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
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
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)
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))
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
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
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
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)
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))
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)
# ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
# FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
# details.
#
# You should have received a copy of the GNU General Public License along with
# this program; if not, see <http://www.gnu.org/licenses/>
#
import sys
from JSBSim_utils import CreateFDM, Table, SandBox
sandbox = SandBox("check_cases", "orbit")
fdm = CreateFDM(sandbox)
fdm.load_script(sandbox.path_to_jsbsim_file("scripts", "ball_orbit.xml"))
fdm.run_ic()
while fdm.run():
pass
ref, current = Table(), Table()
ref.ReadCSV(sandbox.elude(sandbox.path_to_jsbsim_file("logged_data", "BallOut.csv")))
current.ReadCSV(sandbox("BallOut.csv"))
diff = ref.compare(current)
if not diff.empty():
print diff
sys.exit(-1) # Needed for 'make test' to report the test passed.
sandbox.erase()
class TestAccelerometer(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def AddAccelerometersToAircraft(self, script_path):
tree, aircraft_name, b = CopyAircraftDef(script_path, self.sandbox)
system_tag = et.SubElement(tree.getroot(), 'system')
system_tag.attrib['file'] = 'accelerometers'
tree.write(self.sandbox('aircraft', aircraft_name, aircraft_name+'.xml'))
def testOrbit(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
# The time step is too small in ball_orbit so let's increase it to 0.1s
# for a quicker run
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
run_tag.attrib['dt'] = '0.1'
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_name)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
fdm.run_ic()
while fdm.run():
self.assertAlmostEqual(fdm.get_property_value('fcs/accelerometer/X'),
0.0, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('fcs/accelerometer/Y'),
0.0, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('fcs/accelerometer/Z'),
0.0, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-x-ft_sec2'),
0.0, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-y-ft_sec2'),
0.0, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-z-ft_sec2'),
0.0, delta=1E-8)
del fdm
def testOnGround(self):
script_name = 'c1721.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Use the standard gravity (i.e. GM/r^2)
fdm.set_property_value('simulation/gravity-model', 0)
# Simplifies the transformation to compare the accelerometer with the
# gravity
fdm.set_property_value('ic/psi-true-rad', 0.0)
fdm.run_ic()
for i in xrange(500):
fdm.run()
ax = fdm.get_property_value('accelerations/udot-ft_sec2')
ay = fdm.get_property_value('accelerations/vdot-ft_sec2')
az = fdm.get_property_value('accelerations/wdot-ft_sec2')
g = fdm.get_property_value('accelerations/gravity-ft_sec2')
theta = fdm.get_property_value('attitude/theta-rad')
# There is a lag of one time step between the computations of the
# accelerations and the update of the accelerometer
fdm.run()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
fax -= ax
faz -= az
self.assertAlmostEqual(fay, 0.0, delta=1E-6)
self.assertAlmostEqual(fax / (g * math.sin(theta)), 1.0, delta=1E-5)
self.assertAlmostEqual(faz / (g * math.cos(theta)), -1.0, delta=1E-7)
del fdm
def testSteadyFlight(self):
script_name = 'c1722.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Use the standard gravity (i.e. GM/r^2)
fdm.set_property_value('simulation/gravity-model', 0)
# Simplifies the transformation to compare the accelerometer with the
# gravity
fdm.set_property_value('ic/psi-true-rad', 0.0)
fdm.run_ic()
while fdm.get_property_value('simulation/sim-time-sec') <= 0.5:
fdm.run()
fdm.set_property_value('simulation/do_simple_trim', 1)
ax = fdm.get_property_value('accelerations/udot-ft_sec2')
ay = fdm.get_property_value('accelerations/vdot-ft_sec2')
az = fdm.get_property_value('accelerations/wdot-ft_sec2')
g = fdm.get_property_value('accelerations/gravity-ft_sec2')
theta = fdm.get_property_value('attitude/theta-rad')
# There is a lag of one time step between the computations of the
# accelerations and the update of the accelerometer
fdm.run()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
fax -= ax
fay -= ay
faz -= az
# Deltas are relaxed because the tolerances of the trimming algorithm
# are quite relaxed themselves.
self.assertAlmostEqual(faz / (g * math.cos(theta)), -1.0, delta=1E-5)
self.assertAlmostEqual(fax / (g * math.sin(theta)), 1.0, delta=1E-5)
self.assertAlmostEqual(math.sqrt(fax*fax+fay*fay+faz*faz)/g, 1.0, delta=1E-6)
del fdm
def testSpinningBodyOnOrbit(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_model('ball')
# Offset the CG along Y (by 30")
fdm.set_property_value('inertia/pointmass-weight-lbs[1]', 50.0)
aircraft_path = self.sandbox.elude(self.sandbox.path_to_jsbsim_file('aircraft', 'ball'))
fdm.load_ic(os.path.join(aircraft_path, 'reset00.xml'), False)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Set the orientation such that the spinning axis is Z.
fdm.set_property_value('ic/phi-rad', 0.5*math.pi)
# Set the angular velocities to 0.0 in the ECEF frame. The angular
# velocity R_{inertial} will therefore be equal to the Earth rotation
# rate 7.292115E-5 rad/sec
fdm.set_property_value('ic/p-rad_sec', 0.0)
fdm.set_property_value('ic/q-rad_sec', 0.0)
fdm.set_property_value('ic/r-rad_sec', 0.0)
fdm.run_ic()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
cgy_ft = fdm.get_property_value('inertia/cg-y-in') / 12.
omega = 0.00007292115 # Earth rotation rate in rad/sec
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-x-ft_sec2'),
fax, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-y-ft_sec2'),
fay, delta=1E-8)
self.assertAlmostEqual(fdm.get_property_value('accelerations/a-pilot-z-ft_sec2'),
faz, delta=1E-8)
# Acceleration along X should be zero
self.assertAlmostEqual(fax, 0.0, delta=1E-8)
# Acceleration along Y should be equal to r*omega^2
self.assertAlmostEqual(fay / (cgy_ft * omega * omega), 1.0, delta=1E-7)
# Acceleration along Z should be zero
self.assertAlmostEqual(faz, 0.0, delta=1E-8)
class TestICOverride(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_IC_override(self):
# Run the script c1724.xml
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'c1724.xml')
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
vt0 = fdm.get_property_value('ic/vt-kts')
fdm.run_ic()
ExecuteUntil(fdm, 1.0)
# Check that the total velocity exported in the output file matches the IC
# defined in the initialization file
ref = Table()
ref.ReadCSV(self.sandbox('JSBout172B.csv'))
for col, title in enumerate(ref._lines[0]):
if title == 'V_{Total} (ft/s)':
self.assertTrue(
abs(ref._lines[1][col] - (vt0 / fpstokts)) < 1E-5,
msg=
"Original script %s\nThe total velocity is %f. The value %f was expected"
% (script_path, ref._lines[1][col], vt0 / fpstokts))
break
else:
self.fail("The total velocity is not exported in %s" %
(script_path, ))
# Now, we will re-run the same test but the IC will be overridden in the scripts
# The initial total velocity is increased by 1 ft/s
vt0 += 1.0
# The script c1724.xml is loaded and the following line is added in it:
# <property value="..."> ic/vt-kts </property>
# The modified script is then saved with the named 'c1724_0.xml'
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find("./run")
property = et.SubElement(run_tag, 'property')
property.text = 'ic/vt-kts'
property.attrib['value'] = str(vt0)
tree.write(self.sandbox('c1724_0.xml'))
# Re-run the same check than above. This time we are making sure than the total
# initial velocity is increased by 1 ft/s
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('c1724_0.xml')
self.assertTrue(
abs(fdm.get_property_value('ic/vt-kts') - vt0) < 1E-5,
msg=
"Modified script %s\nThe total velocity in the IC (%f) is different from %f"
% (self.sandbox('JSBout172B.csv'),
fdm.get_property_value('ic/vt-kts'), vt0))
fdm.run_ic()
ExecuteUntil(fdm, 1.0)
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
for col, title in enumerate(mod._lines[0]):
if title == 'V_{Total} (ft/s)':
self.assertTrue(
abs(mod._lines[1][col] - (vt0 / fpstokts)) < 1E-5,
msg=
"Modified script %s\nThe total velocity is %f. The value %f was expected"
% (self.sandbox('JSBout172B.csv'), mod._lines[1][col],
vt0 / fpstokts))
break
else:
self.fail("The total velocity is not exported in %s" %
(sandbox('JSBout172B.csv'), ))
class TestModelLoading(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def BuildReference(self, script_name):
# Run the script
self.script = self.sandbox.path_to_jsbsim_file(os.path.join('scripts',
script_name))
self.sandbox.delete_csv_files()
fdm = CreateFDM(self.sandbox)
fdm.set_output_directive(self.sandbox.path_to_jsbsim_file('tests',
'output.xml'))
fdm.load_script(self.script)
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.run_ic()
ExecuteUntil(fdm, 50.0)
self.ref = Table()
self.ref.ReadCSV(self.sandbox("output.csv"))
# Since the script will work with modified versions of the aircraft XML
# definition file, we need to make a copy of the directory that contains
# all the input data of that aircraft
tree, self.aircraft_name, self.path_to_jsbsim_aircrafts = CopyAircraftDef(self.script, self.sandbox)
self.aircraft_path = self.sandbox('aircraft', self.aircraft_name)
def ProcessAndCompare(self, section):
