Interesting transfer combinations
# initial and final elements
oe0 = np .array ([1.0 , 1e-2 , 1e-2 , 1e-3 , 1e-3 , 1e-3 ])
oeT = np .array ([3.6 , 0.6 , 1.2 , 2.8 , 0.0 ])
woe = [1.0 , 1.0 , 1.0 , 1.0 , 1.0 ]
# spacecraft parameters
mass0 = 1.0
tmax = 5e-3
mdot = 1e-4
tf_max = 2500.0
t_step = 0.5
# initial and final elements
oe0 = np .array ([1.0 , 1e-2 , 1e-4 , 1e-4 , 1e-4 , 1e-4 ])
oeT = np .array ([1.1 , 0.05 , 0.01 , 0.0 , 0.0 ])
woe = [1 ,1 ,0 ,0 ,0 ]
# spacecraft parameters
mass0 = 1.0
tmax = 1e-3
mdot = 1e-4
tf_max = 100.0
t_step = 0.1
# initial and final elements: [a,e,i,RAAN,omega,ta]
oe0 = np .array ([1.0 , 1e-2 , 1e-2 , 1e-2 , 1e-2 , 1e-3 ])
oeT = np .array ([1.3 , 0.1 , np .pi / 2.4 , 0.0 , 0.0 ])
woe = [1.0 , 1.0 , 1.0 , 1.0 , 1.0 ]
# spacecraft parameters
mass0 = 1.0
tmax = 1e-3
mdot = 1e-4
tf_max = 3000.0
t_step = 1.0
prob = pyqlaw .QLaw (
integrator = "rk4" ,
elements_type = "mee_with_a" ,
disable_tqdm = False ,
)
# initial and final elements: [a,e,i,RAAN,omega,ta]
oe0 = pyqlaw .kep2mee_with_a (np .array ([1.0 , 1e-4 , 0.0 , 1e-2 , 1e-2 , 1e-3 ]))
oeT = pyqlaw .kep2mee_with_a (np .array ([1.8 , 0.4 , np .pi / 4 , 1e-2 , 1e-2 , 1e-3 ]))
# initial and final elements: [a,e,i,RAAN,omega,ta]
#oe0_kep = np.array([1.5, 0.2, 0.3, 1e-2, 1e-2, 1e-3])
#oeT_kep = np.array([2.2, 0.3, 1.1, 0.3, 0.0, 0.0])
#oe0 = pyqlaw.kep2mee_with_a(oe0_kep)
#oeT = pyqlaw.kep2mee_with_a(oeT_kep)
woe = [1.0 , 1.0 , 1.0 , 1.0 , 1.0 ]
# spacecraft parameters
mass0 = 1.0
tmax = 1e-3
mdot = 1e-4
tf_max = 3000.0
t_step = 1.0