本文整理汇总了Python中JSBSim_utils.SandBox类的典型用法代码示例。如果您正苦于以下问题:Python SandBox类的具体用法?Python SandBox怎么用?Python SandBox使用的例子?那么, 这里精选的类代码示例或许可以为您提供帮助。
在下文中一共展示了SandBox类的15个代码示例,这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞,您的评价将有助于系统推荐出更棒的Python代码示例。
示例1: TestDebugLvl
class TestDebugLvl(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox('check_cases', 'orbit')
def tearDown(self):
self.sandbox.erase()
def testDebugLvl(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'ball_orbit.xml'))
fdm.run_ic()
ExecuteUntil(fdm, 1000.)
ref, current = Table(), Table()
ref.ReadCSV(self.sandbox('BallOut.csv'))
del fdm
os.environ["JSBSIM_DEBUG"]=str(0)
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'ball_orbit.xml'))
fdm.run_ic()
ExecuteUntil(fdm, 1000.)
current.ReadCSV(self.sandbox('BallOut.csv'))
diff = ref.compare(current)
self.longMessage = True
self.assertTrue(diff.empty(), msg='\n'+repr(diff))
示例2: TestGustReset
class TestGustReset(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_gust_reset(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'c172_cruise_8K.xml'))
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.set_output_directive(self.sandbox.path_to_jsbsim_file('tests', 'output.xml'))
fdm.run_ic()
ExecuteUntil(fdm, 15.5)
ref, current = Table(), Table()
ref.ReadCSV(self.sandbox('output.csv'))
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.reset_to_initial_conditions(1)
ExecuteUntil(fdm, 15.5)
current.ReadCSV(self.sandbox('output_0.csv'))
diff = ref.compare(current)
self.longMessage = True
self.assertTrue(diff.empty(), msg='\n'+repr(diff))
示例3: CheckScripts
class CheckScripts(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
self.scripts = 0
def tearDown(self):
print "Tested %g scripts" % (self.scripts,)
self.sandbox.erase()
def testScripts(self):
script_path = self.sandbox.path_to_jsbsim_file('scripts')
for f in os.listdir(self.sandbox.elude(script_path)):
fullpath = os.path.join(self.sandbox.elude(script_path), f)
# Does f contains a JSBSim script ?
if not CheckXMLFile(fullpath, 'runscript'):
continue
fdm = CreateFDM(self.sandbox)
self.assertTrue(fdm.load_script(os.path.join(script_path, f)),
msg="Failed to load script %s" % (fullpath,))
fdm.run_ic()
self.scripts += 1
del fdm
示例4: TestScriptOutput
class TestScriptOutput(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
self.script_path = self.sandbox.path_to_jsbsim_file('scripts',
'c1722.xml')
def tearDown(self):
self.sandbox.erase()
def test_no_output(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.script_path)
fdm.run_ic()
ExecuteUntil(fdm, 10.)
self.assertFalse(self.sandbox.exists('output.csv'),
msg="Results have unexpectedly been written to 'output.csv'")
def test_output_from_file(self):
tree = et.parse(self.sandbox.elude(self.script_path))
output_tag = et.SubElement(tree.getroot(), 'output')
output_tag.attrib['file'] = self.sandbox.elude(self.sandbox.path_to_jsbsim_file('tests', 'output.xml'))
tree.write(self.sandbox('c1722_0.xml'))
fdm = CreateFDM(self.sandbox)
fdm.load_script('c1722_0.xml')
fdm.run_ic()
ExecuteUntil(fdm, 10.)
self.assertTrue(self.sandbox.exists('output.csv'),
msg="The file 'output.csv' has not been created")
def test_output(self):
tree = et.parse(self.sandbox.elude(self.script_path))
output_tag = et.SubElement(tree.getroot(), 'output')
output_tag.attrib['name'] = 'test.csv'
output_tag.attrib['type'] = 'CSV'
output_tag.attrib['rate'] = '10'
property_tag = et.SubElement(output_tag, 'property')
property_tag.text = 'position/vrp-radius-ft'
tree.write(self.sandbox('c1722_0.xml'))
fdm = CreateFDM(self.sandbox)
fdm.load_script('c1722_0.xml')
fdm.run_ic()
ExecuteUntil(fdm, 10.)
