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Details for: "acrobot"

Name: acrobot (Key: 5CVFG)
Path: ackrep_data/system_models/acrobot_system View on GitHub
Type: system_model
Short Description: planar two-link robotic arm in the vertical plane with an actuator at the elbow, but no actuator at the shoulder
Created: 2022-09-14
Compatible Environment: default_conda_environment (Key: CDAMA)
Source Code [ / ] simulation.py
import numpy as np
import system_model
from scipy.integrate import solve_ivp

from ackrep_core import ResultContainer
from ackrep_core.system_model_management import save_plot_in_dir
import matplotlib.pyplot as plt
import os


# link to documentation with examples: https://ackrep-doc.readthedocs.io/en/latest/devdoc/contributing_data.html


def simulate():
    """
    simulate the system model with scipy.integrate.solve_ivp

    :return: result of solve_ivp, might contains input function
    """

    model = system_model.Model()

    rhs_symb = model.get_rhs_symbolic()
    print("Computational Equations:\n")
    for i, eq in enumerate(rhs_symb):
        print(f"dot_x{i+1} =", eq)

    xx0 = [0, 0, 0, 0]

    rhs = model.get_rhs_func()

    t_end = 10
    tt = np.linspace(0, t_end, 10000)
    simulation_data = solve_ivp(rhs, (0, t_end), xx0, t_eval=tt)

    save_plot(simulation_data)

    return simulation_data


def save_plot(simulation_data):
    """
    plot your data and save the plot

    :param simulation_data: simulation_data of system_model
    :return: None
    """
    # ---------start of edit section--------------------------------------
    fig1, axs = plt.subplots(nrows=4, ncols=1, figsize=(12.8, 9))

    # print in axes top left
    axs[0].plot(simulation_data.t, simulation_data.y[0])
    axs[0].set_ylabel("Angle 1 [rad]")  # y-label
    axs[0].grid()

    axs[1].plot(simulation_data.t, simulation_data.y[1])
    axs[1].set_ylabel("Angle 2 [rad]")  # y-label
    axs[1].grid()

    axs[2].plot(simulation_data.t, simulation_data.y[2])
    axs[2].set_ylabel("Angle velocity 1 [rad/s]")  # y-label
    axs[2].grid()

    axs[3].plot(simulation_data.t, simulation_data.y[3])
    axs[3].set_ylabel("Angle velocity 2 [rad/s]")  # y-label
    axs[3].set_xlabel("Time [s]")  # x-label
    axs[3].grid()

    # ---------end of edit section----------------------------------------

    plt.tight_layout()

    save_plot_in_dir()


def evaluate_simulation(simulation_data):
    """
    assert that the simulation results are as expected

    :param simulation_data: simulation_data of system_model
    :return:
    """
    # ---------start of edit section--------------------------------------
    # fill in final states of simulation to check your model
    # simulation_data.y[i][-1]
    expected_final_state = [-0.14133623, 0.51763847, -0.0637786, 0.244969662]

    # ---------end of edit section----------------------------------------

    rc = ResultContainer(score=1.0)
    simulated_final_state = simulation_data.y[:, -1]
    rc.final_state_errors = [
        simulated_final_state[i] - expected_final_state[i] for i in np.arange(0, len(simulated_final_state))
    ]
    rc.success = np.allclose(expected_final_state, simulated_final_state, rtol=0, atol=1e-2)

    return rc
system_model.py
import sympy as sp
import symbtools as st
import importlib
import sys, os
import symbtools.modeltools as mt

# from ipydex import IPS, activate_ips_on_exception

from ackrep_core.system_model_management import GenericModel, import_parameters

# Import parameter_file
params = import_parameters()


# link to documentation with examples: https://ackrep-doc.readthedocs.io/en/latest/devdoc/contributing_data.html


class Model(GenericModel):
    def initialize(self):
        """
        this function is called by the constructor of GenericModel

        :return: None
        """

        # ---------start of edit section--------------------------------------
        # Define number of inputs -- MODEL DEPENDENT
        self.u_dim = 1

        # Set "sys_dim" to constant value, if system dimension is constant
        self.sys_dim = 4

        # ---------end of edit section----------------------------------------

        # check existence of params file
        self.has_params = True
        self.params = params

    # ----------- SET DEFAULT INPUT FUNCTION ---------- #
    # --------------- Only for non-autonomous Systems
    def uu_default_func(self):
        """
        define input function
        :return:(function with 2 args - t, xx_nv) default input function
        """
        # ---------start of edit section--------------------------------------
        def uu_rhs(t, xx_nv):
            """
            sequence of numerical input values

