class ShaftVT(VariableTree):
mass = Float(desc='blade mass')
I_x = Float(desc='first area moment of inertia')
I_y = Float(desc='Second area moment of inertia')
CM = Array(np.zeros(3), desc='')
length = Float()
class NacelleVT(VariableTree):
mass = Float(desc='blade mass')
I_x = Float(desc='first area moment of inertia')
I_y = Float(desc='Second area moment of inertia')
CM = Array(np.zeros(3), desc='')
diameter = Float()
class HubVT(VariableTree):
diameter = Float(desc='blade length')
mass = Float(desc='blade mass')
I_x = Float(desc='first area moment of inertia')
I_y = Float(desc='Second area moment of inertia')
CM = Array(np.zeros(3), desc='')
class HAWC2ConstraintFix23(VariableTree):
con_type = Str()
mbdy = Str(desc='Main_body name to which the next main_body is fixed')
dof = Array(np.zeros(3),
desc='Direction in global coo that is fixed in rotation'
'0: free, 1: fixed')
class HAWC2AirfoilDataset(VariableTree):
"""A set of airfoil polars for a range of relative thicknesses"""
np = Int(desc='number of airfoil polars in set')
rthick = Array(
desc='Array of relative thicknesses linked to the airfoil polars')
polars = List(desc='List of polars')
class ConfigGravity(AtlasConfiguration):
""" Atlas configuration for gravity case """
Omega_opt = Float(iotype='in', desc='rotor angular velocity')
OmegaRatio = Float(iotype='in')
Cl_opt = Array(iotype='in')
H_opt = Float(iotype='in', desc='height of aircraft')
TWire_opt = Float(iotype='in', desc='')
def execute(self):
super(ConfigGravity, self).execute()
# use optimizer provided values
self.Omega = (self.Omega_opt**3 * self.OmegaRatio)**(1. / 3.)
self.Cl = self.Cl_opt
self.h = self.H_opt + self.zWire
self.TWire = [self.TWire_opt]
self.flags.Load = 1 # gravity and wire forces only
# FIXME: the following two flags are ignored
self.flags.FreeWake = 0 # momentum theory
self.flags.AeroStr = 0 # assume flat wing (no deformation)
def __init__(self, n, rawG=None):
super(Comm_GainPattern, self).__init__()
self.n = n
if rawG is None:
fpath = os.path.dirname(os.path.realpath(__file__))
rawGdata = np.genfromtxt(fpath + '/data/Comm/Gain.txt')
rawG = (10**(rawGdata / 10.0)).reshape((361, 361), order='F')
# Inputs
self.add(
'azimuthGS',
Array(
np.zeros(n),
iotype='in',
shape=(n, ),
units="rad",
desc=
"Azimuth angle from satellite to ground station in Earth-fixed frame over time"
))
self.add(
'elevationGS',
Array(
np.zeros(n),
iotype='in',
shape=(self.n, ),
units="rad",
desc=
"Elevation angle from satellite to ground station in Earth-fixed frame over time"
))
# Outputs
self.add(
'gain',
Array(np.zeros(n),
iotype='out',
shape=(n, ),
units="unitless",
desc="Transmitter gain over time"))
pi = np.pi
az = np.linspace(0, 2 * pi, 361)
el = np.linspace(0, 2 * pi, 361)
self.MBI = MBI.MBI(rawG, [az, el], [15, 15], [4, 4])
self.x = np.zeros((self.n, 2), order='F')
class RotorLoadsArrayVT(VariableTree):
wsp = Array(units='m/s', desc='Wind speeds')
rpm = Array(units='rpm', desc='Rotor speed')
pitch = Array(units='deg', desc='Pitch angle')
T = Array([0.], units='N', desc='thrust')
Q = Array([0.], units='N*m', desc='torque')
P = Array([0.], units='W', desc='power')
CT = Array([0.], units=None, desc='thrust coefficient')
CQ = Array([0.], units=None, desc='torque coefficient')
CP = Array([0.], units=None, desc='power coefficient')
def __init__(self, pitch_array):
super(FASTInitialConditions, self).__init__()
self.add(
'Pitch',
Array(pitch_array,
dtype=float,
desc="Pitch points used for blade pitch interp [degrees]",
iotype='in'))
class HAWC2Constraint(VariableTree):
con_name = Str()
con_type = Enum('free',
