model checkpoint

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2026-06-16 22:42:49 -05:00
parent c7432320fe
commit dd9bd5511e

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@@ -100,3 +100,69 @@ import math
# eq 23: temporal boundary conditions # eq 23: temporal boundary conditions
# y(-1, n) = -y(1, n) # y(-1, n) = -y(1, n)
# y(N + 1, n) = -y(N - 1, n) # y(N + 1, n) = -y(N - 1, n)
# string parameters
E = 1 # youngs modulus
mu = 1 # linear mass density
kappa = 1 # radius of gyration
L = 1 # string length
M_S = mu*L # string mass
S = 1 # string cross sectional area
T = 1 # string tension
c = math.sqrt(T/mu) # transverse wave velocity
stiffness = 1 # string stiffness parameter
sigma = 1 # decay rate
tau = 1/sigma # decay time
omega = 1 # angular frequency
# hammer parameters
M_H = 1 # hammer mass
HSMR = M_H/M_S # hammer-mass string ratio
V_H_0 = 1 # initial hammer velocity at t=0
x_0 = 1 # distance of hammer from agraffe
alpha = x_0 / L # relative hammer striking position
# simulation parameters
f1 = 440 # fundamental frequency
f_e = 44100 # sampling frequency
N = 100 # number of string segments
delta_t = 1/f_e # time step
delta_x = L/N # spatial step
H = f_e * 10 # length of simulation in time
# empirical constants
b_1 = 1 # some constant
b_3 = 1 # some constant
K = 1 # hammer stiffness
p = 1 # stiffness nonlinear exponent
# derived components
D = 1 + b_1*delta_t + 2*b_3/delta_t
r = c*delta_t/delta_x
a_1 = (2 - 2*r**2 + b_1/delta_t - 6*stiffness*N**2*r**2)/D
a_2 = (-1 + b_1*delta_t + 2*b_3/delta_t)/D
a_3 = (r**2*(1 + 4*stiffness*N**2))/D
a_4 = (b_3/delta_t - stiffness*N**2*r**2)/D
a_5 = (-b_3/delta_t)/D
x = [0] * N # current string position
last_x1 = [0] * N # string position from last timestep
last_x2 = [0] * N # string position from two timesteps ago
x_next = [0] * N # buffer for next string position
x_out = np.zeros(H) # taking this as the sound output at some artibraty point along the string
t = np.arange(0, H/f_e, delta_t)
for n in range(H): # time
for i in range(N): # space
x_out[n] = math.sin(n/10000)
# plotting
plt.plot(t, x_out)
plt.title("Step Response")
plt.xlabel("t")
plt.ylabel("y")
plt.grid()
plt.show()