self.assertTrue(self.sandbox.exists(output_tag.attrib['name']),
msg="The file 'output.csv' has not been created")
orig = pd.read_csv(self.sandbox('JSBout172B.csv'))
test = pd.read_csv(self.sandbox('test.csv'))
self.assertEqual(np.max(orig['Time']-test['Time']), 0.0)
pname = '/fdm/jsbsim/' + property_tag.text
self.assertEqual(np.max(orig[pname]-test[pname]), 0.0)
示例5: setUp
def setUp(self):
self.sandbox = SandBox()
self.script_path = self.sandbox.path_to_jsbsim_file("scripts", "c1724.xml")
# Since we will alter the aircraft definition file, we need make a copy
# of it and of all the files it is refering to.
self.tree, self.aircraft_name, self.path_to_jsbsim_aircrafts = CopyAircraftDef(self.script_path, self.sandbox)
示例6: setUp
def setUp(self):
self.sandbox = SandBox()
self.fdm = CreateFDM(self.sandbox)
self.script_path = self.sandbox.path_to_jsbsim_file("scripts", "c1722.xml")
# Read the time step 'dt' from the script file
self.tree = et.parse(self.sandbox.elude(self.script_path))
root = self.tree.getroot()
use_tag = root.find("./use")
aircraft_name = use_tag.attrib["aircraft"]
self.run_tag = root.find("./run")
self.dt = float(self.run_tag.attrib["dt"])
# Read the date at which the trim will be run
event_tags = root.findall("./run/event")
for event in event_tags:
if event.attrib["name"] == "Trim":
cond_tag = event.find("./condition")
self.trim_date = float(string.split(cond_tag.text)[-1])
break
# Read the output rate and the output file from the aircraft file
aircraft_path = self.sandbox.path_to_jsbsim_file("aircraft", aircraft_name, append_xml(aircraft_name))
tree = et.parse(self.sandbox.elude(aircraft_path))
output_tag = tree.getroot().find("./output")
self.output_file = self.sandbox(output_tag.attrib["name"])
self.rateHz = float(output_tag.attrib["rate"])
self.rate = int(1.0 / (self.rateHz * self.dt))
示例7: setUp
def setUp(self):
self.sandbox = SandBox()
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'c1722.xml')
# The aircraft c172x does not contain an <input> tag so we need
# to add one.
tree, aircraft_name, b = CopyAircraftDef(script_path, self.sandbox)
self.root = tree.getroot()
input_tag = et.SubElement(self.root, 'input')
input_tag.attrib['port']='1137'
tree.write(self.sandbox('aircraft', aircraft_name, aircraft_name+'.xml'))
self.fdm = CreateFDM(self.sandbox)
self.fdm.set_aircraft_path('aircraft')
self.fdm.load_script(script_path)
self.fdm.run_ic()
self.fdm.hold()
# Execute JSBSim in a separate thread
self.cond = threading.Condition()
self.thread = JSBSimThread(self.fdm, self.cond, 5., time.time())
self.thread.start()
# Wait for the thread to be started before connecting a telnet session
self.cond.acquire()
self.cond.wait()
self.tn = telnetlib.Telnet("localhost", 1137)
self.cond.release()
示例8: TestCosineGust
class TestCosineGust(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def testMagnitude(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts',
'c172_cruise_8K.xml'))
fdm.run_ic()
t = 0.0
startup_duration = 5.0
steady_duration = 1.0
end_duration = 5.0
start_time = 10.0
magnitude = 30.0
end_time = start_time + startup_duration + steady_duration + end_duration
while fdm.get_property_value('simulation/run_id') == 0:
fdm.run()
wn = fdm.get_property_value('atmosphere/total-wind-north-fps')
we = fdm.get_property_value('atmosphere/total-wind-east-fps')
wd = fdm.get_property_value('atmosphere/total-wind-down-fps')
if t >= start_time and t <= end_time:
wmag = math.sqrt(wn*wn + we*we + wd*wd)
t -= start_time
if t <= startup_duration:
self.assertAlmostEqual(0.5 * magnitude * (1.0 - math.cos(math.pi*t/startup_duration)),
wmag, delta=1E-3)
else:
t -= startup_duration
if t <= steady_duration:
self.assertAlmostEqual(magnitude, wmag, delta=1E-8)
else:
t -= steady_duration
if t <= end_duration:
self.assertAlmostEqual(0.5 * magnitude * (1.0 + math.cos(math.pi*t/end_duration)),
wmag, delta=1E-3)
t = fdm.get_property_value('simulation/sim-time-sec')
示例9: CheckTrim
class CheckTrim(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_trim_doesnt_ignite_rockets(self):