('fixed', 'fixed_to_body', 'free', 'prescribed_angle'),
desc='Constraint type')
body1 = Str(desc='Main body name to which the body is attached')
DOF = Array(np.zeros(6), desc='Degrees of freedom')
def set_outputs(self, entries):
for i, c in enumerate(entries):
self.add(
'out_%i' % (i + 1),
Array(desc='Output %i of type2_dll %s: %s' %
((i + 1), self.parent.name, c.name + ' ' +
' '.join([str(val) for val in _makelist(c.val)]))))
class HAWC2SVar(VariableTree):
ground_fixed = VarTree(HAWC2SBody())
rotating_axissym = VarTree(HAWC2SBody())
rotating_threebladed = VarTree(HAWC2SBody())
second_order_actuator = VarTree(SecondOrderActuator())
commands = List()
options = VarTree(HAWC2SCommandsOpt())
operational_data_filename = Str()
ch_list_in = VarTree(HAWC2OutputListVT())
ch_list_out = VarTree(HAWC2OutputListVT())
wsp_curve = Array(desc='Pitch curve from operational data file')
pitch_curve = Array(desc='Pitch curve from operational data file')
rpm_curve = Array(desc='RPM curve from operational data file')
wsp_cases = List()
cases = List(desc='List of input dictionaries with wsp, rpm and pitch')
class GenericInflowGenerator(Component):
"""
Framework for an inflow model
"""
wind_speed = Float(0.0,
iotype='in',
units='m/s',
desc='the reference wind speed')
ws_positions = Array(
[],
iotype='in',
desc=
'the positions of the wind speeds in the global frame of reference [n,3] (x,y,z)'
)
ws_array = Array([],
iotype='out',
desc='an array of wind speed to find wind speed')
class Dummy(Component):
x = Array([[-1, 1],[-2, 2]], iotype='in', shape=(2,2))
xlist = List([1,2], iotype='in')
xdict = Dict({'a' : 'b'}, iotype='in')
def execute(self):
self.y = self.x
def __init__(self, datasize=0):
super(windSpeedToCPCT, self).__init__()
self.add(
'wind_speed',
Array(np.zeros(datasize),
iotype='in',
units='m/s',
desc='range of wind speeds'))
self.add(
'CP',
Array(np.zeros(datasize), iotype='out', desc='power coefficients'))
self.add(
'CT',
Array(np.zeros(datasize), iotype='out',
desc='thrust coefficients'))
class Strain(VariableTree):
top = Array(desc='')
bottom = Array(desc='')
back = Array(desc='')
front = Array(desc='')
bending_x = Array(desc='')
bending_z = Array(desc='')
axial_y = Array(desc='')
torsion_y = Array(desc='')
def __init__(self, n_times):
super(BatterySOC, self).__init__()
# Inputs
self.add(
'iSOC',
Array([0.0],
shape=(1, ),
dtype=np.float,
iotype="in",
units="unitless",
desc="Initial state of charge"))
self.add(
'P_bat',
Array(np.zeros((n_times, )),
shape=(n_times, ),
dtype=np.float,
units="W",
iotype="in",
desc="Battery power over time"))
self.add(
'temperature',
Array(np.zeros((5, n_times)),
shape=(5, n_times),
dtype=np.float,
units="degK",
iotype="in",
desc="Battery temperature over time"))
# Outputs
self.add(
'SOC',
Array(np.zeros((1, n_times)),
shape=(1, n_times),
dtype=np.float,
iotype="out",
units="unitless",
desc="Battery state of charge over time"))
self.state_var = "SOC"
self.init_state_var = "iSOC"
self.external_vars = ["P_bat", "temperature"]
def __init__(self, n=2):
super(Attitude_Torque, self).__init__()
self.n = n
# Inputs
self.add(
'w_B',
Array(np.zeros((3, n)),
iotype='in',
shape=(3, n),
units="1/s",
desc="Angular velocity in body-fixed frame over time"))
self.add(
'wdot_B',
Array(np.zeros((3, n)),
iotype='in',
shape=(3, n),
units="1/s**2",
desc="Time derivative of w_B over time"))
# Outputs
self.add(
'T_tot',
Array(np.zeros((3, n)),
iotype='out',
shape=(3, n),
units="N*m",
desc="Total reaction wheel torque over time"))
self.dT_dwdot = np.zeros((n, 3, 3))
self.dwx_dw = np.zeros((3, 3, 3))
self.dwx_dw[0, :, 0] = (0., 0., 0.)