# Here we determine if the original aircraft definition <section> is
# inline or read from an external file.
tree = et.parse(os.path.join(self.path_to_jsbsim_aircrafts,
self.aircraft_name + '.xml'))
root = tree.getroot()
# Iterate over all the tags named <section>
for section_element in root.findall(section):
if 'file' in section_element.keys():
self.InsertAndCompare(section_element, tree)
else:
self.DetachAndCompare(section_element, tree)
def DetachAndCompare(self, section_element, tree):
# Extract <section> from the original aircraft definition file and copy
# it in a separate XML file 'section.xml'
section_tree = et.ElementTree(element=section_element)
if 'name' in section_element.keys():
section = section_element.attrib['name']
else:
section = section_element.tag
section_tree.write(os.path.join(self.aircraft_path, section+'.xml'),
xml_declaration=True)
# Now, we need to clean up the aircraft definition file from all
# references to <section>. We just need a single <section> tag that
# points to the file 'section.xml'
for element in list(section_element):
section_element.remove(element)
section_element.attrib = {'file': section+'.xml'}
tree.write(os.path.join(self.aircraft_path, self.aircraft_name+'.xml'),
xml_declaration=True)
self.Compare(section)
def InsertAndCompare(self, section_element, tree):
file_name = append_xml(section_element.attrib['file'])
section_file = os.path.join(self.path_to_jsbsim_aircrafts, file_name)
# If <section> is actually <system>, we need to iterate over all the
# directories in which the file is allowed to be stored until the file
# is located.
if not os.path.exists(section_file) and section_element.tag == 'system':
section_file = os.path.join(self.path_to_jsbsim_aircrafts, "systems", file_name)
if not os.path.exists(section_file):
section_file = self.sandbox.elude(self.sandbox.path_to_jsbsim_file("systems", file_name))
# The original <section> tag is dropped and replaced by the content of
# the file.
section_root = et.parse(section_file).getroot()
del section_element.attrib['file']
section_element.attrib.update(section_root.attrib)
section_element.extend(section_root)
tree.write(os.path.join(self.aircraft_path, self.aircraft_name+'.xml'))
self.Compare(section_element.tag+" file:"+section_file)
def Compare(self, section):
# Rerun the script with the modified aircraft definition
self.sandbox.delete_csv_files()
fdm = CreateFDM(self.sandbox)
# We need to tell JSBSim that the aircraft definition is located in the
# directory build/.../aircraft
fdm.set_aircraft_path('aircraft')
fdm.set_output_directive(self.sandbox.path_to_jsbsim_file('tests', 'output.xml'))
fdm.load_script(self.script)
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.run_ic()
ExecuteUntil(fdm, 50.0)
mod = Table()
mod.ReadCSV(self.sandbox('output.csv'))
# Whether the data is read from the aircraft definition file or from an
# external file, the results shall be exactly identical. Hence the
# precision set to 0.0.
diff = self.ref.compare(mod, 0.0)
self.assertTrue(diff.empty(),
msg='\nTesting section "'+section+'"\n'+repr(diff))
def test_model_loading(self):
self.longMessage = True
self.BuildReference('c1724.xml')
output_ref = Table()
output_ref.ReadCSV(self.sandbox('JSBout172B.csv'))
self.ProcessAndCompare('aerodynamics')
self.ProcessAndCompare('autopilot')
self.ProcessAndCompare('flight_control')
self.ProcessAndCompare('ground_reactions')
self.ProcessAndCompare('mass_balance')
self.ProcessAndCompare('metrics')
self.ProcessAndCompare('propulsion')
self.ProcessAndCompare('system')
# The <output> section needs special handling. In addition to the check
# conducted by ProcessAndCompare with a directive file, we need to
# verify that the <output> tag has been correctly executed by JSBSim.
# In the case of the script c1724.xml, this means that the data output
# in JSBout172B.csv is the same between the reference 'output_ref' and
# the result 'mod' below where the <output> tag was moved in a separate
# file.
self.ProcessAndCompare('output')
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
diff = output_ref.compare(mod, 0.0)
self.assertTrue(diff.empty(),
msg='\nTesting section "output"\n'+repr(diff))
self.BuildReference('weather-balloon.xml')
self.ProcessAndCompare('buoyant_forces')
self.BuildReference('Concorde_runway_test.xml')
self.ProcessAndCompare('external_reactions')
class TestInputSocket(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 sanityCheck(self, _tn):
# Check that the connection has been established
out = _tn.getOutput()
self.assertTrue(string.split(out, '\n')[0] == 'Connected to JSBSim server',
msg="Not connected to the JSBSim server.\nGot message '%s' instead" % (out,))
# Check that "help" returns the minimum set of commands that will be
# tested
self.assertEqual(sorted(map(lambda x: string.strip(string.split(x, '{')[0]),
string.split(_tn.sendCommand("help"), '\n')[2:-2])),
['get', 'help', 'hold', 'info', 'iterate', 'quit', 'resume', 'set'])
def test_no_input(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.script_path)
fdm.run_ic()
fdm.hold()
with self.assertRaises(socket.error):
TelnetInterface(fdm, 5., 1137)
def test_input_socket(self):
# The aircraft c172x does not contain an <input> tag so we need
# to add one.
tree, aircraft_name, b = CopyAircraftDef(self.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'))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(self.script_path)
fdm.run_ic()
fdm.hold()
tn = TelnetInterface(fdm, 5., 1137)
self.sanityCheck(tn)
# Check the aircraft name and its version
msg = string.split(tn.sendCommand("info"), '\n')
self.assertEqual(string.strip(string.split(msg[2], ':')[1]),
string.strip(self.root.attrib['name']))
self.assertEqual(string.strip(string.split(msg[1], ':')[1]),
string.strip(self.root.attrib['version']))
# Check that the simulation time is 0.0
self.assertEqual(float(string.strip(string.split(msg[3], ':')[1])), 0.0)
self.assertEqual(tn.getSimTime(), 0.0)
self.assertEqual(tn.getPropertyValue("simulation/sim-time-sec"), 0.0)
# Check that 'iterate' iterates the correct number of times
tn.sendCommand("iterate 19")
self.assertEqual(tn.getSimTime(), 19. * tn.getDeltaT())
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
tn.getSimTime(), delta=1E-5)
# Wait a little bit and make sure that the simulation time has not
# changed meanwhile thus confirming that the simulation is on hold.
tn.wait(0.1)
self.assertEqual(tn.getSimTime(), 19. * tn.getDeltaT())
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
tn.getSimTime(), delta=1E-5)
# Modify the tank[0] contents via the "send" command
half_contents = 0.5 * tn.getPropertyValue("propulsion/tank/contents-lbs")
tn.sendCommand("set propulsion/tank/contents-lbs " + str(half_contents))
self.assertEqual(tn.getPropertyValue("propulsion/tank/contents-lbs"),
half_contents)
# Check the resume/hold commands
tn.setRealTime(True)
t = tn.getSimTime()
tn.sendCommand("resume")
tn.wait(0.5)
self.assertNotEqual(tn.getSimTime(), t)
tn.wait(0.5)
tn.sendCommand("hold")
tn.setRealTime(False)
t = tn.getSimTime()
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
t, delta=1E-5)
