本文整理汇总了Python中cfclient.ui.widgets.ai.AttitudeIndicator.setHover方法的典型用法代码示例。如果您正苦于以下问题：Python AttitudeIndicator.setHover方法的具体用法？Python AttitudeIndicator.setHover怎么用？Python AttitudeIndicator.setHover使用的例子？那么, 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类cfclient.ui.widgets.ai.AttitudeIndicator的用法示例。
在下文中一共展示了AttitudeIndicator.setHover方法的4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: FlightTab
# 需要导入模块: from cfclient.ui.widgets.ai import AttitudeIndicator [as 别名]
# 或者: from cfclient.ui.widgets.ai.AttitudeIndicator import setHover [as 别名]
#.........这里部分代码省略.........
def uiSetupReady(self):
flightComboIndex = self.flightModeCombo.findText(
Config().get("flightmode"), Qt.MatchFixedString)
if (flightComboIndex < 0):
self.flightModeCombo.setCurrentIndex(0)
self.flightModeCombo.currentIndexChanged.emit(0)
else:
self.flightModeCombo.setCurrentIndex(flightComboIndex)
self.flightModeCombo.currentIndexChanged.emit(flightComboIndex)
def _logging_error(self, log_conf, msg):
QMessageBox.about(self, "Log error", "Error when starting log config"
" [%s]: %s" % (log_conf.name, msg))
def _motor_data_received(self, timestamp, data, logconf):
if self.isVisible():
self.actualM1.setValue(data["motor.m1"])
self.actualM2.setValue(data["motor.m2"])
self.actualM3.setValue(data["motor.m3"])
self.actualM4.setValue(data["motor.m4"])
def _baro_data_received(self, timestamp, data, logconf):
if self.isVisible():
self.actualASL.setText(("%.2f" % data["baro.aslLong"]))
self.ai.setBaro(data["baro.aslLong"])
def _althold_data_received(self, timestamp, data, logconf):
if self.isVisible():
target = data["altHold.target"]
if target>0:
if not self.targetASL.isEnabled():
self.targetASL.setEnabled(True)
self.targetASL.setText(("%.2f" % target))
self.ai.setHover(target)
elif self.targetASL.isEnabled():
self.targetASL.setEnabled(False)
self.targetASL.setText("Not set")
self.ai.setHover(0)
def _imu_data_received(self, timestamp, data, logconf):
if self.isVisible():
self.actualRoll.setText(("%.2f" % data["stabilizer.roll"]))
self.actualPitch.setText(("%.2f" % data["stabilizer.pitch"]))
self.actualYaw.setText(("%.2f" % data["stabilizer.yaw"]))
self.actualThrust.setText("%.2f%%" %
self.thrustToPercentage(
data["stabilizer.thrust"]))
self.ai.setRollPitch(-data["stabilizer.roll"],
data["stabilizer.pitch"])
def connected(self, linkURI):
# IMU & THRUST
lg = LogConfig("Stabilizer", Config().get("ui_update_period"))
lg.add_variable("stabilizer.roll", "float")
lg.add_variable("stabilizer.pitch", "float")
lg.add_variable("stabilizer.yaw", "float")
lg.add_variable("stabilizer.thrust", "uint16_t")
try:
self.helper.cf.log.add_config(lg)
lg.data_received_cb.add_callback(self._imu_data_signal.emit)
lg.error_cb.add_callback(self._log_error_signal.emit)
lg.start()
except KeyError as e:
logger.warning(str(e))示例2: FlightTab
# 需要导入模块: from cfclient.ui.widgets.ai import AttitudeIndicator [as 别名]
# 或者: from cfclient.ui.widgets.ai.AttitudeIndicator import setHover [as 别名]
#.........这里部分代码省略.........
