def run_subcommand(command, options, targets, blade_path, build_dir):
if command == 'query' and options.depended:
targets = ['.:...']
blade.blade = blade.Blade(targets, blade_path, _WORKING_DIR, build_dir,
_BLADE_ROOT_DIR, options, command)
# Build the targets
blade.blade.load_targets()
if options.stop_after == 'load':
return 0
blade.blade.analyze_targets()
if options.stop_after == 'analyze':
return 0
blade.blade.generate()
if options.stop_after == 'generate':
return 0
# Switch case due to different sub command
action = {
'build': build,
'run': run,
'test': test,
'clean': clean,
'query': query
}[command]
try:
returncode = action(options)
finally:
clear_build_script()
return returncode
def main():
os.system("cls")
songsdir = "songs"
for i in range(math.floor(maxsong / cpucount)):
for j in range(1, cpucount + 1):
worker = blade.Blade(i * j, nectarine_url, songsdir)
worker.start()
print("Ripping song {}".format(i * j), end='\r')
time.sleep(0.2)
def appStarted(app):
app.running = True
app.debugMode = False
app.maxThreads = 8
app.runThreads = True
app.focalLength = 600
app.ticks = 0
app.timerDelay = 1
app.cubes = []
app.polys = []
app.cubeSpeed = 10 #no units
app.grid = grid3d.Grid3d(app, app.focalLength)
app.blade = blade.Blade(app)
app.beatCount = 0
#number of beats a block spawns beforehand
app.preSpawnBeats = 4
app.camThreshold = .9
app.cam = camTracker.camTracker()
app.playerPos = (0,0)
cThread = camThread(1, "camThread", app)
cThread.start()
app.driver = audioDriver.audioDriver("all")
app.totalScore = 0
app.totalCubes = 0
app.goodSlices = 0
app.badSlices = 0
app.sliceErrorRange = (0,0.5) #by how many beats the player can be off
app.timeScoreWeight = 20
app.sliceScoreWeight = 20
app.songName = app.app.song
app.loadSong()
app.sparks = []
app.animationPulse = 0
app.bgColor = (0,0,0)
aThread = animationThread("aThread", app)
aThread.start()
def main():
"""実行用関数."""
# クオータニオンモジュールの初期化.
att = attitude.Attitude6DoF()
att.omegaBody = [0.0, 0.0 * pi / 180, 0.0 * pi / 180]
# ブレードの初期化（複数の翼をつける場合は逐次appendする）
blade_pitch = -80.0
Blades = []
Blades.append(
blade.Blade(
n_elem=10,
pos_root=[0.0, 0.06, -0.05],
att=[0.0 * pi / 180, blade_pitch * pi / 180, 0.0 * pi / 180],
b_len=0.13,
c_len=0.1,
airfoil=af.NACA0012_181127))
Blades.append(
blade.Blade(
n_elem=10,
pos_root=[0.0, -0.06, -0.05],
att=[0.0 * pi / 180, blade_pitch * pi / 180, 180.0 * pi / 180],
b_len=0.13,
c_len=0.1,
airfoil=af.NACA0012_181127))
Blades.append(
blade.Blade(
n_elem=10,
pos_root=[0.06, 0.0, -0.05],
att=[0.0 * pi / 180, blade_pitch * pi / 180, 270.0 * pi / 180],
b_len=0.13,
c_len=0.1,
airfoil=af.NACA0012_181127))
Blades.append(
blade.Blade(
n_elem=10,
pos_root=[-0.06, 0.0, -0.05],
att=[0.0 * pi / 180, blade_pitch * pi / 180, 90.0 * pi / 180],
b_len=0.13,
c_len=0.1,
airfoil=af.NACA0012_181127))
# 状態量の初期化
x0 = np.zeros((13), dtype=float)
x0[0:4] = att.setQuartanionFrom(5.0 * pi / 180, 0.0 * pi / 180,
0.0 * pi / 180)
x0[4:7] = att.omegaBody
# x0[7:10]: position of the model
x0[10:13] = att.velocityBody
t0 = 0.0
tf = 2.0
dt = 0.0001
F = np.array([0.0, 0.0, 0])
M = np.array([0.0, 0.0, 0])
# ODEの設定
solver = ode(func).set_integrator('dopri5', method='bdf')
solver.set_initial_value(x0, t0)
solver.set_f_params(att, solver.y, F, M)
x = np.zeros([int((tf - t0) / dt) + 1, 13])
t = np.zeros([int((tf - t0) / dt) + 1, 1])
F_log = np.zeros((int((tf - t0) / dt) + 1, 3))
M_log = np.zeros((int((tf - t0) / dt) + 1, 3))
arrP_log = np.zeros((int((tf - t0) / dt) + 1, len(Blades), 3, 11),
dtype=float)
# TODO: solver.yのクオータニオン地を正規化しなければならない
index = 0
while solver.successful() and solver.t < tf and index < int(
(tf - t0) / dt) + 1:
solver.integrate(solver.t + dt)
x[index] = solver.y
t[index] = solver.t
print(solver.y)
F, M, arrPressures = blade_FM(solver.y, Blades)
F_log[index] = F
M_log[index] = M
arrP_log[index, :, :, :] = arrPressures
xt = postProcess(att, solver.y)
solver.set_initial_value(xt, solver.t)
solver.set_f_params(att, solver.y, F, M)
index += 1
x_log = np.hstack((t, x))
F_log = np.hstack((t, F_log))
M_log = np.hstack((t, M_log))
np.save('x_1', x_log)
np.save('M_1', M_log)
np.save('F_1', F_log)
np.save('dist_df', arrP_log)
"""Just some testing."""
from sqlalchemy import create_engine
from sqlalchemy.orm import sessionmaker
from base import Base
import blade
import airfoil
import flosim
import flosolver
engine = create_engine('sqlite:///my_test_db.sqlite3')
Session = sessionmaker(bind=engine)
session = Session()
# Create table
Base.metadata.create_all(engine)
myblade = blade.Blade()
myairfoil = airfoil.Airfoil(airfoil_name='jfoil')
airfoil2 = airfoil.Airfoil(airfoil_name='bfoil')
myblade.airfoils.append(myairfoil)
myblade.airfoils.append(airfoil2)
session.add(myblade)
session.commit()