - srr**2)/(2*self.xyz[0]*d2)
self.ii[ip] = math.acos(self.ii[ip])
self.ii[ip] = math.degrees(self.ii[ip]) #位相角
if self.ii[ip] < 0:
self.ii[ip] = self.ii[ip] + 180
# 惑星の明るさ（光度）
if ip == 0:
self.br[ip] = 1.16 + 5*math.log10(self.xyz[0]*d2) + 0.02838*abs(self.ii[ip]-50) + 1.023e-4*abs((self.ii[ip]-50)**2)
if ip == 1:
self.br[ip] = -4 + 5*math.log10(self.xyz[0]*d2) + 0.01322*abs(self.ii[ip]) + 0.4247e-6*abs(self.ii[ip]**3)
if ip == 2:
self.br[ip] = -1.3 + 5*math.log10(self.xyz[0]*d2) + 0.01486*abs(self.ii[ip])
if ip == 3:
self.br[ip] = -8.93 + 5*math.log10(self.xyz[0]*d2)
if ip == 4:
self.br[ip] = -8.68 + 5*math.log10(self.xyz[0]*d2)
# print(" hl=",hl," ii =",self.ii[ip]," br=",self.br[ip])
self.plane_counter = 0 # 惑星の地平座標を計算
for i in range(5):
ad = yogen_AD(self.pl_RA[i],self.pl_DC[i])
# ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] < 0.0 :
continue
self.ph[self.plane_counter], self.pA[self.plane_counter] = h
self.pname[self.plane_counter] = self. pname[i]
self.br[self.plane_counter] = self.br[i]
self.plane_counter += 1
for i in range(self.plane_counter):
self.xy= dispXY(self.ph[i],self.pA[i])
self.xp[i], self.yp[i] = self.xy
def planet_display(self):
# 惑星の表示
for i in range(self.plane_counter):
self.br[i] = magnitude(self.br[i])
self.br[i] = self.br[i]/2
app.point_star(self.xp[i], self.yp[i], self.br[i], "yellow")
app.text_in(self.xp[i]-10,self.yp[i]-8, self.pname[i], 'white')
def solar_display(self):
# 太陽の表示
sxyz = solar_Pos()
sx = sxyz[1] ; sy = sxyz[2]; sz = sxyz[3]; srr = sxyz[0]; ss = sxyz[5]
ss = int(ss * 25) # 視半径を画面サイズに
obl = 23.4523 - 1.30125e-2*Cent # 黄道傾斜角
cos = math.cos(math.radians(obl))
sin = math.sin(math.radians(obl))
xq = sx
yq = sy * cos - sz * sin
zq = sy * sin + sz * cos
sun_R = math.sqrt(xq**2 + yq**2 + zq**2)
sun_RA = math.degrees(math.atan(yq / xq))
if xq < 0.0:
sun_RA = sun_RA + 180
sun_DC = math.degrees(math.asin(zq / sun_R))
ad = yogen_AD(sun_RA,sun_DC)
# ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] > 0.0 :
xy= dispXY(h[0],h[1])
app.point_star(xy[0], xy[1], ss, 'white')
app.text_in(xy[0]-8,xy[1]-12, "Solar", 'white')
def luna_display(self): # 月の位置計算と表示
# print("Luna")
J = (JD -2378496)/36525 # Epoch A.D.1800 I 0.5 UT
ml = 335.723436 + 481267.887361*J + 3.38888e-3*J*J + 1.83333e-6*J**3 # 平均黄径
ml = 360*(ml/360 - int(ml/360))
if ml < 0:
ml = ml + 360
# 摂動補正
AA = 1.2949 + 413335.4078*J -7.2201e-3*J*J - 7.2305e-6*J**3
AA = 360*(AA/360 - int(AA/360))
BB = 111.6209 + 890534.2514*J + 6.9838e-3*J*J + 6.9778e-6*J**3
BB = 360*(BB/360 - int(BB/360))
CC = 180.40885 + 35999.0552*J -0.0001988*J*J
CC = 360*(CC/360 - int(CC/360))
DD = 0.88605 + 377336.3526*J - 7.0213e-3*J*J - 7.2305e-6*J**3
DD = 360*(DD/360 - int(DD/360))
EE = 111.21205 + 854535.1962*J + 7.1826e-3*J*J + 6.9778e-6*J**3
EE = 360*(EE/360 - int(EE/360))
HH = 169.1706 + 407332.2103*J + 5.3354e-3*J*J + 5.3292e-6*J**3
HH = 360*(HH/360 - int(HH/360))
A0 = 1.2408*math.sin(math.radians(AA))