return ((thrust / MAX_THRUST) * 100.0)
def uiSetupReady(self):
flightComboIndex = self.flightModeCombo.findText(
GuiConfig().get("flightmode"), Qt.MatchFixedString)
if (flightComboIndex < 0):
self.flightModeCombo.setCurrentIndex(0)
self.flightModeCombo.currentIndexChanged.emit(0)
else:
self.flightModeCombo.setCurrentIndex(flightComboIndex)
self.flightModeCombo.currentIndexChanged.emit(flightComboIndex)
def _logging_error(self, log_conf, msg):
QMessageBox.about(self, "Log error", "Error when starting log config"
" [%s]: %s" % (log_conf.getName(), msg))
def _motor_data_received(self, data, timestamp):
self.actualM1.setValue(data["motor.m1"])
self.actualM2.setValue(data["motor.m2"])
self.actualM3.setValue(data["motor.m3"])
self.actualM4.setValue(data["motor.m4"])
self.motor_power = data["motor.m1"] + data["motor.m2"] + data["motor.m3"] + data["motor.m4"]
def _baro_data_received(self, data, timestamp):
self.actualASL.setText(("%.2f" % data["baro.aslLong"]))
self.ai.setBaro(data["baro.aslLong"])
def _althold_data_received(self, data, timestamp):
target = data["altHold.target"]
if target>0:
if not self.targetASL.isEnabled():
self.targetASL.setEnabled(True)
self.targetASL.setText(("%.2f" % target))
self.ai.setHover(target)
elif self.targetASL.isEnabled():
self.targetASL.setEnabled(False)
self.targetASL.setText("Not set")
self.ai.setHover(0)
def _imu_data_received(self, data, timestamp):
self.aroll = data["stabilizer.roll"]
self.apitch = data["stabilizer.pitch"]
self.actualRoll.setText(("%.2f" % data["stabilizer.roll"]))
self.actualPitch.setText(("%.2f" % data["stabilizer.pitch"]))
self.actualYaw.setText(("%.2f" % data["stabilizer.yaw"]))
self.actualThrust.setText("%.2f%%" %
self.thrustToPercentage(
data["stabilizer.thrust"]))
self.ai.setRollPitch(-data["stabilizer.roll"],
data["stabilizer.pitch"])
def _heading_data_received(self, data, timestamp):
# hard and soft correction values generated by Processing Magnetometer_calibration script + calibrate_hardsoft.py
# magn_ellipsoid_center = [1341.66, -537.690, 41.1584]
# magn_ellipsoid_transform = [[0.934687, 0.0222809, 0.0151145], [0.0222809, 0.919365, -0.00622367], [0.0151145, -0.00622367, 0.996487]]
magn_ellipsoid_center = [-170.956, -1056.30, 19.4655]
magn_ellipsoid_transform = [[0.852266, 0.00526498, 0.0195745], [0.00526498, 0.888268, -0.00355351], [0.0195745, -0.00355351, 0.997333]]
# values generated by calibrate_powered.py
qx = [0.067946222436498283, -0.25034004667098259, 8.3336994198409666, -0.17762637163222378]
qy = [-0.13945102271766135, 2.9074808469097495, 1.6764850422889934, 0.19244505046927501]
qz = [0.018800599305554239, -0.79590273035713055, -3.1033531112103478, 0.13550993988096199]
# matrix by vector multiplication示例3: FlightTab
# 需要导入模块: from cfclient.ui.widgets.ai import AttitudeIndicator [as 别名]
# 或者: from cfclient.ui.widgets.ai.AttitudeIndicator import setHover [as 别名]
#.........这里部分代码省略.........
d.m2 = data["motor.m2"]
d.m3 = data["motor.m3"]
d.m4 = data["motor.m4"]
self.motor_pub.publish(d)
def _gyro_data_received(self, timestamp, data, logconf):
if self.isVisible():
d = GyroData()
d.x = data["gyro.x"]
d.y = data["gyro.y"]
d.z = data["gyro.z"]
self.gyro_pub.publish(d)
def _accel_data_received(self, timestamp, data, logconf):
if self.isVisible():
d = AccelData()
d.x = data["acc.x"]
d.y = data["acc.y"]
d.z = data["acc.z"]
self.acc_pub.publish(d)
def _baro_data_received(self, timestamp, data, logconf):
if self.isVisible():
self.actualASL.setText(("%.2f" % data["baro.aslLong"]))
self.ai.setBaro(data["baro.aslLong"])
def _althold_data_received(self, timestamp, data, logconf):
if self.isVisible():
target = data["altHold.target"]
if target>0:
if not self.targetASL.isEnabled():
self.targetASL.setEnabled(True)
self.targetASL.setText(("%.2f" % target))
self.ai.setHover(target)
elif self.targetASL.isEnabled():
self.targetASL.setEnabled(False)
self.targetASL.setText("Not set")
self.ai.setHover(0)
def _imu_data_received(self, timestamp, data, logconf):
if self.isVisible():
self.actualRoll.setText(("%.2f" % data["stabilizer.roll"]))
self.actualPitch.setText(("%.2f" % data["stabilizer.pitch"]))
self.actualYaw.setText(("%.2f" % data["stabilizer.yaw"]))
self.actualThrust.setText("%.2f%%" %
self.thrustToPercentage(
data["stabilizer.thrust"]))
self.ai.setRollPitch(-data["stabilizer.roll"],
data["stabilizer.pitch"])
d = StabData()
d.pitch = data["stabilizer.pitch"]
d.roll = data["stabilizer.roll"]
d.yaw = data["stabilizer.yaw"]
self.stab_pub.publish(d)
def connected(self, linkURI):
# IMU & THRUST
lg = LogConfig("Stabalizer", GuiConfig().get("ui_update_period"))
lg.add_variable("stabilizer.roll", "float")
lg.add_variable("stabilizer.pitch", "float")
lg.add_variable("stabilizer.yaw", "float")
lg.add_variable("stabilizer.thrust", "uint16_t")
self.helper.cf.log.add_config(lg)
if (lg.valid):示例4: FlightTab
# 需要导入模块: from cfclient.ui.widgets.ai import AttitudeIndicator [as 别名]
# 或者: from cfclient.ui.widgets.ai.AttitudeIndicator import setHover [as 别名]
#.........这里部分代码省略.........