# Wait a little bit and make sure that the simulation time has not
# changed meanwhile thus confirming that the simulation is on hold.
tn.wait(0.1)
self.assertEqual(tn.getSimTime(), t)
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
t, delta=1E-5)
def test_script_input(self):
tree = et.parse(self.sandbox.elude(self.script_path))
input_tag = et.SubElement(tree.getroot(), 'input')
input_tag.attrib['port'] = '1138'
tree.write(self.sandbox('c1722_1.xml'))
fdm = CreateFDM(self.sandbox)
fdm.load_script('c1722_1.xml')
fdm.run_ic()
fdm.hold()
tn = TelnetInterface(fdm, 5., 1138)
self.sanityCheck(tn)
class TestModelLoading(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def BuildReference(self, script_name):
# Run the script
self.script = self.sandbox.path_to_jsbsim_file(
os.path.join('scripts', script_name))
self.sandbox.delete_csv_files()
fdm = CreateFDM(self.sandbox)
fdm.set_output_directive(
self.sandbox.path_to_jsbsim_file('tests', 'output.xml'))
fdm.load_script(self.script)
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.run_ic()
ExecuteUntil(fdm, 50.0)
self.ref = Table()
self.ref.ReadCSV(self.sandbox("output.csv"))
# Since the script will work with modified versions of the aircraft XML
# definition file, we need to make a copy of the directory that contains
# all the input data of that aircraft
tree, self.aircraft_name, self.path_to_jsbsim_aircrafts = CopyAircraftDef(
self.script, self.sandbox)
self.aircraft_path = self.sandbox('aircraft', self.aircraft_name)
def ProcessAndCompare(self, section):
# Here we determine if the original aircraft definition <section> is
# inline or read from an external file.
tree = et.parse(
os.path.join(self.path_to_jsbsim_aircrafts,
self.aircraft_name + '.xml'))
root = tree.getroot()
# Iterate over all the tags named <section>
for section_element in root.findall(section):
if 'file' in section_element.keys():
self.InsertAndCompare(section_element, tree)
else:
self.DetachAndCompare(section_element, tree)
def DetachAndCompare(self, section_element, tree):
# Extract <section> from the original aircraft definition file and copy
# it in a separate XML file 'section.xml'
section_tree = et.ElementTree(element=section_element)
if 'name' in section_element.keys():
section = section_element.attrib['name']
else:
section = section_element.tag
section_tree.write(os.path.join(self.aircraft_path, section + '.xml'),
xml_declaration=True)
# Now, we need to clean up the aircraft definition file from all
# references to <section>. We just need a single <section> tag that
# points to the file 'section.xml'
for element in list(section_element):
section_element.remove(element)
section_element.attrib = {'file': section + '.xml'}
tree.write(os.path.join(self.aircraft_path,
self.aircraft_name + '.xml'),
xml_declaration=True)
self.Compare(section)
def InsertAndCompare(self, section_element, tree):
file_name = append_xml(section_element.attrib['file'])
section_file = os.path.join(self.path_to_jsbsim_aircrafts, file_name)
# If <section> is actually <system>, we need to iterate over all the
# directories in which the file is allowed to be stored until the file
# is located.
if not os.path.exists(
section_file) and section_element.tag == 'system':
section_file = os.path.join(self.path_to_jsbsim_aircrafts,
"systems", file_name)
if not os.path.exists(section_file):
section_file = self.sandbox.elude(
self.sandbox.path_to_jsbsim_file("systems", file_name))
# The original <section> tag is dropped and replaced by the content of
# the file.
section_root = et.parse(section_file).getroot()
del section_element.attrib['file']
section_element.attrib.update(section_root.attrib)
section_element.extend(section_root)
tree.write(
os.path.join(self.aircraft_path, self.aircraft_name + '.xml'))
self.Compare(section_element.tag + " file:" + section_file)
def Compare(self, section):
# Rerun the script with the modified aircraft definition
self.sandbox.delete_csv_files()
fdm = CreateFDM(self.sandbox)
# We need to tell JSBSim that the aircraft definition is located in the
# directory build/.../aircraft
fdm.set_aircraft_path('aircraft')
fdm.set_output_directive(
self.sandbox.path_to_jsbsim_file('tests', 'output.xml'))
fdm.load_script(self.script)
fdm.set_property_value('simulation/randomseed', 0.0)
fdm.run_ic()
ExecuteUntil(fdm, 50.0)
mod = Table()
mod.ReadCSV(self.sandbox('output.csv'))
# Whether the data is read from the aircraft definition file or from an
# external file, the results shall be exactly identical. Hence the
# precision set to 0.0.
diff = self.ref.compare(mod, 0.0)
self.assertTrue(diff.empty(),
msg='\nTesting section "' + section + '"\n' +
repr(diff))
def test_model_loading(self):
self.longMessage = True
self.BuildReference('c1724.xml')
output_ref = Table()
output_ref.ReadCSV(self.sandbox('JSBout172B.csv'))
self.ProcessAndCompare('aerodynamics')
self.ProcessAndCompare('autopilot')
self.ProcessAndCompare('flight_control')
self.ProcessAndCompare('ground_reactions')
self.ProcessAndCompare('mass_balance')
self.ProcessAndCompare('metrics')
self.ProcessAndCompare('propulsion')
self.ProcessAndCompare('system')
# The <output> section needs special handling. In addition to the check
# conducted by ProcessAndCompare with a directive file, we need to
# verify that the <output> tag has been correctly executed by JSBSim.
# In the case of the script c1724.xml, this means that the data output
# in JSBout172B.csv is the same between the reference 'output_ref' and
# the result 'mod' below where the <output> tag was moved in a separate
# file.
self.ProcessAndCompare('output')
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
diff = output_ref.compare(mod, 0.0)
self.assertTrue(diff.empty(),
msg='\nTesting section "output"\n' + repr(diff))
self.BuildReference('weather-balloon.xml')
self.ProcessAndCompare('buoyant_forces')
self.BuildReference('Concorde_runway_test.xml')
self.ProcessAndCompare('external_reactions')
class TestPitotAngle(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_CAS_ic(self):
script_name = 'Short_S23_3.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts',
script_name)
# Add a Pitot angle to the Short S23
tree, aircraft_name, path_to_jsbsim_aircrafts = CopyAircraftDef(script_path, self.sandbox)
metrics_tag = tree.getroot().find('./metrics')
pitot_tag = et.SubElement(metrics_tag, 'pitot_angle')
pitot_tag.attrib['unit'] = 'DEG'
pitot_tag.text = '5.0'
tree.write(self.sandbox('aircraft', aircraft_name,
aircraft_name+'.xml'))
# Read the CAS specified in the IC file
tree = et.parse(self.sandbox.elude(script_path))
use_element = tree.getroot().find('use')
IC_file = use_element.attrib['initialize']
tree = et.parse(os.path.join(path_to_jsbsim_aircrafts,
append_xml(IC_file)))
vc_tag = tree.getroot().find('./vc')
VCAS = float(vc_tag.text)
if 'unit' in vc_tag.attrib and vc_tag.attrib['unit'] == 'FT/SEC':
VCAS /= 1.68781
# Run the IC and check that the model is initialized correctly
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
fdm.run_ic()
self.assertAlmostEqual(fdm.get_property_value('ic/vc-kts'),
VCAS, delta=1E-7)
self.assertAlmostEqual(fdm.get_property_value('velocities/vc-kts'),
VCAS, delta=1E-7)
def test_pitot_angle(self):
script_name = 'ball_chute.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
# Add a Pitot angle to the Cessna 172
tree, aircraft_name, path_to_jsbsim_aircrafts = CopyAircraftDef(script_path, self.sandbox)
root = tree.getroot()
metrics_tag = root.find('./metrics')
pitot_tag = et.SubElement(metrics_tag, 'pitot_angle')
pitot_tag.attrib['unit'] = 'DEG'
pitot_tag.text = '5.0'
contact_tag = root.find('./ground_reactions/contact')
contact_tag.attrib['type'] = 'STRUCTURE'
tree.write(self.sandbox('aircraft', aircraft_name,
aircraft_name+'.xml'))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_model('ball')
pitot_angle = float(pitot_tag.text) * math.pi / 180.
weight = fdm.get_property_value('inertia/weight-lbs')
spring_tag = contact_tag.find('./spring_coeff')
spring_coeff = float(spring_tag.text)
print "Weight=%d Spring=%d" % (weight, spring_coeff)
fdm.set_property_value('ic/h-sl-ft', weight / spring_coeff)
fdm.set_property_value('forces/hold-down', 1.0)
fdm.run_ic()
ExecuteUntil(fdm, 10.)