B0 = 0.5958*math.sin(math.radians(BB))
C0 = 0.1828*math.sin(math.radians(CC))
D0 = 0.055*math.sin(math.radians(DD))
E0 = 0.0431*math.sin(math.radians(EE))
H0 = 0.1453*math.sin(math.radians(HH))
st = A0 + B0 + C0 + D0 + E0
ml = ml + st
pnl = 225.397325 + 4069.053805*J - 1.02869e-2*J*J - 1.22222e-5*J**3 #近日点黄径
pnl = 360*(pnl/360 - int(pnl/360))
ma = ml - pnl
ec = 0.05490897 # 離心率
ma = math.radians(ma)
EX = ma
SS = EX - ec*math.sin(EX) - ma
# kepplar equation
while abs(SS) > 1.0e-8:
DE = SS/(1 - ec*math.cos(EX))
EX = EX - DE
SS = EX - ec*math.sin(EX) - ma
TT = math.sqrt((1 + ec)/(1 - ec))*math.tan(EX/2)
TA = 2*math.atan(TT)
TA = math.degrees(TA)
if TA < 0:
TA = TA +360
omg = 33.272936 - 1934.144694*J + 2.08028e-3*J*J + 2.08333e-6*J**3 # 昇降点黄径Ω
omg = 360*(omg/360 - int(omg/360))
if omg < 0:
omg = omg + 360
uu = pnl - omg + TA
uu = 360*(uu/360 - int(uu/360))
inc = 5.144433 # 軌道傾斜角
JJ = math.cos(math.radians(inc))*math.tan(math.radians(uu))
MM = math.atan(JJ)
MM = math.degrees(MM)
if math.cos(math.radians(uu)) < 0:
MM = MM + 180
MM = 360*(MM/360 - int(MM/360))
lam = MM + omg
lam = 360*(lam/360 - int(lam/360))
BE = math.tan(math.radians(inc))*math.sin(math.radians(MM))
tb = math.atan(BE)
tb = math.degrees(tb)
tb = tb + H0 # lam tb :地心視位置（黄経，黄緯）
lst = koseji(JD,long)
lst = lst*15
ax = 60.2682 # 軌道長半径(地球半径を１とする）
RR = ax*(1 - ec*math.cos(EX)) # 地心距離
G = 1/RR/.99
PI = math.asin(G)
PI = math.degrees(PI) # 月の赤道水平視差
obl = 23.4523 - 0.013*Cent -1.6388e-6*Cent*Cent
A = math.cos(math.radians(obl))*math.cos(math.radians(LAT))*math.sin(math.radians(lst)) \
+ math.sin(math.radians(obl))*math.sin(math.radians(LAT))
B = math.cos(math.radians(LAT))*math.cos(math.radians(lst))
L = math.atan(A/B)
L = math.degrees(L) # 観測地点の地心黄経
if A < 0 and B < 0 :
L = L + 180
if A < 0 and B > 0:
L = L +360
if A > 0 and B < 0:
L = L + 180
JJ = - math.sin(math.radians(obl))*math.cos(math.radians(LAT))*math.sin(math.radians(lst))\
+ math.cos(math.radians(obl))*math.sin(math.radians(LAT))
B = math.asin(JJ)
B = math.degrees(B) # 観測地点の黄緯
# 視差の計算
PP = math.sin(math.radians(PI))*math.cos(math.radians(B))*math.sin(math.radians(L - lam))\
/math.cos(math.radians(tb))
lam1 = math.asin(PP)
lam1 = -math.degrees(lam1)
GG = math.tan(math.radians(B))/math.cos(math.radians(L - lam))
GA1 = math.atan(GG)
GA1 = math.degrees(GA1)
QQ = math.sin(math.radians(PI))*math.sin(math.radians(B))*math.sin(math.radians(GA1-tb))\
/math.sin(math.radians(GA1))
tb1 = -math.asin(QQ)
tb1 = math.degrees(tb1)
lam2 = lam + lam1
tb2 = tb + tb1
obl = 23.452 - 1.30125e-2*Cent
s = math.cos(math.radians(obl))*math.sin(math.radians(tb2)) + math.sin(math.radians(obl))*math.cos(math.radians(tb2))*math.sin(math.radians(lam2))
luna_DC = math.asin(s)
luna_DC = math.degrees(luna_DC)
A = -math.sin(math.radians(obl))*math.sin(math.radians(tb2)) + math.cos(math.radians(obl))*math.cos(math.radians(tb2))*math.sin(math.radians(lam2))
B = math.cos(math.radians(tb2))*math.cos(math.radians(lam2))
