import numpy as np
from cpsim import Simulator
from cpsim.controllers.PID import PID
# system dynamics
R = 10000
L = 0.5
C = 0.0001
A = [[0, 1 / C], [-1 / L, -R / L]]
B = [[0], [1 / L]]
C = [[1, 0]]
D = [[0]]
x_0 = np.array([0.0, 0.0])
# utils parameters
KP = 5
KI = 5
KD = 0
control_limit = {'lo': [-15], 'up': [15]}
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class Controller:
def __init__(self, dt):
self.dt = dt
self.pid = PID(KP, KI, KD, current_time=-dt)
self.pid.setWindup(100)
self.pid.setSampleTime(dt)
self.set_control_limit(control_limit['lo'], control_limit['up'])
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def update(self, ref: np.ndarray, feedback_value: np.ndarray, current_time) -> np.ndarray:
self.pid.set_reference(ref[0])
cin = self.pid.update(feedback_value[0], current_time)
return np.array([cin])
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def set_control_limit(self, control_lo, control_up):
self.control_lo = control_lo
self.control_up = control_up
self.pid.set_control_limit(self.control_lo[0], self.control_up[0])
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def clear(self):
self.pid.clear(current_time=-self.dt)
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class RlcCircuit(Simulator):
def __init__(self, name, dt, max_index, noise=None):
super().__init__('Aircraft Pitch ' + name, dt, max_index)
self.linear(A, B, C)
controller = Controller(dt)
settings = {
'init_state': x_0,
'feedback_type': 'output',
'controller': controller
}
if noise:
settings['noise'] = noise
self.sim_init(settings)
if __name__ == "__main__":
max_index = 500
dt = 0.02
ref = [np.array([2])] * 201 + [np.array([3])] * 200 + [np.array([2])] * 100
noise = {
'process': {
'type': 'white',
'param': {'C': np.eye(2) * 0.01}
}
}
rlc_circuit = RlcCircuit('test', dt, max_index, noise)
for i in range(0, max_index + 1):
assert rlc_circuit.cur_index == i
rlc_circuit.update_current_ref(ref[i])
# attack here
rlc_circuit.evolve()
# print results
import matplotlib.pyplot as plt
t_arr = np.linspace(0, 10, max_index + 1)
ref = [x[0] for x in rlc_circuit.refs[:max_index + 1]]
y_arr = [x[0] for x in rlc_circuit.outputs[:max_index + 1]]
plt.plot(t_arr, y_arr, t_arr, ref)
plt.show()