def moon_asteroid(pos):
moon_RA_deg = od.HMStoDeg(pos[0])
ast_RA_deg = od.HMStoDeg(pos[1])
moon_dec_deg = od.DMStoDeg(pos[2])
ast_dec_deg = od.DMStoDeg(pos[3])
angle = 0
m_RA = moon_RA_deg * pi / 180
a_RA = ast_RA_deg * pi / 180
m_dec = moon_dec_deg * pi / 180
a_dec = ast_dec_deg * pi / 180
RA_dif = abs(m_RA - a_RA)
angle = acos(
sin(m_dec) * sin(a_dec) + cos(m_dec) * cos(a_dec) * cos(RA_dif))
ang_sep_deg = angle / pi * 180
deg = int(ang_sep_deg)
minute = int((ang_sep_deg - int(ang_sep_deg)) * 60)
sec = ang_sep_deg % 15 / 1000 * 60
ang_sep = str(deg) + ':' + str(minute) + ':' + str(sec)
print('Date and time: July 7 05:00 to 08:00 UTC')
print('RA and Dec for 99795: 17:37:59.80, -24:55:30.8')
print('RA and Dec for moon: 11:07:22.52, +09:31:09.1')
print('Angular separation between the Moon and 99795: ', ang_sep)
def getRhoHat(rah, ram, ras, dech, decm, decs):
raRad = odlib.degreesToRadians(odlib.HMStoDeg(rah, ram, ras))
decRad = odlib.degreesToRadians(odlib.DMStoDeg(dech, decm, decs))
rhox = cos(raRad) * cos(decRad)
rhoy = sin(raRad) * cos(decRad)
rhoz = sin(decRad)
return [rhox, rhoy, rhoz]
def find_vector():
RA = [[18, 41, 48.08], [18, 14, 30.53], [17, 54, 29.36]]
DEC = [[36, 15, 14.1], [36, 9, 46.0], [34, 29, 32.2]]
for i in range(3):
RA[i] = od.HMStoDeg(RA[i]) * pi / 180
DEC[i] = od.DMStoDeg(DEC[i]) * pi / 180
rho_hat1 = [
cos(RA[0]) * cos(DEC[0]),
sin(RA[0]) * cos(DEC[0]),
sin(DEC[0])
] # calculating rho from RA and Dec
rho_hat2 = [
cos(RA[1]) * cos(DEC[1]),
sin(RA[1]) * cos(DEC[1]),
sin(DEC[1])
]
rho_hat3 = [
cos(RA[2]) * cos(DEC[2]),
sin(RA[2]) * cos(DEC[2]),
sin(DEC[2])
]
rho1 = [0.07410335127715940, -.4015611046271995,
0.2994573000142365] # exact rho values
rho2 = [0.02816887198319436, -0.4437310883473226, 0.3249882273840305]
rho3 = [-0.01187334735101580, -0.4953819999141603, 0.3404906007681184]
rho_hat_1_ex = [
rho1[0] / od.mag(rho1), rho1[1] / od.mag(rho1), rho1[2] / od.mag(rho1)
] # rho hat calculation from exact values
rho_hat_2_ex = [
rho2[0] / od.mag(rho2), rho2[1] / od.mag(rho2), rho2[2] / od.mag(rho2)
]
rho_hat_3_ex = [
rho3[0] / od.mag(rho3), rho3[1] / od.mag(rho3), rho3[2] / od.mag(rho3)
]
error_1x = (rho_hat1[0] - rho_hat_1_ex[0])**2 # error by component
error_1y = (rho_hat1[1] - rho_hat_1_ex[1])**2
error_1z = (rho_hat1[2] - rho_hat_1_ex[2])**2
error_2x = (rho_hat2[0] - rho_hat_2_ex[0])**2
error_2y = (rho_hat2[1] - rho_hat_2_ex[1])**2
error_2z = (rho_hat2[1] - rho_hat_2_ex[1])**2
error_3x = (rho_hat3[0] - rho_hat_3_ex[0])**2
error_3y = (rho_hat3[1] - rho_hat_3_ex[1])**2
error_3z = (rho_hat3[2] - rho_hat_3_ex[2])**2
error_1 = error_1x - error_1y - error_1z # cummulative error
error_2 = error_2x - error_2y - error_2z
error_3 = error_3x - error_3y - error_3z
print('Error for rho 1: ', error_1)
print('Error for rho 2: ', error_2)
print('Error for rho 3: ', error_3)
def __init__(self, x, y, rah, ram, ras, decd, decam, decas, m):
self.x = x
self.y = y
self.RAhr = rah
self.RAmin = ram
self.RAsec = ras
self.RA = odlib.HMStoDeg(rah, ram, ras)
self.DECdeg = decd
self.DECamin = decam
self.DECasec = decas
self.DEC = odlib.DMStoDeg(decd, decam, decas)
self.mag = m
def getRhoHat(rah, ram, ras=0, dech=0, decm=0, decs=0):
# First two elements will be RA (hr) and DEC (deg) if radecAsDecimal
if radecAsDecimal:
raRad = odlib.degreesToRadians(rah * 15)
decRad = odlib.degreesToRadians(ram)
else:
raRad = odlib.degreesToRadians(odlib.HMStoDeg(rah, ram, ras))
decRad = odlib.degreesToRadians(odlib.DMStoDeg(dech, decm, decs))
rhox = cos(raRad) * cos(decRad)
rhoy = sin(raRad) * cos(decRad)
rhoz = sin(decRad)
return np.array([rhox, rhoy, rhoz])
import numpy as np
import copy as cp
# defining input values!
RA = [[18, 41, 48.08], [18, 14, 30.53], [17, 54, 29.36]]
DEC = [[36, 15, 14.1], [36, 9, 46.0], [34, 29, 32.2]]
R = [[-0.2069177625542078, 0.9132792377095497, 0.3959074080096284],
[-0.3689266994628273, 0.8690904003976556, 0.3767540914983889],
[-0.5205074019556455, 0.8003914633545058, 0.3469760777959491]]
k = 0.01720209847
t1 = 2458303.5
t2 = 2458313.5
t3 = 2458323.5
for i in range(3):
RA[i] = od.HMStoDeg(RA[i]) * pi / 180
DEC[i] = od.DMStoDeg(DEC[i]) * pi / 180
rho_hat1 = [cos(RA[0]) * cos(DEC[0]),
sin(RA[0]) * cos(DEC[0]),
sin(DEC[0])] # calculating rho from RA and Dec
rho_hat2 = [cos(RA[1]) * cos(DEC[1]), sin(RA[1]) * cos(DEC[1]), sin(DEC[1])]
rho_hat3 = [cos(RA[2]) * cos(DEC[2]), sin(RA[2]) * cos(DEC[2]), sin(DEC[2])]
T0 = k * (t3 - t1)
T1 = k * (t1 - t2)
T3 = k * (t3 - t2)
a1 = T3 / T0
a2 = -1
a3 = -T1 / T0
a = [a1, a2, a3]