luna_RA = math.atan(A/B)
luna_RA = math.degrees(luna_RA)
if A > 0 and B < 0 :
luna_RA = luna_RA + 180
if A < 0 and B > 0:
luna_RA = luna_RA + 360
if A < 0 and B < 0:
luna_RA = luna_RA + 180
# 視半径
K = 0.2725*G
ms = math.asin(K)
ms = math.degrees(ms)
ms = int(ms*25)
# Moon's phase
solar = solar_Pos()
mp = lam2 - solar[4]
mp = 360*(mp/360 - int(mp/360))
if mp < 0:
mp = mp + 360
# Earth's shadow
moo = lam - solar[4] - 180
if moo < 0:
moo = moo + 360
bke = 1 / (60.2682*(1 - ec*math.cos(EX)))
bke = math.degrees(bke)
bae = 2.443e-3 / solar[0]
kem = bke - solar[5] + bae
kem = int(1.02 * 12 * kem) # 地球の本影の半径(display)
# oek = 0.25905 / (1 - ec*math.cos(EX)) 月の支直径
# print("moo =",moo ,"kem=",kem,"oek=",oek)
sx = solar[1] ; sy = solar[2] ; sz = solar[3]
cos = math.cos(math.radians(obl))
sin = math.sin(math.radians(obl))
xq = sx
yq = sy * cos - sz * sin
zq = sy * sin + sz * cos
sun_R = math.sqrt(xq**2 + yq**2 + zq**2)
sun_RA = math.degrees(math.atan(yq / xq))
if xq < 0.0:
sun_RA = sun_RA + 180
sun_DC = math.degrees(math.asin(zq / sun_R))
sdRA = sun_RA + 180
if sdRA >360:
sdRA = sdRA - 360
sdDC = - sun_DC
ad = yogen_AD(sdRA,sdDC) # 月食の影の描画
# ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] > 0.0 :
xy= dispXY(h[0],h[1])
app.point_eclip(xy[0], xy[1], kem, 'green')
app.text_in(xy[0]-20, xy[1]-20, "shadow", 'gray')
# 月の描画
ad = yogen_AD(luna_RA,luna_DC)
#ad = saisa_hosei(ad)
h = horizon(ad)
if h[0] > 0.0 :
xy= dispXY(h[0],h[1])
app.point_star(xy[0], xy[1], ms, 'gray')
app.text_in(xy[0]-8, xy[1]-12, "Moon", 'white')
# print(" 月齢 = ",round(mp*0.082,1))
return round(mp*0.082,1)
class Time:
def __init__(self,Y,D,lo):
self.Ydate = Y
self.Dtime = D
self.LAT = 34.6
self.JD = 0
self.ST = 0
self.Cent = 0
self.YY = 0
self.long = lo
def Julian(self): # （ユリウス日）の計算
self.JD = 0
if self.Ydate != abs(self.Ydate):
SP1 = -1
self.Ydate = abs(self.Ydate)
else:
SP1 = 1
self.YY = int(self.Ydate/10000)
MD = int(self.Ydate-10000*self.YY)
MM = int(MD/100)
DD = MD - 100 * MM
HH = int(self.Dtime/100)
MS = self.Dtime-100*HH
if SP1 < 0:
self.YY = self.YY * SP1 # +1 BC.でなく，BC1年を0年として－で入力する
SP2 = self.YY + (MM-1)/12 + DD/365.25
if MM <= 2 :
MM = MM + 12
self.YY = self.YY - 1
if self.YY < 0:
self.JD = math.floor(365.25*self.YY) + int(30.59*(MM-2)) + DD - self.long/360 + 1721086.5
else:
self.JD = int(365.25*self.YY) + int(30.59*(MM-2)) + DD - self.long/360 + 1721086.5
if SP2 > 1582.78: # グレゴリオ暦以降
self.JD = self.JD + int(self.YY/400) - int(self.YY/100) + 2
if MM > 12:
MM = MM - 12
self.YY = self.YY + 1
self.JD = self.JD + HH/24 + MS/1440
self.ST = koseji(self.JD,self.long)*15 # ST 恒星時(度)
self.Cent = (self.JD - 2415021.0)/36525 # 元期1900年I.1 0.5
def Batch():
app.refresh()
plt.star_culc()
plt.star_display()
plt.coordinate_Planet()
plt.planet_display()
plt.solar_display()
plt.luna_display()
def update(event):
global LAT
global long
global ymd
global ST
global Cent
global YY
global JD
gvl.getV()
Dtime = gvl.D_time
Dtime = float(Dtime)
Ydate = gvl.Y_date
