def extract_semi_major(en):
shape = (ens.nbod-1,ens.nsys)
value = numpy.empty(shape)
for sysid, sys in enumerate(en):
star = sys[0]
center = (star.pos,star.vel,star.mass)
for bodid in range(1,en.nbod):
bod = sys[bodid]
planet = (bod.pos,bod.vel,bod.mass)
orbital_elements = swarmng.keplerian_for_cartesian(planet,center)
value[bodid-1,sysid] = orbital_elements.a
return value
# * planet number 0 to nbod-1
# * orbital element number : 0 to 5
# * system id
#
import numpy
shape = (ens.nbod-1, 6, ens.nsys)
value = numpy.empty(shape)
for sysid, sys in enumerate(ens):
star = sys[0]
center = (star.pos,star.vel,star.mass)
for bodid in range(1,ens.nbod):
bod = sys[bodid]
planet = (bod.pos,bod.vel,bod.mass)
orbital_elements = swarmng.keplerian_for_cartesian(planet,center)
value[bodid-1, :,sysid] = orbital_elements
# @section pr Write the information to standard output
# Now iterate through the 3-dimensional array
# and calculate the average and standard deviation
# of each orbital element value for each body, then
# print it to the output.
#
print("Body number, Semi-major axis, Eccentricity, Inclination, Longtitude of the ascending node, Argument of periapsis, Mean anomaly")
for bodid in range(1,ens.nbod):
orbital_elements = [0,0,0,0,0]
o = "{0}".format(bodid)
for i in range(0,6):
o += ", {0}±{1}".format(numpy.average(value[bodid-1,i,:]),numpy.std(value[bodid-1,i,:]))
print(o)