for i in xrange(36):
for j in xrange(-9, 10):
angle = math.pi * i / 18.0
angle2 = math.pi * j / 18.0
ca2 = math.cos(angle2)
fdm.set_property_value('atmosphere/wind-north-fps',
10. * math.cos(angle) * ca2)
fdm.set_property_value('atmosphere/wind-east-fps',
10. * math.sin(angle) * ca2)
fdm.set_property_value('atmosphere/wind-down-fps',
10. * math.sin(angle2))
fdm.run()
vg = fdm.get_property_value('velocities/vg-fps')
self.assertAlmostEqual(vg, 0.0, delta=1E-7)
vt = fdm.get_property_value('velocities/vt-fps')
self.assertAlmostEqual(vt, 10., delta=1E-7)
mach = vt / fdm.get_property_value('atmosphere/a-fps')
P = fdm.get_property_value('atmosphere/P-psf')
pt = P * math.pow(1+0.2*mach*mach, 3.5)
psl = fdm.get_property_value('atmosphere/P-sl-psf')
rhosl = fdm.get_property_value('atmosphere/rho-sl-slugs_ft3')
A = math.pow((pt-P)/psl+1.0, 1.0/3.5)
alpha = fdm.get_property_value('aero/alpha-rad')
beta = fdm.get_property_value('aero/beta-rad')
vc = math.sqrt(7.0*psl/rhosl*(A-1.0))*math.cos(alpha+pitot_angle)*math.cos(beta)
self.assertAlmostEqual(fdm.get_property_value('velocities/vc-kts'),
max(0.0, vc) / 1.68781, delta=1E-7)
class CheckOutputRate(unittest.TestCase):
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))
def tearDown(self):
del self.fdm
self.sandbox.erase()
def testOutputRate(self):
self.fdm.load_script(self.script_path)
# Check that the output is enabled by default
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"),
1.0)
# Check that the rate is consistent with the values extracted from the
# script and the aircraft definition
self.assertAlmostEqual(self.fdm.get_property_value("simulation/output/log_rate_hz"),
self.rateHz, delta=1E-5)
self.fdm.run_ic()
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 2 lines in
# addition to the headers :
# 1. The initial conditions
# 2. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1], 0.0)
self.assertEqual(output.get_column(0)[2], self.rate * self.dt)
self.assertEqual(output.get_column(0)[2],
self.fdm.get_property_value("simulation/sim-time-sec"))
def testDisablingOutput(self):
self.fdm.load_script(self.script_path)
# Disables the output during the initialization
self.fdm.set_property_value("simulation/output/enabled", 0.0)
self.fdm.run_ic()
self.fdm.set_property_value("simulation/output/enabled", 1.0)
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 1 line in
# addition to the headers :
# 1. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1],
self.fdm.get_property_value("simulation/sim-time-sec"))
def testTrimRestoresOutputSettings(self):
self.fdm.load_script(self.script_path)
# Disables the output during the initialization
self.fdm.set_property_value("simulation/output/enabled", 0.0)
self.fdm.run_ic()
# Check that the output remains disabled even after the trim is
# executed
while self.fdm.get_property_value("simulation/sim-time-sec") < self.trim_date + 2.0*self.dt:
self.fdm.run()
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"),
0.0)
# Re-enable the output and check that the output rate is unaffected by
# the previous operations
self.fdm.set_property_value("simulation/output/enabled", 1.0)
frame = int(self.fdm.get_property_value("simulation/frame"))
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# The frame at which the data is logged must be the next multiple of
# the output rate
self.assertEqual(int(output.get_column(0)[1]/self.dt),
(1 + frame/self.rate)*self.rate)
def testDisablingOutputInScript(self):
property = et.SubElement(self.run_tag, 'property')
property.text = 'simulation/output/enabled'
property.attrib['value'] = "0.0"
self.tree.write(self.sandbox('c1722_0.xml'))
self.fdm.load_script('c1722_0.xml')
# Check that the output is disabled
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"),
0.0)
self.fdm.run_ic()
self.fdm.set_property_value("simulation/output/enabled", 1.0)
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 1 line in
# addition to the headers :
# 1. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1],
self.fdm.get_property_value("simulation/sim-time-sec"))
class TestICOverride(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_IC_override(self):
# Run the script c1724.xml
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'c1724.xml')
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
vt0 = fdm.get_property_value('ic/vt-kts')
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
self.assertAlmostEqual(fdm.get_property_value('velocities/vt-fps'),
vt0 / fpstokts,
delta=1E-7)
ExecuteUntil(fdm, 1.0)
# Check that the total velocity exported in the output file matches the
# IC defined in the initialization file
ref = Table()
ref.ReadCSV(self.sandbox('JSBout172B.csv'))
self.assertEqual(ref.get_column('Time')[1], 0.0)
self.assertAlmostEqual(ref.get_column('V_{Total} (ft/s)')[1],
vt0 / fpstokts,
delta=1E-7)
# Now, we will re-run the same test but the IC will be overridden in the
# script. The initial total velocity is increased by 1 ft/s
vt0 += 1.0
# The script c1724.xml is loaded and the following line is added in it:
# <property value="..."> ic/vt-kts </property>
# The modified script is then saved with the named 'c1724_0.xml'
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find("./run")
property = et.SubElement(run_tag, 'property')
property.text = 'ic/vt-kts'
property.attrib['value'] = str(vt0)
tree.write(self.sandbox('c1724_0.xml'))
# Re-run the same check than above. This time we are making sure than
# the total initial velocity is increased by 1 ft/s
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('c1724_0.xml')
self.assertAlmostEqual(fdm.get_property_value('ic/vt-kts'),
vt0,
delta=1E-6)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
self.assertAlmostEqual(fdm.get_property_value('velocities/vt-fps'),
vt0 / fpstokts,
delta=1E-6)
ExecuteUntil(fdm, 1.0)
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
self.assertAlmostEqual(mod.get_column('V_{Total} (ft/s)')[1],
vt0 / fpstokts,
delta=1E-6)
class TestInputSocket(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 sanityCheck(self, _tn):
# Check that the connection has been established
out = _tn.getOutput()
self.assertTrue(
string.split(out, '\n')[0] == 'Connected to JSBSim server',
msg="Not connected to the JSBSim server.\nGot message '%s' instead"
% (out, ))
# Check that "help" returns the minimum set of commands that will be
# tested
self.assertEqual(
sorted(
map(lambda x: string.strip(string.split(x, '{')[0]),
string.split(_tn.sendCommand("help"), '\n')[2:-2])), [
'get', 'help', 'hold', 'info', 'iterate', 'quit',
'resume', 'set'
])
def test_no_input(self):
fdm = CreateFDM(self.sandbox)
fdm.load_script(self.script_path)
fdm.run_ic()
fdm.hold()
with self.assertRaises(socket.error):
TelnetInterface(fdm, 5., 1137)
def test_input_socket(self):
# The aircraft c172x does not contain an <input> tag so we need
# to add one.
tree, aircraft_name, b = CopyAircraftDef(self.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'))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(self.script_path)
fdm.run_ic()
fdm.hold()
tn = TelnetInterface(fdm, 5., 1137)
self.sanityCheck(tn)
# Check the aircraft name and its version
msg = string.split(tn.sendCommand("info"), '\n')
self.assertEqual(string.strip(string.split(msg[2], ':')[1]),
string.strip(self.root.attrib['name']))
self.assertEqual(string.strip(string.split(msg[1], ':')[1]),
string.strip(self.root.attrib['version']))
# Check that the simulation time is 0.0
self.assertEqual(float(string.strip(string.split(msg[3], ':')[1])),
0.0)
self.assertEqual(tn.getSimTime(), 0.0)
self.assertEqual(tn.getPropertyValue("simulation/sim-time-sec"), 0.0)
# Check that 'iterate' iterates the correct number of times
tn.sendCommand("iterate 19")
self.assertEqual(tn.getSimTime(), 19. * tn.getDeltaT())
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
tn.getSimTime(),
delta=1E-5)
# Wait a little bit and make sure that the simulation time has not
# changed meanwhile thus confirming that the simulation is on hold.
tn.wait(0.1)
self.assertEqual(tn.getSimTime(), 19. * tn.getDeltaT())
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
tn.getSimTime(),
delta=1E-5)
# Modify the tank[0] contents via the "send" command
half_contents = 0.5 * tn.getPropertyValue(
"propulsion/tank/contents-lbs")
tn.sendCommand("set propulsion/tank/contents-lbs " +
str(half_contents))
self.assertEqual(tn.getPropertyValue("propulsion/tank/contents-lbs"),
half_contents)
# Check the resume/hold commands
tn.setRealTime(True)
t = tn.getSimTime()
tn.sendCommand("resume")
tn.wait(0.5)
self.assertNotEqual(tn.getSimTime(), t)
tn.wait(0.5)
tn.sendCommand("hold")
tn.setRealTime(False)
t = tn.getSimTime()
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
t,
delta=1E-5)