            :param t:(scalar or vector) time
            :param xx_nv:(vector or array of vectors) numeric state vector
            :return:(list) numeric inputs
            """

            if t < 5:
                u1 = 0.5
            else:
                u1 = 0

            return [u1]

        # ---------end of edit section----------------------------------------

        return uu_rhs

    def get_rhs_symbolic(self):
        """
        define symbolic rhs function

        :return: matrix of symbolic rhs-functions
        """

        np = 1
        nq = 1
        n = np + nq

        x1, x2, x3, x4 = self.xx_symb
        ttheta = st.row_stack(x1, x2)

        xdot1, xdot2 = sp.symbols("xdot1, xdot2")

        s1, s2, m1, m2, J1, J2, l1, g = self.pp_symb

        u1 = self.uu_symb[0]

        mt.Rz(x2)

        # unuit vectors
        ex = sp.Matrix([1, 0])
        ey = sp.Matrix([0, 1])

        # coordinates of the centers of gravity and joints
        S1 = mt.Rz(x1) * (-ey) * s1
        G1 = mt.Rz(x1) * (-ey) * l1  # "elbow joint"
        S2 = G1 + mt.Rz(x2 + x1) * (-ey) * s2

        # time derivatives of the center of gravity coordinates
        Sd1, Sd2 = st.col_split(st.time_deriv(st.col_stack(S1, S2), ttheta))

        # kinetic energy
        T_rot = (J1 * x3**2) / 2 + (J2 * (x4 + x3) ** 2) / 2
        T_trans = (m1 * Sd1.T * Sd1 + m2 * Sd2.T * Sd2) / 2

        T = T_rot + T_trans[0]

        # potential energy
        V = m1 * g * S1[1] + m2 * g * S2[1]

        external_forces = [0, u1]
        assert not any(external_forces[:np])
        mod = mt.generate_symbolic_model(T, V, ttheta, external_forces)

        mod.calc_state_eq(simplify=False)

        state_eq = mod.state_eq.subs([(xdot1, x3), (xdot2, x4)])

        return state_eq
parameters.py
import sys
import os
import numpy as np
import sympy as sp

import tabulate as tab


# link to documentation with examples: https://ackrep-doc.readthedocs.io/en/latest/devdoc/contributing_data.html


# set model name
model_name = ".."


# ---------- create symbolic parameters
pp_symb = [s1, s2, m1, m2, J1, J2, l1, g] = sp.symbols("s1, s2, m1, m2, J1, J2, l1, g", real=True)


# ---------- create symbolic parameter functions
# parameter values can be constant/fixed values OR set in relation to other parameters (for example: a = 2*b)
s1_sf = 0.25
s2_sf = 0.25
m1_sf = 1
m2_sf = 1
J1_sf = 1 / 150
J2_sf = 1 / 75
l1_sf = 0.5
g_sf = 9.81


# list of symbolic parameter functions
# tailing "_sf" stands for "symbolic parameter function"
pp_sf = [s1_sf, s2_sf, m1_sf, m2_sf, J1_sf, J2_sf, l1_sf, g_sf]


#  ---------- list for substitution
# -- entries are tuples like: (independent symbolic parameter, numerical value)
pp_subs_list = []


# OPTONAL: Dictionary which defines how certain variables shall be written
# in the table - key: Symbolic Variable, Value: LaTeX Representation/Code
# useful for example for complex variables: {Z: r"\underline{Z}"}
latex_names = {}


# ---------- Define LaTeX table

# Define table header
# DON'T CHANGE FOLLOWING ENTRIES: "Symbol", "Value"
tabular_header = ["Parameter Name", "Symbol", "Value", "Unit"]

# Define column text alignments
col_alignment = ["left", "center", "left", "center"]


# Define Entries of all columns before the Symbol-Column
# --- Entries need to be latex code
col_1 = [
    "center of gravity distance of first bar",
    "center of gravity distance of second bar",
    "mass of first bar",
    "mass of second bar",
    "moment of inertia of first bar",
    "moment of inertia of second bar",
    "length of first bar",
    "acceleration due to gravity",
]

# contains all lists of the columns before the "Symbol" Column
# --- Empty list, if there are no columns before the "Symbol" Column
start_columns_list = [col_1]


# Define Entries of the columns after the Value-Column
# --- Entries need to be latex code
col_4 = ["m", "m", "kg", "kg", r"$kg \cdot m^2$", r"$kg \cdot m^2$", "m", r"$\frac{m}{s^2}$"]

# contains all lists of columns after the FIX ENTRIES
# --- Empty list, if there are no columns after the "Value" column
end_columns_list = [col_4]

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