Ydate = float(Ydate)
long = gvl.LONG
long = float(long)
LAT = gvl.Lat
LAT = float(LAT)
tm = Time(Ydate, Dtime, long)
tm.Julian()
JD = tm.JD
ST = tm.ST
Cent = tm.Cent
YY = tm.YY
ymd = JDT(JD)
Batch()
def Timeforward():
global ST
global JD
ymd[3] = ymd[3] + 1
ST = ST + 15
JD = JD + (1/24)
Batch()
def Timeback():
global ST
global JD
ymd[3] = ymd[3] - 1
ST = ST - 15
JD = JD - (1/24)
Batch()
def Dateforward():
global ST
global JD
ymd[2] = ymd[2] + 1
ST = ST + 1.002738
JD = JD + 1
Batch()
def Dateback():
global ST
global JD
ymd[2] = ymd[2] - 1
ST = ST - 1.002738
JD = JD -1
Batch()
class Application(tk.Frame):
def __init__(self,master = None):
super().__init__(master)
master.title(u"星座早見（古天文学バージョン2.4）")
master.geometry("1200x900")
self.c0 = tk.Canvas(master=None, width = 1200, height = 900, bg="#001766")
self.pack()
self.create_widgets()
def create_widgets(self):
self.c0.create_oval(190, 40, 1010, 860, fill = 'black',outline = 'skyblue',width =1)
self.c0.pack()
self.c0.create_text(600, 20, text="N", font=('', 18), fill="yellow")
self.c0.create_text(600, 880, text="S", font=('', 18), fill="yellow")
self.c0.create_text(170, 450, text="E", font=('', 18), fill="yellow")
self.c0.create_text(1030, 450, text="W", font=('', 18), fill="yellow")
self.c0.create_text(1055, 720, text="その日の時刻を１時間", font=('', 12), anchor='c', fill="white")
self.c0.create_text(1055, 785, text="日付を１日", font=('', 12), anchor='c', fill='white')
self.c0.create_text(35, 820, text="紀元前はB.C.1年を0年として計算する。入力は-１で", font=('', 10), fill='white', anchor='w')
self.lb1 = tk.Label(text=u"観測地の緯度・経度(南緯は－，東経は＋）", fg='white', bg="#001766", anchor='w', font=('', 14)).place(x=830,
y=30)
self.inputbox1 = tk.Entry(width=4, font=('', 14))
self.inputbox1.place(x=920, y=60)
self.inputbox1.insert(tk.END, "34.6")
self.inputbox1.bind("<KeyPress-Return>", update)
self.inputbox2 = tk.Entry(width=6, font=('', 14))
self.inputbox2.place(x=1000, y=60)
self.inputbox2.insert(tk.END, "135.7")
self.inputbox2.bind("<KeyPress-Return>", update)
self.lb2 = tk.Label(text="日付(YYYYMMDD) 時刻(hhmm)", fg='white', bg="#001766", anchor='w', font=('', 14)).place(x=900,
y=95)
self.inputbox3 = tk.Entry(width=10, font=('', 14))
self.inputbox3.place(x=950, y=120)
self.inputbox3.insert(tk.END, "6280410")
self.inputbox3.bind("<KeyPress-Return>", update)
self.inputbox4 = tk.Entry(width=6, font=('', 14))
self.inputbox4.place(x=1080, y=120)
self.inputbox4.insert(tk.END, "0900")
self.inputbox4.bind("<KeyPress-Return>", update)
self.lb3 = tk.Label(text=u'入力→Enterで再表示します', width=22, font=('', 12), fg='#001766', bg='skyblue').place(x=950, y=165)
self.Button1 = tk.Button(text=u'進む>>', command=Timeforward, width=10, font=('', 10)).place(x=1060, y=740)
self.Button2 = tk.Button(text=u'<<もどる', command=Timeback, width=10, font=('', 10)).place(x=960, y=740)
self.Button3 = tk.Button(text=u'進む>', command=Dateforward, width=10, font=('', 10)).place(x=1060, y=800)