# Wait a little bit and make sure that the simulation time has not
# changed meanwhile thus confirming that the simulation is on hold.
tn.wait(0.1)
self.assertEqual(tn.getSimTime(), t)
self.assertAlmostEqual(tn.getPropertyValue("simulation/sim-time-sec"),
t,
delta=1E-5)
def test_script_input(self):
tree = et.parse(self.sandbox.elude(self.script_path))
input_tag = et.SubElement(tree.getroot(), 'input')
input_tag.attrib['port'] = '1138'
tree.write(self.sandbox('c1722_1.xml'))
fdm = CreateFDM(self.sandbox)
fdm.load_script('c1722_1.xml')
fdm.run_ic()
fdm.hold()
tn = TelnetInterface(fdm, 5., 1138)
self.sanityCheck(tn)
class TestSimTimeReset(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_no_script(self):
fdm = CreateFDM(self.sandbox)
aircraft_path = self.sandbox.path_to_jsbsim_file('aircraft')
fdm.set_aircraft_path(aircraft_path)
fdm.load_model('c172x')
aircraft_path = os.path.join(self.sandbox.elude(aircraft_path), 'c172x')
fdm.load_ic(os.path.join(aircraft_path, 'reset01.xml'), False)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
ExecuteUntil(fdm, 5.0)
t = fdm.get_property_value('simulation/sim-time-sec')
fdm.set_property_value('simulation/do_simple_trim', 1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), t)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
del fdm
def test_script_start_time_0(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
del fdm
def test_script_start_time(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
run_tag.attrib['start'] = '1.2'
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_name)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 1.2)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 1.2)
del fdm
def test_script_no_start_time(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
# Remove the parameter 'start' from the tag <run>
del run_tag.attrib['start']
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_name)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
del fdm
class TestInitialConditions(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_initial_conditions(self):
prop_output_to_CSV = ['velocities/vc-kts']
# A dictionary that contains the XML tags to extract from the IC file
# along with the name of the properties that contain the values
# extracted from the IC file.
vars = [{'tag': 'vt', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vt-fps', 'prop': 'velocities/vt-fps',
'CSV_header': 'V_{Total} (ft/s)'},
{'tag': 'vc', 'unit': convtokts, 'default_unit': 'KTS',
'ic_prop': 'ic/vc-kts', 'prop': 'velocities/vc-kts',
'CSV_header': '/fdm/jsbsim/velocities/vc-kts'},
{'tag': 'ubody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/u-fps', 'prop': 'velocities/u-fps',
'CSV_header': 'UBody'},
{'tag': 'vbody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/v-fps', 'prop': 'velocities/v-fps',
'CSV_header': 'VBody'},
{'tag': 'wbody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/w-fps', 'prop': 'velocities/w-fps',
'CSV_header': 'WBody'},
{'tag': 'vnorth', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vn-fps', 'prop': 'velocities/v-north-fps',
'CSV_header': 'V_{North} (ft/s)'},
{'tag': 'veast', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/ve-fps', 'prop': 'velocities/v-east-fps',
'CSV_header': 'V_{East} (ft/s)'},
{'tag': 'vdown', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vd-fps', 'prop': 'velocities/v-down-fps',
'CSV_header': 'V_{Down} (ft/s)'},
{'tag': 'latitude', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/lat-gc-deg', 'prop': 'position/lat-gc-deg',
'CSV_header': 'Latitude (deg)'},
{'tag': 'longitude', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/long-gc-deg', 'prop': 'position/long-gc-deg',
'CSV_header': 'Longitude (deg)'},
{'tag': 'altitude', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-agl-ft', 'prop': 'position/h-agl-ft',
'CSV_header': 'Altitude AGL (ft)'},
{'tag': 'altitudeAGL', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-agl-ft', 'prop': 'position/h-agl-ft',
'CSV_header': 'Altitude AGL (ft)'},
{'tag': 'altitudeMSL', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-sl-ft', 'prop': 'position/h-sl-ft',
'CSV_header': 'Altitude ASL (ft)'},
{'tag': 'phi', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/phi-deg', 'prop': 'attitude/phi-deg',
'CSV_header': 'Phi (deg)'},
{'tag': 'theta', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/theta-deg', 'prop': 'attitude/theta-deg',
'CSV_header': 'Theta (deg)'},
{'tag': 'psi', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/psi-true-deg', 'prop': 'attitude/psi-deg',
'CSV_header': 'Psi (deg)'},
{'tag': 'elevation', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/terrain-elevation-ft',
'prop': 'position/terrain-elevation-asl-ft',
'CSV_header': 'Terrain Elevation (ft)'}]
script_path = self.sandbox.path_to_jsbsim_file('scripts')
for f in os.listdir(self.sandbox.elude(script_path)):
# TODO These scripts need some further investigation
if f in ('ZLT-NT-moored-1.xml',
'737_cruise_steady_turn_simplex.xml'):
continue
fullpath = os.path.join(self.sandbox.elude(script_path), f)
# Does f contains a JSBSim script ?
if not CheckXMLFile(fullpath, 'runscript'):
continue
# Read the IC file name from the script
tree = et.parse(fullpath)
root = tree.getroot()
use_tag = root.find('use')
aircraft_name = use_tag.attrib['aircraft']
aircraft_path = os.path.join('aircraft', aircraft_name)
path_to_jsbsim_aircrafts = self.sandbox.elude(self.sandbox.path_to_jsbsim_file(aircraft_path))
IC_file = append_xml(use_tag.attrib['initialize'])
IC_tree = et.parse(os.path.join(path_to_jsbsim_aircrafts, IC_file))
IC_root = IC_tree.getroot()
# Only testing version 1.0 of init files
if 'version' in IC_root.attrib:
if float(IC_root.attrib['version']) == 2.0:
continue
# Extract the IC values from XML
for var in vars:
var_tag = IC_root.find('./'+var['tag'])
var['specified'] = var_tag is not None
if not var['specified']:
var['value'] = 0.0
continue
var['value'] = float(var_tag.text)
if 'unit' in var_tag.attrib:
conv = var['unit'][var_tag.attrib['unit']]
else:
conv = var['unit'][var['default_unit']]
var['value'] *= conv
# Generate a CSV file to check that it is correctly initialized
# with the initial values
output_tag = et.SubElement(root, 'output')
output_tag.attrib['name'] = 'check_csv_values.csv'
output_tag.attrib['type'] = 'CSV'
output_tag.attrib['rate'] = '10'
position_tag = et.SubElement(output_tag, 'position')
position_tag.text = 'ON'
velocities_tag = et.SubElement(output_tag, 'velocities')
velocities_tag.text = 'ON'
for props in prop_output_to_CSV:
property_tag = et.SubElement(output_tag, 'property')
property_tag.text = props
tree.write(self.sandbox(f))
# Initialize the script
fdm = CreateFDM(self.sandbox)
fdm.load_script(f)
fdm.run_ic()
# Sanity check, we just initialized JSBSim with the ICs, the time
# must be set to 0.0
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
# Check that the properties (including in 'ic/') have been
# correctly initialized (i.e. that they contain the value read from
# the XML file).
for var in vars:
if not var['specified']:
continue
value = var['value']
prop = fdm.get_property_value(var['ic_prop'])
if var['tag'] == 'psi':
if abs(prop - 360.0) <= 1E-8:
prop = 0.0
self.assertAlmostEqual(value, prop, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, prop))
prop = fdm.get_property_value(var['prop'])
if var['tag'] == 'psi':
if abs(prop - 360.0) <= 1E-8:
prop = 0.0
self.assertAlmostEqual(value, prop, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, prop))
# Execute the first second of the script. This is to make sure that
# the CSV file is open and the ICs have been written in it.
try:
ExecuteUntil(fdm, 1.0)
except RuntimeError as e:
if e.args[0] == 'Trim Failed':
self.fail("Trim failed in script %s" % (f,))
else:
raise
# Copies the CSV file content in a table
ref = pd.read_csv(self.sandbox('check_csv_values.csv'))
# Sanity check: make sure that the time step 0.0 has been copied in
# the CSV file.
self.assertEqual(ref['Time'][0], 0.0)
