def print_iirv_points(st, table):
for i in range(0, len(table)):
print("GIIRV MANY\r\r\n")
tt = table[i][0].timetuple()
string = "1111800001%3.3d%3.3d%2.2d%2.2d%2.2d%3.3d" % (i+1, tt.tm_yday, tt.tm_hour, tt.tm_min, tt.tm_sec, int(table[i][0].microsecond/1000.0))
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
gmst_radians = astronomy.gmst(table[i][0])
#print("gmst_radians=%s, degrees=%s" % (gmst_radians, gmst_radians * 180.0/3.1415927))
(x, y, z) = (table[i][1][0], table[i][1][1], table[i][1][2])
r = math.sqrt(x*x + y*y)
theta = math.atan2(y, x)
x = r*math.cos(-1.0*gmst_radians+theta)
y = r*math.sin(-1.0*gmst_radians+theta)
string = "% 013.0f% 013.0f% 013.0f" % (x*1000.0, y*1000.0, z*1000.0)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
(x, y, z) = (table[i][2][0], table[i][2][1], table[i][2][2])
r = math.sqrt(x*x + y*y)
theta = math.atan2(y, x)
x = r*math.cos(-1.0*gmst_radians+theta)
y = r*math.sin(-1.0*gmst_radians+theta)
string = "% 013.0f% 013.0f% 013.0f" % (x*1000000.0, y*1000000.0, z*1000000.0)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
mass = 4544100
cross = 99999
drag = 200
solar = 1500000
string = "%08.0f%05.0f%04.0f% 08.0f" % (mass, cross, drag, solar)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
print("ITERM GAQD\r\r\n")
def print_ephemeris_point(st, point, inertial=True):
#print point
if (inertial):
coords = "ECI"
else:
coords = "ECEF"
print("===== %s =====" % coords)
if (not inertial):
gmst_radians = astronomy.gmst(point[0])
print("Date/Time: %s Satellite Number: %s" % \
(point[0], st.get_satellite_number()))
(x, y, z) = (point[1][0], point[1][1], point[1][2])
if (not inertial):
r = math.sqrt(x * x + y * y)
theta = math.atan2(y, x)
x = r * math.cos(-1.0 * gmst_radians + theta)
y = r * math.sin(-1.0 * gmst_radians + theta)
print("Position (km, x/y/z %s): %s/%s/%s" % (coords, x, y, z))
(x, y, z) = (point[2][0], point[2][1], point[2][2])
if (not inertial):
r = math.sqrt(x * x + y * y)
theta = math.atan2(y, x)
x = r * math.cos(-1.0 * gmst_radians + theta)
y = r * math.sin(-1.0 * gmst_radians + theta)
print("Velocity (km/s, x/y/z %s): %s/%s/%s" % (coords, x, y, z))
def print_iirv_point(st, point):
print("GIIRV MANY\r\r\n")
tt = point[0].timetuple()
string = "1211800001000%3.3d%2.2d%2.2d%2.2d%3.3d" % (tt.tm_yday, tt.tm_hour, tt.tm_min, tt.tm_sec, int(point[0].microsecond/1000.0))
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
gmst_radians = astronomy.gmst(point[0])
#print("gmst_radians=%s, degrees=%s" % (gmst_radians, gmst_radians * 180.0/3.1415927))
(x, y, z) = (point[1][0], point[1][1], point[1][2])
r = math.sqrt(x*x + y*y)
theta = math.atan2(y, x)
x = r*math.cos(-1.0*gmst_radians+theta)
y = r*math.sin(-1.0*gmst_radians+theta)
string = "% 013.0f% 013.0f% 013.0f" % (x*1000.0, y*1000.0, z*1000.0)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
(x, y, z) = (point[2][0], point[2][1], point[2][2])
r = math.sqrt(x*x + y*y)
theta = math.atan2(y, x)
x = r*math.cos(-1.0*gmst_radians+theta)
y = r*math.sin(-1.0*gmst_radians+theta)
string = "% 013.0f% 013.0f% 013.0f" % (x*1000000.0, y*1000000.0, z*1000000.0)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
mass = 4475570
cross = 99999
drag = 207
solar = 0
string = "%08.0f%05.0f%04.0f% 08.0f" % (mass, cross, drag, solar)
csum = checksum(string)
print("%s%3.3d\r\r\n" % (string, csum))
print("ITERM GAQD\r\r\n")
def print_ephemeris_table(st, table, inertial=True):
if (inertial):
coords = "ECI"
else:
coords = "ECEF"
print "===== %s =====" % coords
print "Time, X,Y,Z in km, VX,VY,VZ in km/s (%s Coordinates)" % coords
for i in range(0, len(table)):
( x, y, z) = (table[i][1][0], table[i][1][1], table[i][1][2])
(vx, vy, vz) = (table[i][2][0], table[i][2][1], table[i][2][2])
if (not inertial):
gmst_radians = astronomy.gmst(table[i][0])
r = math.sqrt(x*x + y*y)
x = r*math.cos(-1.0*gmst_radians)
y = r*math.sin(-1.0*gmst_radians)
vr = math.sqrt(vx*vx + vy*vy)
vx = r*math.cos(-1.0*gmst_radians)
vy = r*math.sin(-1.0*gmst_radians)
print "%s, %16.8f,%16.8f,%16.8f, %13.9f,%13.9f,%13.9f" % \
(table[i][0], x, y, z, vx, vy, vz)
