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Python CreateFDM.get_property_manager方法代码示例

本文整理汇总了Python中JSBSim_utils.CreateFDM.get_property_manager方法的典型用法代码示例。如果您正苦于以下问题:Python CreateFDM.get_property_manager方法的具体用法?Python CreateFDM.get_property_manager怎么用?Python CreateFDM.get_property_manager使用的例子?那么恭喜您, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在JSBSim_utils.CreateFDM的用法示例。


在下文中一共展示了CreateFDM.get_property_manager方法的5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: testFunctionWithIndexedProps

# 需要导入模块: from JSBSim_utils import CreateFDM [as 别名]
# 或者: from JSBSim_utils.CreateFDM import get_property_manager [as 别名]
    def testFunctionWithIndexedProps(self):
        tree = et.parse(self.sandbox.path_to_jsbsim_file('engine',
                                                         'eng_PegasusXc.xml'))
        # Define the function starter-max-power-W as a 'post' function
        root = tree.getroot()
        startPowFunc_tag = root.find("function/[@name='propulsion/engine[#]/starter-max-power-W']")
        startPowFunc_tag.attrib['type']='post'
        tree.write('eng_PegasusXc.xml')

        # Copy the propeller file.
        shutil.copy(self.sandbox.path_to_jsbsim_file('engine', 'prop_deHavilland5000.xml'),
                    '.')
        fdm = CreateFDM(self.sandbox)
        fdm.set_engine_path('.')
        fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts',
                                                         'Short_S23_1.xml'))
        fdm.run_ic()
        pm = fdm.get_property_manager()
        self.assertTrue(pm.hasNode('propulsion/engine[0]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[1]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[2]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[3]/starter-max-power-W'))

        while fdm.run():
            rpm = [fdm['propulsion/engine[0]/engine-rpm'],
                   fdm['propulsion/engine[1]/engine-rpm'],
                   fdm['propulsion/engine[2]/engine-rpm'],
                   fdm['propulsion/engine[3]/engine-rpm']]
            for i in range(4):
                maxPower = max(0.0, 1.0-rpm[i]/400)*498.941*0.10471976*rpm[i]
                self.assertAlmostEqual(fdm['propulsion/engine[%d]/starter-max-power-W' % (i,)],
                                       maxPower)
开发者ID:agodemar,项目名称:jsbsim,代码行数:34,代码来源:TestEngineIndexedProps.py

示例2: testEnginePowerVC

# 需要导入模块: from JSBSim_utils import CreateFDM [as 别名]
# 或者: from JSBSim_utils.CreateFDM import get_property_manager [as 别名]
    def testEnginePowerVC(self):
        fdm = CreateFDM(self.sandbox)
        fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts',
                                                         'L4102.xml'))
        fdm.run_ic()
        pm = fdm.get_property_manager()
        self.assertTrue(pm.hasNode('propulsion/engine[0]/EnginePowerVC'))
        self.assertTrue(pm.hasNode('propulsion/engine[1]/EnginePowerVC'))

        while fdm.run():
            self.assertAlmostEqual(fdm['propulsion/engine[0]/EnginePowerVC'],
                                   fdm['propulsion/engine[1]/EnginePowerVC'])
开发者ID:agodemar,项目名称:jsbsim,代码行数:14,代码来源:TestEngineIndexedProps.py

示例3: steerType

# 需要导入模块: from JSBSim_utils import CreateFDM [as 别名]
# 或者: from JSBSim_utils.CreateFDM import get_property_manager [as 别名]
    def steerType(self, hasSteerPosDeg, hasSteeringAngle, hasCastered):
        self.tree.write(self.sandbox('aircraft', self.aircraft_name,
                                     self.aircraft_name+'.xml'))

        fdm = CreateFDM(self.sandbox)
        fdm.set_aircraft_path('aircraft')
        fdm.load_script(self.script_path)
        fdm.run_ic()
        pm = fdm.get_property_manager()
        self.assertTrue(pm.hasNode('fcs/steer-pos-deg') == hasSteerPosDeg)
        self.assertTrue(pm.hasNode('gear/unit/steering-angle-deg')
                        == hasSteeringAngle)
        self.assertTrue(pm.hasNode('gear/unit/castered') == hasCastered)