# Check that the value in the CSV file equals the value read from
# the IC file.
for var in vars:
if not var['specified']:
continue
value = var['value']
csv_value = ref[var['CSV_header']][0]
if var['tag'] == 'psi':
if abs(csv_value - 360.0) <= 1E-8:
csv_value = 0.0
self.assertAlmostEqual(value, csv_value, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, csv_value))
del fdm
class TestSimTimeReset(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_no_script(self):
fdm = CreateFDM(self.sandbox)
aircraft_path = self.sandbox.path_to_jsbsim_file('aircraft')
fdm.set_aircraft_path(aircraft_path)
fdm.load_model('c172x')
aircraft_path = os.path.join(self.sandbox.elude(aircraft_path),
'c172x')
fdm.load_ic(os.path.join(aircraft_path, 'reset01.xml'), False)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
ExecuteUntil(fdm, 5.0)
t = fdm.get_property_value('simulation/sim-time-sec')
fdm.set_property_value('simulation/do_simple_trim', 1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), t)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
del fdm
def test_script_start_time_0(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
del fdm
def test_script_start_time(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
run_tag.attrib['start'] = '1.2'
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_name)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
1.2)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
1.2)
del fdm
def test_script_no_start_time(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
# Remove the parameter 'start' from the tag <run>
del run_tag.attrib['start']
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_name)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
ExecuteUntil(fdm, 5.0)
fdm.reset_to_initial_conditions(1)
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
del fdm
class TestAccelerometer(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def AddAccelerometersToAircraft(self, script_path):
tree, aircraft_name, b = CopyAircraftDef(script_path, self.sandbox)
system_tag = et.SubElement(tree.getroot(), 'system')
system_tag.attrib['file'] = 'accelerometers'
tree.write(
self.sandbox('aircraft', aircraft_name, aircraft_name + '.xml'))
def testOrbit(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
# The time step is too small in ball_orbit so let's increase it to 0.1s
# for a quicker run
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find('./run')
run_tag.attrib['dt'] = '0.1'
tree.write(self.sandbox(script_name))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_name)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
fdm.run_ic()
while fdm.run():
self.assertAlmostEqual(
fdm.get_property_value('fcs/accelerometer/X'), 0.0, delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('fcs/accelerometer/Y'), 0.0, delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('fcs/accelerometer/Z'), 0.0, delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-x-ft_sec2'),
0.0,
delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-y-ft_sec2'),
0.0,
delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-z-ft_sec2'),
0.0,
delta=1E-8)
del fdm
def testOnGround(self):
script_name = 'c1721.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Use the standard gravity (i.e. GM/r^2)
fdm.set_property_value('simulation/gravity-model', 0)
# Simplifies the transformation to compare the accelerometer with the
# gravity
fdm.set_property_value('ic/psi-true-rad', 0.0)
fdm.run_ic()
for i in xrange(500):
fdm.run()
ax = fdm.get_property_value('accelerations/udot-ft_sec2')
ay = fdm.get_property_value('accelerations/vdot-ft_sec2')
az = fdm.get_property_value('accelerations/wdot-ft_sec2')
g = fdm.get_property_value('accelerations/gravity-ft_sec2')
theta = fdm.get_property_value('attitude/theta-rad')
# There is a lag of one time step between the computations of the
# accelerations and the update of the accelerometer
fdm.run()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
fax -= ax
faz -= az
self.assertAlmostEqual(fay, 0.0, delta=1E-6)
self.assertAlmostEqual(fax / (g * math.sin(theta)), 1.0, delta=1E-5)
self.assertAlmostEqual(faz / (g * math.cos(theta)), -1.0, delta=1E-7)
del fdm
def testSteadyFlight(self):
script_name = 'c1722.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Use the standard gravity (i.e. GM/r^2)
fdm.set_property_value('simulation/gravity-model', 0)
# Simplifies the transformation to compare the accelerometer with the
# gravity
fdm.set_property_value('ic/psi-true-rad', 0.0)
fdm.run_ic()
while fdm.get_property_value('simulation/sim-time-sec') <= 0.5:
fdm.run()
fdm.set_property_value('simulation/do_simple_trim', 1)
ax = fdm.get_property_value('accelerations/udot-ft_sec2')
ay = fdm.get_property_value('accelerations/vdot-ft_sec2')
az = fdm.get_property_value('accelerations/wdot-ft_sec2')
g = fdm.get_property_value('accelerations/gravity-ft_sec2')
theta = fdm.get_property_value('attitude/theta-rad')
# There is a lag of one time step between the computations of the
# accelerations and the update of the accelerometer
fdm.run()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
fax -= ax
fay -= ay
faz -= az
# Deltas are relaxed because the tolerances of the trimming algorithm
# are quite relaxed themselves.
self.assertAlmostEqual(faz / (g * math.cos(theta)), -1.0, delta=1E-5)
self.assertAlmostEqual(fax / (g * math.sin(theta)), 1.0, delta=1E-5)
self.assertAlmostEqual(math.sqrt(fax * fax + fay * fay + faz * faz) /
g,
1.0,
delta=1E-6)
del fdm
def testSpinningBodyOnOrbit(self):
script_name = 'ball_orbit.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
self.AddAccelerometersToAircraft(script_path)
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_model('ball')
# Offset the CG along Y (by 30")
fdm.set_property_value('inertia/pointmass-weight-lbs[1]', 50.0)
aircraft_path = self.sandbox.elude(
self.sandbox.path_to_jsbsim_file('aircraft', 'ball'))
fdm.load_ic(os.path.join(aircraft_path, 'reset00.xml'), False)
# Switch the accel on
fdm.set_property_value('fcs/accelerometer/on', 1.0)
# Set the orientation such that the spinning axis is Z.
fdm.set_property_value('ic/phi-rad', 0.5 * math.pi)
# Set the angular velocities to 0.0 in the ECEF frame. The angular
# velocity R_{inertial} will therefore be equal to the Earth rotation
# rate 7.292115E-5 rad/sec
fdm.set_property_value('ic/p-rad_sec', 0.0)
fdm.set_property_value('ic/q-rad_sec', 0.0)
fdm.set_property_value('ic/r-rad_sec', 0.0)
fdm.run_ic()
fax = fdm.get_property_value('fcs/accelerometer/X')
fay = fdm.get_property_value('fcs/accelerometer/Y')
faz = fdm.get_property_value('fcs/accelerometer/Z')
cgy_ft = fdm.get_property_value('inertia/cg-y-in') / 12.
omega = 0.00007292115 # Earth rotation rate in rad/sec
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-x-ft_sec2'),
fax,
delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-y-ft_sec2'),
fay,
delta=1E-8)
self.assertAlmostEqual(
fdm.get_property_value('accelerations/a-pilot-z-ft_sec2'),
faz,
delta=1E-8)
# Acceleration along X should be zero
self.assertAlmostEqual(fax, 0.0, delta=1E-8)
# Acceleration along Y should be equal to r*omega^2
self.assertAlmostEqual(fay / (cgy_ft * omega * omega), 1.0, delta=1E-7)
# Acceleration along Z should be zero
self.assertAlmostEqual(faz, 0.0, delta=1E-8)
class TestInitialConditions(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_initial_conditions(self):
# A dictionary that contains the XML tags to extract from the IC file
# along with the name of the properties that contain the values
# extracted from the IC file.
vars = [{'tag': 'vt', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vt-fps', 'prop': 'velocities/vt-fps',
'CSV_header': 'V_{Total} (ft/s)'},
{'tag': 'ubody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/u-fps', 'prop': 'velocities/u-fps',
'CSV_header': 'UBody'},
{'tag': 'vbody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/v-fps', 'prop': 'velocities/v-fps',
'CSV_header': 'VBody'},
{'tag': 'wbody', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/w-fps', 'prop': 'velocities/w-fps',
'CSV_header': 'WBody'},
{'tag': 'vnorth', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vn-fps', 'prop': 'velocities/v-north-fps',
'CSV_header': 'V_{North} (ft/s)'},
{'tag': 'veast', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/ve-fps', 'prop': 'velocities/v-east-fps',
'CSV_header': 'V_{East} (ft/s)'},
{'tag': 'vdown', 'unit': convtofps, 'default_unit': 'FT/SEC',
'ic_prop': 'ic/vd-fps', 'prop': 'velocities/v-down-fps',
'CSV_header': 'V_{Down} (ft/s)'},
{'tag': 'latitude', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/lat-gc-deg', 'prop': 'position/lat-gc-deg',
'CSV_header': 'Latitude (deg)'},
{'tag': 'longitude', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/long-gc-deg', 'prop': 'position/long-gc-deg',
'CSV_header': 'Longitude (deg)'},
{'tag': 'altitude', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-agl-ft', 'prop': 'position/h-agl-ft',
'CSV_header': 'Altitude AGL (ft)'},
{'tag': 'altitudeAGL', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-agl-ft', 'prop': 'position/h-agl-ft',
'CSV_header': 'Altitude AGL (ft)'},
{'tag': 'altitudeMSL', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/h-sl-ft', 'prop': 'position/h-sl-ft',
'CSV_header': 'Altitude ASL (ft)'},
{'tag': 'phi', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/phi-deg', 'prop': 'attitude/phi-deg',
'CSV_header': 'Phi (deg)'},
{'tag': 'theta', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/theta-deg', 'prop': 'attitude/theta-deg',
'CSV_header': 'Theta (deg)'},
{'tag': 'psi', 'unit': convtodeg, 'default_unit': 'RAD',
'ic_prop': 'ic/psi-true-deg', 'prop': 'attitude/psi-deg',
'CSV_header': 'Psi (deg)'},
{'tag': 'elevation', 'unit': convtoft, 'default_unit': 'FT',
'ic_prop': 'ic/terrain-elevation-ft', 'prop': 'position/terrain-elevation-asl-ft',
'CSV_header': 'Terrain Elevation (ft)'}]
script_path = self.sandbox.path_to_jsbsim_file('scripts')
for f in os.listdir(self.sandbox.elude(script_path)):
# TODO These scripts need some further investigation
if f in ('ZLT-NT-moored-1.xml',):
continue
fullpath = os.path.join(self.sandbox.elude(script_path), f)
