<gh_stars>0

# do not edit, generated by pymola

from __future__ import print_function, division
import sympy
import sympy.physics.mechanics as mech
from pymola.sympy_runtime import OdeModel
from sympy import sin, cos, tan


class Aircraft(OdeModel):

    def __init__(self):

        super(Aircraft, self).__init__()

        # states
        self.x = sympy.Matrix([])
        self.x0 = {
            }

        # variables
        self.v = sympy.Matrix([])

        # constants
        self.c = sympy.Matrix([])
        self.c0 = {
            }

        # parameters
        self.p = sympy.Matrix([])
        self.p0 = {
            }

        # inputs
        self.u = sympy.Matrix([])
        self.u0 = {
            }

        # outputs
        self.y = sympy.Matrix([])

        # equations
        self.eqs = [
            ,
            ]

        self.compute_fg()