# Run a longitudinal trim with a rocket equipped with solid propellant
# boosters (aka SRBs). The trim algorithm will try to reach a vertical
# equilibrium by tweaking the throttle but since the rocket is nose up,
# the trim cannot converge. As a result the algorithm will set full
# throttle which will result in the SRBs ignition if the integration is
# not suspended. This bug has been reported in FlightGear and this test
# is checking that there is no regression.
fdm = CreateFDM(self.sandbox)
fdm.load_model('J246')
aircraft_path = self.sandbox.elude(self.sandbox.path_to_jsbsim_file('aircraft'))
fdm.load_ic(os.path.join(aircraft_path, 'J246', 'LC39'), False)
fdm.run_ic()
# Check that the SRBs are not ignited
self.assertEqual(fdm['propulsion/engine[0]/thrust-lbs'], 0.0)
self.assertEqual(fdm['propulsion/engine[1]/thrust-lbs'], 0.0)
try:
fdm['simulation/do_simple_trim'] = 1
except RuntimeError as e:
# The trim cannot succeed. Just make sure that the raised exception
# is due to the trim failure otherwise rethrow.
if e.args[0] != 'Trim Failed':
raise
# Check that the trim did not ignite the SRBs
self.assertEqual(fdm['propulsion/engine[0]/thrust-lbs'], 0.0)
self.assertEqual(fdm['propulsion/engine[1]/thrust-lbs'], 0.0)
def test_trim_on_ground(self):
fdm = CreateFDM(self.sandbox)
fdm.load_model('c172x')
fdm['ic/theta-deg'] = 10.0
fdm.run_ic()
fdm['ic/theta-deg'] = 0.0
fdm['simulation/do_simple_trim'] = 2
示例10: CheckAircrafts
class CheckAircrafts(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def testAircrafts(self):
aircraft_path = self.sandbox.elude(self.sandbox.path_to_jsbsim_file('aircraft'))
for d in os.listdir(aircraft_path):
fullpath = os.path.join(aircraft_path, d)
# Is d a directory ?
if not os.path.isdir(fullpath):
continue
f = os.path.join(aircraft_path, d, append_xml(d))
# Is f an aircraft definition file ?
if not CheckXMLFile(f, 'fdm_config'):
continue
if d in ('blank'):
continue
fdm = CreateFDM(self.sandbox)
self.assertTrue(fdm.load_model(d),
msg='Failed to load aircraft %s' % (d,))
for f in os.listdir(fullpath):
f = os.path.join(aircraft_path, d, f)
if CheckXMLFile(f, 'initialize'):
self.assertTrue(fdm.load_ic(f, False),
msg='Failed to load IC %s for aircraft %s' %(f,d))
try:
fdm.run_ic()
except RuntimeError:
self.fail('Failed to run IC %s for aircraft %s' %(f,d))
break
del fdm
示例11: TestHoldDown
class TestHoldDown(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_static_hold_down(self):
fdm = CreateFDM(self.sandbox)
fdm.load_model('J246')
aircraft_path = self.sandbox.elude(self.sandbox.path_to_jsbsim_file('aircraft'))
fdm.load_ic(os.path.join(aircraft_path, 'J246', 'LC39'), False)
fdm.set_property_value('forces/hold-down', 1.0)
fdm.run_ic()
h0 = fdm.get_property_value('position/h-sl-ft')
t = 0.0
while t < 420.0:
fdm.run()
t = fdm.get_property_value('simulation/sim-time-sec')
self.assertAlmostEqual(fdm.get_property_value('position/h-sl-ft'),
h0, delta=1E-5)
示例12: TestOrbitCheckCase
class TestOrbitCheckCase(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox('check_cases', 'orbit')
def tearDown(self):
self.sandbox.erase()
def testOrbitCheckCase(self):
os.environ['JSBSIM_DEBUG'] = str(0)
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'ball_orbit.xml'))
fdm.run_ic()
while fdm.run():
pass
ref, current = Table(), Table()
ref.ReadCSV(self.sandbox.elude(self.sandbox.path_to_jsbsim_file('logged_data', 'BallOut.csv')))
current.ReadCSV(self.sandbox('BallOut.csv'))
diff = ref.compare(current)
self.longMessage = True
self.assertTrue(diff.empty(), msg='\n'+repr(diff))
示例13: CheckMomentsUpdate
class CheckMomentsUpdate(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_moments_update(self):
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'weather-balloon.xml')
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
fdm.run_ic()
# Moves the radio sonde to modify the CG location
fdm.set_property_value('inertia/pointmass-location-X-inches', 5.0)
# Check that the moment is immediately updated accordingly
fdm.run()
Fbz = fdm.get_property_value('forces/fbz-buoyancy-lbs')
CGx = fdm.get_property_value('inertia/cg-x-in') / 12.0 # Converts from in to ft
Mby = fdm.get_property_value('moments/m-buoyancy-lbsft')
self.assertTrue(abs(Fbz * CGx + Mby) < 1E-7,
msg="Fbz*CGx = %f and Mby = %f do not match" % (-Fbz*CGx, Mby))
示例14: ResetOutputFiles
class ResetOutputFiles(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_reset_output_files(self):
#
# Regular run that checks the correct CSV file is created
# We are just checking its existence, not its content. To accelerate the
# test execution, the simulation is interrupted after 1.0sec of simulated
# time.
#
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'c1722.xml'))
fdm.run_ic()
ExecuteUntil(fdm, 1.0)
self.assertTrue(self.sandbox.exists('JSBout172B.csv'),
msg="Standard run: the file 'JSBout172B.csv' should exist.")