# Does f contains a JSBSim script ?
if not CheckXMLFile(fullpath, 'runscript'):
continue
# Read the IC file name from the script
tree = et.parse(fullpath)
root = tree.getroot()
use_tag = root.find('use')
aircraft_name = use_tag.attrib['aircraft']
aircraft_path = os.path.join('aircraft', aircraft_name)
path_to_jsbsim_aircrafts = self.sandbox.elude(self.sandbox.path_to_jsbsim_file(aircraft_path))
IC_file = append_xml(use_tag.attrib['initialize'])
IC_tree = et.parse(os.path.join(path_to_jsbsim_aircrafts, IC_file))
IC_root = IC_tree.getroot()
# Only testing version 1.0 of init files
if 'version' in IC_root.attrib:
if float(IC_root.attrib['version']) == 2.0:
continue
# Extract the IC values from XML
for var in vars:
var_tag = IC_root.find('./'+var['tag'])
var['specified'] = var_tag is not None
if not var['specified']:
var['value'] = 0.0
continue
var['value'] = float(var_tag.text)
if 'unit' in var_tag.attrib:
conv = var['unit'][var_tag.attrib['unit']]
else:
conv = var['unit'][var['default_unit']]
var['value'] *= conv
# Generate a CSV file to check that it is correctly initialized with
# the initial values
output_tag = et.SubElement(root, 'output')
output_tag.attrib['name'] = 'check_csv_values.csv'
output_tag.attrib['type'] = 'CSV'
output_tag.attrib['rate'] = '10'
position_tag = et.SubElement(output_tag, 'position')
position_tag.text = 'ON'
velocities_tag = et.SubElement(output_tag, 'velocities')
velocities_tag.text = 'ON'
tree.write(self.sandbox(f))
# Initialize the script
fdm = CreateFDM(self.sandbox)
fdm.load_script(f)
fdm.run_ic()
# Sanity check, we just initialized JSBSim with the ICs, the time
# must be set to 0.0
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'),
0.0)
# Check that the properties (including in 'ic/') have been correctly
# initialized (i.e. that they contain the value read from the XML
# file).
for var in vars:
if not var['specified']:
continue
value = var['value']
prop = fdm.get_property_value(var['ic_prop'])
if var['tag'] == 'psi':
if abs(prop - 360.0) <= 1E-8:
prop = 0.0
self.assertAlmostEqual(value, prop, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, prop))
prop = fdm.get_property_value(var['prop'])
if var['tag'] == 'psi':
if abs(prop - 360.0) <= 1E-8:
prop = 0.0
self.assertAlmostEqual(value, prop, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, prop))
# Execute the first second of the script. This is to make sure that
# the CSV file is open and the ICs have been written in it.
ExecuteUntil(fdm, 1.0)
# Copies the CSV file content in a table
ref = pd.read_csv(self.sandbox('check_csv_values.csv'))
# Sanity check: make sure that the time step 0.0 has been copied in
# the CSV file.
self.assertEqual(ref['Time'][0], 0.0)
# Check that the value in the CSV file equals the value read from
# the IC file.
for var in vars:
if not var['specified']:
continue
value = var['value']
csv_value = ref[var['CSV_header']][0]
if var['tag'] == 'psi':
if abs(csv_value - 360.0) <= 1E-8:
csv_value = 0.0
self.assertAlmostEqual(value, csv_value, delta=1E-7,
msg="In script %s: %s should be %f but found %f" % (f, var['tag'], value, csv_value))
del fdm
class TestICOverride(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_IC_override(self):
# Run the script c1724.xml
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'c1724.xml')
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
vt0 = fdm.get_property_value('ic/vt-kts')
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
self.assertAlmostEqual(fdm.get_property_value('velocities/vt-fps'),
vt0 / fpstokts, delta=1E-7)
ExecuteUntil(fdm, 1.0)
# Check that the total velocity exported in the output file matches the
# IC defined in the initialization file
ref = Table()
ref.ReadCSV(self.sandbox('JSBout172B.csv'))
self.assertEqual(ref.get_column('Time')[1], 0.0)
self.assertAlmostEqual(ref.get_column('V_{Total} (ft/s)')[1],
vt0 / fpstokts, delta=1E-7)
# Now, we will re-run the same test but the IC will be overridden in the
# script. The initial total velocity is increased by 1 ft/s
vt0 += 1.0
# The script c1724.xml is loaded and the following line is added in it:
# <property value="..."> ic/vt-kts </property>
# The modified script is then saved with the named 'c1724_0.xml'
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find("./run")
property = et.SubElement(run_tag, 'property')
property.text = 'ic/vt-kts'
property.attrib['value'] = str(vt0)
tree.write(self.sandbox('c1724_0.xml'))
# Re-run the same check than above. This time we are making sure than
# the total initial velocity is increased by 1 ft/s
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('c1724_0.xml')
self.assertAlmostEqual(fdm.get_property_value('ic/vt-kts'), vt0,
delta=1E-6)
fdm.run_ic()
self.assertEqual(fdm.get_property_value('simulation/sim-time-sec'), 0.0)
self.assertAlmostEqual(fdm.get_property_value('velocities/vt-fps'),
vt0 / fpstokts, delta=1E-6)
ExecuteUntil(fdm, 1.0)
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
self.assertAlmostEqual(mod.get_column('V_{Total} (ft/s)')[1],
vt0 / fpstokts, delta=1E-6)
class TestICOverride(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_IC_override(self):
# Run the script c1724.xml
script_path = self.sandbox.path_to_jsbsim_file('scripts', 'c1724.xml')
fdm = CreateFDM(self.sandbox)
fdm.load_script(script_path)
vt0 = fdm.get_property_value('ic/vt-kts')
fdm.run_ic()
ExecuteUntil(fdm, 1.0)
# Check that the total velocity exported in the output file matches the IC
# defined in the initialization file
ref = Table()
ref.ReadCSV(self.sandbox('JSBout172B.csv'))
for col, title in enumerate(ref._lines[0]):
if title == 'V_{Total} (ft/s)':
self.assertTrue(abs(ref._lines[1][col] - (vt0 / fpstokts)) < 1E-5,
msg="Original script %s\nThe total velocity is %f. The value %f was expected" % (script_path, ref._lines[1][col], vt0 / fpstokts))
break
else:
self.fail("The total velocity is not exported in %s" % (script_path,))
# Now, we will re-run the same test but the IC will be overridden in the scripts
# The initial total velocity is increased by 1 ft/s
vt0 += 1.0
# The script c1724.xml is loaded and the following line is added in it:
# <property value="..."> ic/vt-kts </property>
# The modified script is then saved with the named 'c1724_0.xml'
tree = et.parse(self.sandbox.elude(script_path))
run_tag = tree.getroot().find("./run")
property = et.SubElement(run_tag, 'property')
property.text = 'ic/vt-kts'
property.attrib['value'] = str(vt0)
tree.write(self.sandbox('c1724_0.xml'))
# Re-run the same check than above. This time we are making sure than the total
# initial velocity is increased by 1 ft/s
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('c1724_0.xml')
self.assertTrue(abs(fdm.get_property_value('ic/vt-kts') - vt0) < 1E-5,
msg="Modified script %s\nThe total velocity in the IC (%f) is different from %f" % (self.sandbox('JSBout172B.csv'), fdm.get_property_value('ic/vt-kts'), vt0))
fdm.run_ic()
ExecuteUntil(fdm, 1.0)
mod = Table()
mod.ReadCSV(self.sandbox('JSBout172B.csv'))
for col, title in enumerate(mod._lines[0]):
if title == 'V_{Total} (ft/s)':
self.assertTrue(abs(mod._lines[1][col] - (vt0 / fpstokts)) < 1E-5,
msg="Modified script %s\nThe total velocity is %f. The value %f was expected" % (self.sandbox('JSBout172B.csv'), mod._lines[1][col], vt0 / fpstokts))
break
else:
self.fail("The total velocity is not exported in %s" % (sandbox('JSBout172B.csv'),))