GuiConfig().get("flightmode"), Qt.MatchFixedString)
if (flightComboIndex < 0):
self.flightModeCombo.setCurrentIndex(0)
self.flightModeCombo.currentIndexChanged.emit(0)
else:
self.flightModeCombo.setCurrentIndex(flightComboIndex)
self.flightModeCombo.currentIndexChanged.emit(flightComboIndex)
def _logging_error(self, log_conf, msg):
QMessageBox.about(self, "Log error", "Error when starting log config"
" [%s]: %s" % (log_conf.name, msg))
def _motor_data_received(self, timestamp, data, logconf):
self.motor_power = data["motor.m1"] + data["motor.m2"] + data["motor.m3"] + data["motor.m4"]
if self.isVisible():
self.actualM1.setValue(data["motor.m1"])
self.actualM2.setValue(data["motor.m2"])
self.actualM3.setValue(data["motor.m3"])
self.actualM4.setValue(data["motor.m4"])
def _baro_data_received(self, timestamp, data, logconf):
self.helper.inputDeviceReader.setCurrentAltitude(data["baro.aslLong"])
if self.isVisible():
self.actualASL.setText(("%.2f" % data["baro.aslLong"]))
self.ai.setBaro(data["baro.aslLong"])
def _althold_data_received(self, timestamp, data, logconf):
if self.isVisible():
target = data["altHold.target"]
if target > 0:
if not self.targetASL.isEnabled():
self.targetASL.setEnabled(True)
self.targetASL.setText(("%.2f" % target))
self.ai.setHover(target)
elif self.targetASL.isEnabled():
self.targetASL.setEnabled(False)
self.targetASL.setText("Not set")
self.ai.setHover(0)
def _imu_data_received(self, timestamp, data, logconf):
self.aroll = data["stabilizer.roll"]
self.apitch = data["stabilizer.pitch"]
if self.isVisible():
self.actualRoll.setText(("%.2f" % data["stabilizer.roll"]))
self.actualPitch.setText(("%.2f" % data["stabilizer.pitch"]))
self.actualYaw.setText(("%.2f" % data["stabilizer.yaw"]))
self.actualThrust.setText("%.2f%%" %
self.thrustToPercentage(
data["stabilizer.thrust"]))
self.ai.setRollPitch(-data["stabilizer.roll"],
data["stabilizer.pitch"])
self.compass.setAngle(-data["stabilizer.yaw"])
# self.helper.cf.commander.setActualPoint(data)
def _mag_data_received(self, timestamp, data, logconf):
# hard and soft correction values generated by Processing Magnetometer_calibration script + calibrate_hardsoft.py
magn_ellipsoid_center = [1341.66, -537.690, 41.1584]
magn_ellipsoid_transform = [[0.934687, 0.0222809, 0.0151145], [0.0222809, 0.919365, -0.00622367], [0.0151145, -0.00622367, 0.996487]]
# values generated by calibrate_powered.py
qx = [0.067946222436498283, -0.25034004667098259, 8.3336994198409666, -0.17762637163222378]
qy = [-0.13945102271766135, 2.9074808469097495, 1.6764850422889934, 0.19244505046927501]
qz = [0.018800599305554239, -0.79590273035713055, -3.1033531112103478, 0.13550993988096199]
# matrix by vector multiplication