        return fdm
开发者ID:Outerra,项目名称:jsbsim,代码行数:17,代码来源:TestLGearSteer.py

示例4: testTableWithIndexedVars

# 需要导入模块: from JSBSim_utils import CreateFDM [as 别名]
# 或者: from JSBSim_utils.CreateFDM import get_property_manager [as 别名]
    def testTableWithIndexedVars(self):
        tree = et.parse(self.sandbox.path_to_jsbsim_file('engine',
                                                         'eng_PegasusXc.xml'))
        # Define the function starter-max-power-W as a 'post' function
        root = tree.getroot()
        startPowFunc_tag = root.find("function/[@name='propulsion/engine[#]/starter-max-power-W']")
        startPowFunc_tag.attrib['type']='post'
        max_tag = startPowFunc_tag.find('product/max')
        diff_tag = max_tag.find('difference')
        max_tag.remove(diff_tag)
        table_tag = et.SubElement(max_tag,'table')
        table_tag.attrib['name']='propulsion/engine[#]/starter-tabular-data'
        indepVar_tag = et.SubElement(table_tag, 'independentVar')
        indepVar_tag.attrib['lookup']='row'
        indepVar_tag.text = 'propulsion/engine[#]/engine-rpm'
        tData_tag = et.SubElement(table_tag, 'tableData')
        tData_tag.text ='0.0 1.0\n400.0 0.0'
        tree.write('eng_PegasusXc.xml')

        # Copy the propeller file.
        shutil.copy(self.sandbox.path_to_jsbsim_file('engine', 'prop_deHavilland5000.xml'),
                    '.')
        fdm = CreateFDM(self.sandbox)
        fdm.set_engine_path('.')
        fdm.load_script(self.sandbox.path_to_jsbsim_file('scripts',
                                                         'Short_S23_1.xml'))
        fdm.run_ic()
        pm = fdm.get_property_manager()
        self.assertTrue(pm.hasNode('propulsion/engine[0]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[1]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[2]/starter-max-power-W'))
        self.assertTrue(pm.hasNode('propulsion/engine[3]/starter-max-power-W'))

        while fdm.run():
            rpm = [fdm['propulsion/engine[0]/engine-rpm'],
                   fdm['propulsion/engine[1]/engine-rpm'],
                   fdm['propulsion/engine[2]/engine-rpm'],
                   fdm['propulsion/engine[3]/engine-rpm']]
            for i in range(4):
                tabularData = max(0.0, 1.0-rpm[i]/400)
                maxPower = tabularData*498.941*0.10471976*rpm[i]
                self.assertAlmostEqual(fdm['propulsion/engine[%d]/starter-max-power-W' % (i,)],
                                       maxPower)
                self.assertAlmostEqual(fdm['propulsion/engine[%d]/starter-tabular-data' % (i,)],
                                       tabularData)
开发者ID:agodemar,项目名称:jsbsim,代码行数:47,代码来源:TestEngineIndexedProps.py

示例5: test_property_access

# 需要导入模块: from JSBSim_utils import CreateFDM [as 别名]
# 或者: from JSBSim_utils.CreateFDM import get_property_manager [as 别名]
    def test_property_access(self):
        fdm = CreateFDM(self.sandbox)
        fdm.load_model('ball')
        fdm.run_ic()

        # Check that the node 'qwerty' does not exist
        pm = fdm.get_property_manager()
        self.assertFalse(pm.hasNode('qwerty'))

        # Check the default behavior of get_property_value. Non existing
        # properties return 0.0
        self.assertEqual(fdm.get_property_value('qwerty'), 0.0)

        # Verify that __getitem__ checks the existence and raises KeyError if
        # the property does not exist.
        with self.assertRaises(KeyError):
            x = fdm['qwerty']

        # Check that we can initialize a non existing property
        fdm['qwerty'] = 42.0
        self.assertAlmostEqual(fdm.get_property_value('qwerty'), 42.0)
        self.assertAlmostEqual(fdm['qwerty'], 42.0)

        del fdm
开发者ID:agodemar,项目名称:jsbsim,代码行数:26,代码来源:TestMiscellaneous.py


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