self.dwx_dw[1, :, 0] = (0., 0., -1.)
self.dwx_dw[2, :, 0] = (0., 1., 0.)
self.dwx_dw[0, :, 1] = (0., 0., 1.)
self.dwx_dw[1, :, 1] = (0., 0., 0.)
self.dwx_dw[2, :, 1] = (-1., 0, 0.)
self.dwx_dw[0, :, 2] = (0., -1., 0)
self.dwx_dw[1, :, 2] = (1., 0., 0.)
self.dwx_dw[2, :, 2] = (0., 0., 0.)
def __init__(self, n):
super(Comm_BitRate, self).__init__()
self.n = n
# Inputs
self.add(
'P_comm',
Array(np.zeros(self.n),
iotype='in',
shape=(self.n, ),
units="W",
desc="Communication power over time"))
self.add(
'gain',
Array(np.zeros(self.n),
iotype='in',
shape=(self.n, ),
units="unitless",
desc="Transmitter gain over time"))
self.add(
'GSdist',
Array(np.zeros(self.n),
iotype='in',
shape=(self.n, ),
units="km",
desc="Distance from ground station to satellite over time"))
self.add(
'CommLOS',
Array(np.zeros(self.n),
iotype='in',
shape=(self.n, ),
units="unitless",
desc="Satellite to ground station line of sight over time"))
# Outputs
self.add(
'Dr',
Array(np.zeros(self.n),
iotype='out',
shape=(self.n, ),
units="Gibyte/s",
desc="Download rate over time"))
def __init__(self,prob_size=1):
super(Discipline,self).__init__()
self.add_trait("z",Array(zeros((prob_size,1)),iotype="in",
desc="global varaibles",
shape=(prob_size,1)))
self.add_trait("C_z",Array(ones((prob_size,prob_size)), iotype="in",
desc="global variable constants",
shape=(prob_size,prob_size)))
self.add_trait("x",Array(zeros((prob_size,1)), iotype="in",
desc="local variables",
shape=(prob_size,1)))
self.add_trait("C_x",Array(ones((prob_size,prob_size)), iotype="in",
desc="local variable constants",
shape=(prob_size,prob_size)))
#have to have the same number of coupling inputs as discipline outputs
self.add_trait("y_out",Array(zeros((prob_size,1)),iotype="out",
desc="discipline output varaibles",
shape=(prob_size,1)))
self.add_trait("y_in",Array(zeros((prob_size,1)), iotype="in",
desc="input coupling variables",
shape=(prob_size,1)))
self.add_trait("C_y",Array(identity(prob_size), iotype="in",
desc="local variable constants",
shape=(prob_size,prob_size)))
def __init__(self, n=2):
super(Power_Total, self).__init__()
self.n = n
self.add(
'P_sol',
Array(np.zeros((n, ), order='F'),
size=(n, ),
dtype=np.float,
units='W',
desc='Solar panels power over time',
iotype="in"))
self.add(
'P_comm',
Array(np.zeros((n, ), order='F'),
size=(n, ),
dtype=np.float,
units='W',
desc='Communication power over time',
iotype="in"))
self.add(
'P_RW',
Array(
np.zeros((
3,
n,
), order='F'),
size=(
3,
n,
),
dtype=np.float,
units='W',
desc='Power used by reaction wheel over time', # qqq ?