self.Button4 = tk.Button(text=u'<もどる', command=Dateback, width=10, font=('', 10)).place(x=960, y=800)
def refresh(self): # 再表示
global img_moon # create_imageに必要
self.c0.create_oval(150, 1, 1050, 899, fill="#001766", outline="#001766")
self.c0.create_text(600, 20, text="N", font=('', 18), fill="yellow")
self.c0.create_text(600, 880, text="S", font=('', 18), fill="yellow")
self.c0.create_text(170, 450, text="E", font=('', 18), fill="yellow")
self.c0.create_text(1030, 450, text="W", font=('', 18), fill="yellow")
self.c0.create_oval(190, 40, 1010, 860, fill='black', outline='skyblue', width=1)
self.c0.pack()
iDir = os.path.abspath(os.path.dirname(__file__))
img_moon = tk.PhotoImage(file=iDir + '\moon-phase\m' + str(int(plt.luna_display())) + '.gif')
self.c0.create_image(150, 740, image=img_moon, anchor='sw')
self.c0.pack()
if ymd[0] <= 0:
self.lb4 = tk.Label(text=f"B.C. {-ymd[0]}年 {ymd[1]}月 {ymd[2]}日 {ymd[3]} 時の星空(地方時） ", fg='white', \
bg="#001766", anchor='w', font=('', 14))
else:
self.lb4 = tk.Label(text=f"A.D. {ymd[0]}年 {ymd[1]}月 {ymd[2]}日 {ymd[3]} 時の星空(地方時） ", fg='white', \
bg="#001766", anchor='w', font=('', 14))
self.lb4.place(x=30, y=25)
self.lb5 = tk.Label(text=f"緯度= {LAT}°経度= {long}°", fg='white', bg="#001766", anchor \
='w', font=('', 14))
self.lb5.place(x=30, y=60)
# self.c0.create_oval(185, 35, 1015, 865, fill='black', outline='skyblue', width=1)
self.lb6 = tk.Label(text=f" ユリウス日は = {round(JD, 3)} 日 ", fg='white', bg="#001766", anchor \
='w', font=('', 10))
self.lb6.place(x=30, y=750)
self.lb7 = tk.Label(text=f" 恒星時は = {round(ST / 15, 1)} 時 ", fg='white', bg="#001766", anchor \
='w', font=('', 10))
self.lb7.place(x=30, y=780)
self.lb8 = tk.Label(text=f" 月齢 = {plt.luna_display()} ", fg='white', bg="#001766", anchor \
='w', font=('', 12))
self.lb8.place(x=30, y=720)
sekido()
def point_star(self, X, Y, dir, color):
self.c0.create_oval(X-dir, Y-dir, X+dir, Y+dir, fill = color)
self.c0.pack()
def co_line(self, X1, Y1, X2, Y2, color):
self.c0.create_line(X1, Y1, X2, Y2, fill = color, smooth = "True")
self.c0.pack()
def text_in(self, X, Y, name, color):
self.c0.create_text(X, Y, text = name, font = ('',8), fill = color)
self.c0.pack()
def point_eclip(self, X, Y, dir, color):
self.c0.create_oval(X-dir, Y-dir, X+dir, Y+dir, outline = color, )
self.c0.pack()
class Get_Value(Application):
def __init__(self,master=None):
super().__init__(master)
self.Lat = 0
self.LONG = 0
self.Y_date = 0
self.D_time = 0
def getV(self):
self.Lat = self.inputbox1.get()
self.LONG = self.inputbox2.get()
self.Y_date = self.inputbox3.get()
self.D_time = self.inputbox4.get()
plt = Planetarium()
root = tk.Tk()
root.resizable(width=False, height=False)
app = Application(master=root) # tkinter(GUI)
gvl = Get_Value(master=root) # 設定変更値の取得
# 日時の計算
tm = Time(6280410, 900, 135.7) # 初期設定（年月日，時刻，経度
tm.Julian()
JD = tm.JD
ST = tm.ST
Cent = tm.Cent
YY = tm.YY
long = tm.long # 経度
LAT = tm.LAT # 緯度
ymd = JDT(JD)
Batch()
if __name__ == '__main__':
app.mainloop()