A measurement method and a measurement device for performing a measurement with respect to a frequency-converting device under test and compensating for a shifting frequency are provided. The measurement method comprises the steps of applying an input signal to an input of the device under test, receiving an output signal from an output of the device under test, converting the output signal into a digitized signal comprising digital samples, estimating a received frequency with respect to the output signal on the basis of the digital samples, and comparing the received frequency to an expected frequency.

A digital sampling oscilloscope (DSO) includes a housing, an analog measurement input interface arranged in a housing wall of the housing and a measurement acquisition system having a digitizer and an acquisition memory coupled to the digitizer. The measurement acquisition system is integrated into the housing and coupled to the analog measurement input interface. The DSO further includes a signal generator integrated into the housing. An operation mode control signal output interface is arranged in a housing wall of the housing. The signal generator is coupled to the operation mode control signal output interface and is configured to output an operation mode control signal to a device under test (DUT) connected to both the operation mode control signal output interface and the analog measurement input interface for controlling a test operation mode of the DUT.

A method for monitoring an FMCW radar sensor and an FMCW radar sensor, including multiple local oscillators. In the method, a first local oscillator signal of a first local oscillator of the local oscillators is mixed in a mixer with a second local oscillator signal of a second local oscillator of the local oscillators to form a baseband signal. The baseband signal is evaluated. A fault is detected due to a result of the evaluation. Methods for monitoring an FMCW radar sensor and an FMCW radar sensor including multiple high frequency components are described which each include a transceiver part for outputting a transmit signal to at least one antenna assigned to the high frequency component and for receiving a receive signal from at least one antenna assigned to the high frequency component.

A system and method for an aircraft includes a probe, first and second current sensors, and a control circuit. The probe includes a heater that includes a resistive heating element routed through the probe, wherein an operational current is provided to the resistive heating element to provide heating for the probe. The first current sensor is configured to sense a first current through the resistive heating element, and the second current sensor is configured to sense a second current through the resistive heating element. The control circuit is configured to determine a leakage current based on the first and second currents and determine a remaining useful life the probe based on the leakage current over time.

A steady-state voltage on an oscillator output can be detected, independent of control signals received from other circuitry, by an oscillator failure detection circuit (OFDC) fabricated within an integrated circuit (IC). The OFDC can, in response to detecting the steady-state voltage, output an oscillator failure signal on a reference fail output. The OFDC can receive, with a first and a second buffer, an oscillator output signal from an oscillator output. Through the use of an electrically interconnected, pull-down device, pull-up network, pull-up device, pull-down network, Schmitt trigger, inverting Schmitt trigger and OR-gate, the OFDC can drive the oscillator failure signal onto an output of the OR-gate electrically connected to a reference fail output (RFO).

A probe system configured to receive a radio-frequency (RF) signal from a radio-frequency (RF) antenna includes a heater and a control circuit. The heater includes a resistive heating element routed through the probe system. An operational voltage is provided to the resistive heating element to provide heating for the probe system and the resistive heating element has an element capacitance. The control circuit is configured to determine an antenna response of the resistive heating element and determine a remaining useful life of the probe system based on the antenna response over time.

Method and system for temperature-dependent frequency compensation. For example, the method for temperature-dependent frequency compensation includes determining a first frequency compensation as a first function of temperature using one or more crystal oscillators, processing information associated with the first frequency compensation as the first function of temperature, and determining a second frequency compensation for a crystal oscillator as a second function of temperature based on at least information associated with the first frequency compensation as the first function of temperature. The one or more crystal oscillators do not include the crystal oscillator, and the first frequency compensation as the first function of temperature is different from the second frequency compensation as the second function of temperature.

Method and system for temperature-dependent frequency compensation. For example, the method for temperature-dependent frequency compensation includes determining a first frequency compensation as a first function of temperature using one or more crystal oscillators, processing information associated with the first frequency compensation as the first function of temperature, and determining a second frequency compensation for a crystal oscillator as a second function of temperature based on at least information associated with the first frequency compensation as the first function of temperature. The one or more crystal oscillators do not include the crystal oscillator, and the first frequency compensation as the first function of temperature is different from the second frequency compensation as the second function of temperature.

A compact millimeter-wave slide screw impedance tuner allows reducing to a minimum the insertion loss between the tuner and the wafer-probe. The structure of the tuner uses a 1 mm slabline and adapters, an eccentrically rotating remotely controlled wideband tuning probe and a sliding rack on which the tuning-probe is attached; the position of the rack is controlled by a permanently anchored motorized pinion. The construction method allows for maximum compactness, needed in order to be able to attach the tuner directly on the wafer-probe and minimize the insertion loss, while maintaining key advantages of electro-mechanical tuners, such as robustness, linearity, simplicity, tuning resolution and calibration and compatibility with existing load pull software and technology.

Method and system for temperature-dependent frequency compensation. For example, the method for temperature-dependent frequency compensation includes determining a first frequency compensation as a first function of temperature using one or more crystal oscillators, processing information associated with the first frequency compensation as the first function of temperature, and determining a second frequency compensation for a crystal oscillator as a second function of temperature based on at least information associated with the first frequency compensation as the first function of temperature. The one or more crystal oscillators do not include the crystal oscillator, and the first frequency compensation as the first function of temperature is different from the second frequency compensation as the second function of temperature.