iotype="in"))
self.add(
'P_bat',
Array(np.zeros((n, ), order='F'),
size=(n, ),
dtype=np.float,
units='W',
desc='Battery power over time',
iotype="out"))
class AxodComp(Component):
""" OpenMDAO component wrapper for AXOD. """
input_filename = Str(iotype='in')
results = []
hpower = Float(iotype='out')
# 'float32' here could be just 'float', but AXOD is single-precision
# so it just takes more space. Not an issue with such small arrays,
# but for larger data it may be important.
tott = Array(_ZEROS48,dtype=float32, shape=(48,), iotype='out')
totp = Array(_ZEROS48,dtype=float32, shape=(48,), iotype='out')
mflow = Array(_ZEROS48,dtype=float32, shape=(48,), iotype='out')
effs = Array(_ZEROS48,dtype=float32, shape=(48,), iotype='out')
effr = Array(_ZEROS48,dtype=float32, shape=(48,), iotype='out')
# tott = Array(dtype=numpy_float32, shape=(48,), iotype='out')
# otp = Array(dtype=numpy_float32, shape=(48,), iotype='out')
# mflow = Array(dtype=numpy_float32, shape=(48,), iotype='out')
# effs = Array(dtype=numpy_float32, shape=(48,), iotype='out')
# effr = Array(dtype=numpy_float32, shape=(48,), iotype='out')
def __init__(self, input_filename=''):
super(AxodComp, self).__init__()
self.input_filename = input_filename
def execute(self):
""" Run AXOD. """
if os.path.exists('axod.out'):
os.remove('axod.out')
self.results = []
self._logger.debug('running')
try:
shutil.copyfile(self.input_filename, 'axod.inp')
(self.hpower, self.tott, self.totp,
self.mflow, self.effs, self.effr) = axod.axod()
except Exception, exc:
self.raise_exception(str(exc), type(exc))
self._logger.debug('done')
if os.path.exists('axod.out'):
inp = open('axod.out', 'rU')
self.results = inp.readlines()
inp.close()
class HAWC2OrientationRelative(VariableTree):
body1 = List(desc='Main body name to which the body is attached')
body2 = List(desc='Main body name to which the body is attached')
body2_eulerang = List(desc='sequence of euler angle rotations, x->y->z')
mbdy2_ini_rotvec_d1 = Array(
np.zeros(4),
desc='Initial rotation velocity of main body and all'
'subsequent attached bodies (vx, vy, vz, |v|)')
class ArrayParaboloid(Component):
inArray = Array([0.0, 0.0], iotype="in")
f_xy = Float(iotype='out', desc='F(x,y)')
def execute(self):
x = self.inArray[0]
y = self.inArray[1]
self.f_xy = (x - 3.0)**2 + x * y + (y + 4.0)**2 - 3.0
def __init__(self, n=2):
super(Sun_LOS, self).__init__()
self.n = n
self.r1 = 6378.137 * 0.85 # Earth's radius is 6378 km. 0.85 is the alpha in John Hwang's paper
self.r2 = 6378.137
self.add(
'r_e2b_I',
Array(np.zeros((6, n), order='F'),
size=(
6,
n,
),
dtype=np.float,
units="unitless",
desc="Position and velocity vectors from " +
"Earth to satellite in Earth-centered " +
"inertial frame over time.",
iotype="in"))
self.add(
'r_e2s_I',
Array(np.zeros((3, n), order='F'),
size=(
3,
n,
),
dtype=np.float,
units="km",
desc="Position vector from " +
"Earth to sun in Earth-centered inertial " +
"frame over time.",