#
# Reset the simulation and check that iteration number is correctly
# appended to the filename.
#
fdm.reset_to_initial_conditions(1)
ExecuteUntil(fdm, 1.0)
self.assertTrue(self.sandbox.exists('JSBout172B_0.csv'),
msg="Reset: the file 'JSBout172B_0.csv' should exist.")
#
# Change the output filename and check that the naming logic is reset
# (e.g. that no iteration number is appended to the filename)
#
fdm.set_output_filename(0, 'dummy.csv')
fdm.reset_to_initial_conditions(1)
ExecuteUntil(fdm, 1.0)
self.assertTrue(self.sandbox.exists('dummy.csv'),
msg="Output name renaming: the file 'dummy.csv' should exist.")
#
# Call FGFDMExec::SetOutputFileName() after the simulation is reset. And
# verify that the new output file name is ignored until the next call to
# FGOutput::SetStartNewOutput(). This should be so according to the
# documentation of FGOutput::SetOutputName().
#
fdm.reset_to_initial_conditions(1)
fdm.set_output_filename(0, 'dummyx.csv')
ExecuteUntil(fdm, 1.0)
self.assertTrue(not self.sandbox.exists('dummyx.csv'),
msg="Late renaming: 'dummyx.csv' should not exist.")
self.assertTrue(self.sandbox.exists('dummy_0.csv'),
msg="Late renaming: 'dummy_0.csv' should exist.")
#
# Check that the new filename is taken into account when the simulation is
# reset.
#
fdm.reset_to_initial_conditions(1)
ExecuteUntil(fdm, 1.0)
self.assertTrue(self.sandbox.exists('dummyx.csv'),
msg="Reset after late renaming: 'dummyx.csv' should exist.")
#
# Check against multiple calls to FGFDMExec::SetOutputFileName()
#
fdm.set_output_filename(0, 'this_one.csv')
fdm.set_output_filename(0, 'that_one.csv')
fdm.reset_to_initial_conditions(1)
ExecuteUntil(fdm, 1.0)
self.assertTrue(not self.sandbox.exists('this_one.csv'),
msg="Output name overwritten: 'this_one.csv' should not exist.")
self.assertTrue(self.sandbox.exists('that_one.csv'),
msg="Output name overwritten: 'that_one.csv' should exist.")
#
# Check again on a brand new FDM
#
self.sandbox.delete_csv_files()
# Because JSBSim internals use static pointers, we cannot rely on Python
# garbage collector to decide when the FDM is destroyed otherwise we can
# get dangling pointers.
del fdm
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts', 'c1722.xml'))
fdm.run_ic()
fdm.set_output_filename(0,'oops.csv') # Oops!! Changed my mind
ExecuteUntil(fdm, 1.0)
self.assertTrue(not self.sandbox.exists('oops.csv'),
#.........这里部分代码省略.........
示例15: ScriptExecution
import os, time, sys, string
import xml.etree.ElementTree as et
from multiprocessing import Process
from scipy import stats
from JSBSim_utils import SandBox, CreateFDM, append_xml, CopyAircraftDef
def ScriptExecution(fdm, script_path, time_limit = 1E+9):
fdm.load_script(script_path)
fdm.run_ic()
while fdm.run() and fdm.get_sim_time() < time_limit:
if fdm.get_property_value('fcs/left-aileron-pos-rad') != 0.0:
sys.exit(-1)
sandbox = SandBox()
# First, the execution time of the script c1724.xml is measured. It will be used
# as a reference to check if JSBSim hangs or not.
script_path = sandbox.path_to_jsbsim_file('scripts', 'c1724.xml')
fdm = CreateFDM(sandbox)
start_time = time.time()
ScriptExecution(fdm, script_path)
exec_time = time.time() - start_time
# Since we will alter the aircraft definition file, we need make a copy of it
# and all the files it is refering to.
tree, aircraft_name, path_to_jsbsim_aircrafts = CopyAircraftDef(script_path, sandbox)
# Now the copy of the aircraft definition file will be altered: the <rate_limit>