This commit is contained in:
Yael-II
2025-01-22 00:00:33 +01:00
parent 969fdb0b44
commit 61a5a5e50f
33 changed files with 276 additions and 111 deletions

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@@ -34,54 +34,65 @@ along with this program. If not, see https://www.gnu.org/licenses/.
"""
import numpy as np
def euler(x0, y0, h, n, func): # FIXME cannot be used with vectors
"""DEPRECIATED - DO NOT USE
Euler method adapted for state vector [[x, y], [u, v]]
:param x0: initial time value
:param y0: initial state vector [[x, y], [u, v]]
:param h: step size (time step)
:param n: number of steps
:param func: RHS of differential equation
:returns: x array, solution array
def euler(t0: float,
W0: np.ndarray,
h: float,
n: int,
func):
"""Euler method adapted for state vector [[x, y], [u, v]]
@ params
- t0: initial time value
- W0: initial state vector [[x, y], [u, v]]
- h: step size (time step)
- n: number of steps
- func: RHS of differential equation
@returns:
- t, W: time and state (solution) arrays
"""
x_values = np.zeros(n)
y_values = np.zeros((n, 2, 2)) # to accommodate the state vector
time = np.zeros(n)
W = np.zeros((n,) + np.shape(W0))
t = t0
w = W0
for i in range(n):
dydt = func(x0, y0)
y0 = y0 + h * dydt
x0 = x0 + h
k1 = func(t, w)
w = w + h*k1
t = t + h
x_values[i] = x0
y_values[i, :, :] = y0
time[i] = t
W[i] = w
return time, W
return x_values, y_values
# Updated RK2 integrator
def rk2(x0, y0, h, n, func): # FIXME cannot be used with vectors
""" DEPRECIATED - DO NOT USE
RK2 method adapted for state vector [[x, y], [u, v]]
:param x0: initial time value
:param y0: initial state vector [[x, y], [u, v]]
:param h: step size (time step)
:param n: number of steps
:param func: RHS of differential equation
:returns: x array, solution array
def rk2(t0: float,
W0: np.ndarray,
h: float,
n: int,
func):
"""RK2 method adapted for state vector [[x, y], [u, v]]
@ params
- t0: initial time value
- W0: initial state vector [[x, y], [u, v]]
- h: step size (time step)
- n: number of steps
- func: RHS of differential equation
@returns:
- t, W: time and state (solution) arrays
"""
x_values = np.zeros(n)
y_values = np.zeros((n, 2, 2)) # to accommodate the state vector
time = np.zeros(n)
W = np.zeros((n,) + np.shape(W0))
t = t0
w = W0
for i in range(n):
k1 = func(x0, y0)
k2 = func(x0 + h / 2., y0 + h / 2. * k1)
k1 = func(t, w)
k2 = func(t + h/2, w + h/2*k1)
y0 = y0 + h * (k1 / 2. + k2 / 2.)
x0 = x0 + h
w = w + h*k2
t = t + h
x_values[i] = x0
y_values[i, :, :] = y0
return x_values, y_values
time[i] = t
W[i] = w
return time, W
def rk4(t0: float,
W0: np.ndarray,
@@ -90,13 +101,13 @@ def rk4(t0: float,
func):
"""RK4 method adapted for state vector [[x, y], [u, v]]
@ params
- x0: initial time value
- y0: initial state vector [[x, y], [u, v]]
- t0: initial time
- W0: initial state vector [[x, y], [u, v]]
- h: step size (time step)
- n: number of steps
- func: RHS of differential equation
@returns:
- t, W: time and state (solution) arrays,
- t, W: time and state (solution) arrays
"""
time = np.zeros(n)
W = np.zeros((n,) + np.shape(W0))
@@ -105,19 +116,50 @@ def rk4(t0: float,
w = W0
for i in range(n):
k1 = func(t, w)
k2 = func(t + h / 2., w + h / 2. * k1)
k3 = func(t + h / 2., w + h / 2. * k2)
k4 = func(t + h, w + h * k3)
k2 = func(t + h/2, w + h/2*k1)
k3 = func(t + h/2, w + h/2*k2)
k4 = func(t + h, w + h*k3)
w = w + h * (k1 / 6. + k2 / 3. + k3 / 3. + k4 / 6.)
w = w + h*(k1/6 + k2/3 + k3/3 + k4/6)
t = t + h
time[i] = t
W[i] = w
return time, W
return t, W
def integrator_type(t0, W0, h, n, func, integrator):
return integrator(t0, W0, h, n, func)
def kepler_analytical(t0: float,
W0: np.ndarray,
h: float,
n: int):
"""Computes the evolution from the Kepler potential derivative
@ params
- t0: initial time value
- W0: initial state vector [[x, y], [u, v]]
- h: step size (time step)
- n: number of steps
@returns:
- t, W: time and state (solution) arrays
"""
X0 = W0[0 ,0]
Y0 = W0[0, 1]
U0 = W0[1, 0]
V0 = W0[1, 1]
def integrator_type(x0, y0, h, n, func, int_type):
"""DEPRECIATED - DO NOT USE"""
return int_type(x0, y0, h, n, func)
time = np.arange(t0, t0 + n*h, h)
W = np.zeros((n,) + np.shape(W0))
R0 = np.sqrt(X0**2 + Y0**2)
Omega0 = np.sqrt(U0**2 + V0**2)/R0
X = R0 * np.cos(Omega0 * time)
Y = R0 * np.sin(Omega0 * time)
U = -R0 * Omega0 * np.sin(Omega0 * time)
V = R0 * Omega0 * np.cos(Omega0 * time)
W = np.array([[X, Y], [U, V]])
W = np.swapaxes(W, 0, 2)
W = np.swapaxes(W, 1, 2)
return time, W