iotype="in"))
self.add(
'LOS',
Array(np.zeros((n, ), order='F'),
size=(n, ),
dtype=np.float,
units="unitless",
desc="Satellite to sun " + "line of sight over time",
iotype="out"))
class Fblade(VariableTree):
Fx = Array(units='N/m', desc='drag axis')
Fz = Array(units='N/m', desc='lift axis')
My = Array(desc='')
Q = Array(desc='Torque')
P = Array(desc='Power')
Pi = Array(desc='')
Pp = Array(desc='')
class Fblade(VariableTree):
Fx = Array(desc='')
Fz = Array(desc='')
My = Array(desc='')
Q = Array(desc='')
P = Array(desc='')
Pi = Array(desc='')
Pp = Array(desc='')
def __init__(self, Ns):
super(Strain, self).__init__()
self.add('top', Array(np.zeros((3, Ns + 1)), desc=''))
self.add('bottom', Array(np.zeros((3, Ns + 1)), desc=''))
self.add('back', Array(np.zeros((3, Ns + 1)), desc=''))
self.add('front', Array(np.zeros((3, Ns + 1)), desc=''))
self.add('bending_x', Array(np.zeros((1, Ns + 1)), desc=''))
self.add('bending_z', Array(np.zeros((1, Ns + 1)), desc=''))
self.add('axial_y', Array(np.zeros((1, Ns + 1)), desc=''))
self.add('torsion_y', Array(np.zeros((1, Ns + 1)), desc=''))
def __init__(self, minSize=(50, 50), smooth=10., return_one=True):
#fn = "cascades/haarcascade_frontalface_default.xml"
fn = "cascades/haarcascade_frontalface_alt.xml"
#fn="cascades/haarcascade_frontalface_alt2.xml"
#fn = "cascades/haarcascade_frontalface_alt_tree"
super(faceDetector, self).__init__(fn,
minSize=minSize,
smooth=smooth,
return_one=return_one)
self.add("foreheads", Array([[0, 0, 2, 2]], iotype="out"))
class SimpleWind(VariableTree):
TimeSteps = Int(desc='number of time steps')
Time = Array(desc='time step')
HorSpd = Array(desc='horizontal wind speed')
WindDir = Array(desc='wind direction')
VerSpd = Array(desc='vertical wind speed')
HorShr = Array(desc='horizontal shear')
VerShr = Array(desc='vertical power-law shear')
LnVShr = Array(desc='vertical linear shear')
GstSpd = Array(desc='gust speed not sheared by Aerodyn')
def __init__(self, iotype, client, rpath, typ):
ProxyMixin.__init__(self, client, rpath)
self._type = typ
default = self._parse(self._valstr)
desc = client.get(rpath+'.description')
if typ == float:
as_units = client.get(rpath+'.units')
if as_units:
om_units = get_translation(as_units)
else:
om_units = None
if typ != str:
if client.get(rpath+'.hasUpperBound') == 'true':
high = typ(client.get(rpath+'.upperBound'))
else:
high = None
if client.get(rpath+'.hasLowerBound') == 'true':
low = typ(client.get(rpath+'.lowerBound'))
else:
low = None
if typ == float:
Array.__init__(self, dtype=typ, iotype=iotype, desc=desc,
default_value=default, low=low, high=high,
units=om_units)
elif typ == int:
Array.__init__(self, dtype=typ, iotype=iotype, desc=desc,
default_value=default, low=low, high=high)
else:
# FIXME: This will pickle, but not unpickle.
# Probabably don't want fixed max-length string storage anyway.
Array.__init__(self, dtype=typ, iotype=iotype, desc=desc,
default_value=default)