class TestPitotAngle(unittest.TestCase):
def setUp(self):
self.sandbox = SandBox()
def tearDown(self):
self.sandbox.erase()
def test_CAS_ic(self):
script_name = 'Short_S23_3.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
# Add a Pitot angle to the Short S23
tree, aircraft_name, path_to_jsbsim_aircrafts = CopyAircraftDef(
script_path, self.sandbox)
metrics_tag = tree.getroot().find('./metrics')
pitot_tag = et.SubElement(metrics_tag, 'pitot_angle')
pitot_tag.attrib['unit'] = 'DEG'
pitot_tag.text = '5.0'
tree.write(
self.sandbox('aircraft', aircraft_name, aircraft_name + '.xml'))
# Read the CAS specified in the IC file
tree = et.parse(self.sandbox.elude(script_path))
use_element = tree.getroot().find('use')
IC_file = use_element.attrib['initialize']
tree = et.parse(
os.path.join(path_to_jsbsim_aircrafts, append_xml(IC_file)))
vc_tag = tree.getroot().find('./vc')
VCAS = float(vc_tag.text)
if 'unit' in vc_tag.attrib and vc_tag.attrib['unit'] == 'FT/SEC':
VCAS /= 1.68781
# Run the IC and check that the model is initialized correctly
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_script(script_path)
fdm.run_ic()
self.assertAlmostEqual(fdm.get_property_value('ic/vc-kts'),
VCAS,
delta=1E-7)
self.assertAlmostEqual(fdm.get_property_value('velocities/vc-kts'),
VCAS,
delta=1E-7)
def test_pitot_angle(self):
script_name = 'ball_chute.xml'
script_path = self.sandbox.path_to_jsbsim_file('scripts', script_name)
# Add a Pitot angle to the Cessna 172
tree, aircraft_name, path_to_jsbsim_aircrafts = CopyAircraftDef(
script_path, self.sandbox)
root = tree.getroot()
metrics_tag = root.find('./metrics')
pitot_tag = et.SubElement(metrics_tag, 'pitot_angle')
pitot_tag.attrib['unit'] = 'DEG'
pitot_tag.text = '5.0'
contact_tag = root.find('./ground_reactions/contact')
contact_tag.attrib['type'] = 'STRUCTURE'
tree.write(
self.sandbox('aircraft', aircraft_name, aircraft_name + '.xml'))
fdm = CreateFDM(self.sandbox)
fdm.set_aircraft_path('aircraft')
fdm.load_model('ball')
pitot_angle = float(pitot_tag.text) * math.pi / 180.
weight = fdm.get_property_value('inertia/weight-lbs')
spring_tag = contact_tag.find('./spring_coeff')
spring_coeff = float(spring_tag.text)
print "Weight=%d Spring=%d" % (weight, spring_coeff)
fdm.set_property_value('ic/h-sl-ft', weight / spring_coeff)
fdm.set_property_value('forces/hold-down', 1.0)
fdm.run_ic()
ExecuteUntil(fdm, 10.)
for i in xrange(36):
for j in xrange(-9, 10):
angle = math.pi * i / 18.0
angle2 = math.pi * j / 18.0
ca2 = math.cos(angle2)
fdm.set_property_value('atmosphere/wind-north-fps',
10. * math.cos(angle) * ca2)
fdm.set_property_value('atmosphere/wind-east-fps',
10. * math.sin(angle) * ca2)
fdm.set_property_value('atmosphere/wind-down-fps',
10. * math.sin(angle2))
fdm.run()
vg = fdm.get_property_value('velocities/vg-fps')
self.assertAlmostEqual(vg, 0.0, delta=1E-7)
vt = fdm.get_property_value('velocities/vt-fps')
self.assertAlmostEqual(vt, 10., delta=1E-7)
mach = vt / fdm.get_property_value('atmosphere/a-fps')
P = fdm.get_property_value('atmosphere/P-psf')
pt = P * math.pow(1 + 0.2 * mach * mach, 3.5)
psl = fdm.get_property_value('atmosphere/P-sl-psf')
rhosl = fdm.get_property_value('atmosphere/rho-sl-slugs_ft3')
A = math.pow((pt - P) / psl + 1.0, 1.0 / 3.5)
alpha = fdm.get_property_value('aero/alpha-rad')
beta = fdm.get_property_value('aero/beta-rad')
vc = math.sqrt(
7.0 * psl / rhosl *
(A - 1.0)) * math.cos(alpha + pitot_angle) * math.cos(beta)
self.assertAlmostEqual(
fdm.get_property_value('velocities/vc-kts'),
max(0.0, vc) / 1.68781,
delta=1E-7)
# FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
# details.
#
# You should have received a copy of the GNU General Public License along with
# this program; if not, see <http://www.gnu.org/licenses/>
#
import sys
from JSBSim_utils import CreateFDM, Table, SandBox
sandbox = SandBox('check_cases', 'orbit')
fdm = CreateFDM(sandbox)
fdm.load_script(sandbox.path_to_jsbsim_file('scripts', 'ball_orbit.xml'))
fdm.run_ic()
while fdm.run():
pass
ref, current = Table(), Table()
ref.ReadCSV(sandbox.elude(sandbox.path_to_jsbsim_file('logged_data', 'BallOut.csv')))
current.ReadCSV(sandbox('BallOut.csv'))
diff = ref.compare(current)
if not diff.empty():
print diff
sys.exit(-1) # Needed for 'make test' to report the test passed.
sandbox.erase()
class CheckOutputRate(unittest.TestCase):
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))
def tearDown(self):
del self.fdm
self.sandbox.erase()
def testOutputRate(self):
self.fdm.load_script(self.script_path)
# Check that the output is enabled by default
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"), 1.0)
# Check that the rate is consistent with the values extracted from the
# script and the aircraft definition
self.assertAlmostEqual(self.fdm.get_property_value("simulation/output/log_rate_hz"), self.rateHz, delta=1e-5)
self.fdm.run_ic()
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 2 lines in
# addition to the headers :
# 1. The initial conditions
# 2. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1], 0.0)
self.assertEqual(output.get_column(0)[2], self.rate * self.dt)
self.assertEqual(output.get_column(0)[2], self.fdm.get_property_value("simulation/sim-time-sec"))
def testDisablingOutput(self):
self.fdm.load_script(self.script_path)
# Disables the output during the initialization
self.fdm.set_property_value("simulation/output/enabled", 0.0)
self.fdm.run_ic()
self.fdm.set_property_value("simulation/output/enabled", 1.0)
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 1 line in
# addition to the headers :
# 1. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1], self.fdm.get_property_value("simulation/sim-time-sec"))
def testTrimRestoresOutputSettings(self):
self.fdm.load_script(self.script_path)
# Disables the output during the initialization
self.fdm.set_property_value("simulation/output/enabled", 0.0)
self.fdm.run_ic()
# Check that the output remains disabled even after the trim is
# executed
while self.fdm.get_property_value("simulation/sim-time-sec") < self.trim_date + 2.0 * self.dt:
self.fdm.run()
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"), 0.0)
# Re-enable the output and check that the output rate is unaffected by
# the previous operations
self.fdm.set_property_value("simulation/output/enabled", 1.0)
frame = int(self.fdm.get_property_value("simulation/frame"))
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# The frame at which the data is logged must be the next multiple of
# the output rate
self.assertEqual(int(output.get_column(0)[1] / self.dt), (1 + frame / self.rate) * self.rate)
def testDisablingOutputInScript(self):
property = et.SubElement(self.run_tag, "property")
property.text = "simulation/output/enabled"
property.attrib["value"] = "0.0"
self.tree.write(self.sandbox("c1722_0.xml"))
self.fdm.load_script("c1722_0.xml")
# Check that the output is disabled
self.assertEqual(self.fdm.get_property_value("simulation/output/enabled"), 0.0)
self.fdm.run_ic()
self.fdm.set_property_value("simulation/output/enabled", 1.0)
for i in xrange(self.rate):
self.fdm.run()
output = Table()
output.ReadCSV(self.output_file)
# According to the settings, the output file must contain 1 line in
# addition to the headers :
# 1. The output after 'rate' iterations
self.assertEqual(output.get_column(0)[1], self.fdm.get_property_value("simulation/sim-time-sec"))
