Source code for cpsim.models.linear.rlc_circuit

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]}


[docs] 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'])
[docs] 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])
[docs] 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])
[docs] def clear(self): self.pid.clear(current_time=-self.dt)
[docs] 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()