548 results about "Control test" patented technology

A selection method and related application is provided for a framework-based application having programming applications with both language program files and configuration files. In one embodiment, the method comprises abstracting a frame configuration model instance by analyzing configuration files prior to any modifications made to the program. The frame configuration model instance denoting individual configuration nodes in the framework model and further defining relationship between one or more code units in the configuration nodes and program code units in the application. Then one or more control test cases are constructed by profiling select test cases of the application, wherein the control flow consists of code units traversed during test case execution and control flow of said code units. Subsequently, an extended control flow is obtained by correlating configuration nodes in the framework configuration model instance with the code units in said control flow.

The invention provides a flight environment simulation system. The system comprises a core calculating module, a signal acquisition module and an input/output module, wherein the core calculating module is used to calculate simulation data; the signal acquisition module is used to provide the data signals of an external device to the core calculating module; the signal acquisition module containsan avionics system test-bed signal acquisition device and an engine control test-bed signal acquisition device and/or an iron-bird test-bed signal acquisition device; and the input/output module is used to input instructions in the core calculating module or output the simulation data calculated by the core calculating module. By adopting the system of the invention, the system can be combined with the real device or high-accuracy simulation device of the aircraft selectively according to the test requirement, thus real data signals or data signals which are very close to the real data signals can be utilized to simulate a special flight environment and the accuracy of the flight environment simulation system can be effectively increased.

A process and laser system for in vitro and in vivo pain research, pain clinical testing and pain management. In preferred embodiments of the present invention a diode laser operating at a 980 nm wavelength is used to produce warmth, tickling, itching, touch, burning, hot pain or pin-prick pain. The device and methods can be used for stimulation of a single nerve fiber, groups of nerve fibers, nerve fibers of single type only as well as more the one type of nerve fibers simultaneously. The present invention is especially useful for research of human/animal sensitivity, pain management, drug investigation and testing, and psychophysiology/electrophysiology studies. The device and methods permit non-contact, reproducible and controlled tests that avoid risk of skin damage. Applicant an his fellow workers have shown that tests with human subjects with the process and laser of the present invention correlate perfectly with laboratory tests with nerve fibers of rats. The device and the methods can be applied in a wide variety of situations involving the study and treatment of pain. Preferred embodiments of the present invention provide laser systems and techniques that permit mapping and single mode activation of C fibers and A-delta fibers.

The invention relates to a universal satellite ground overall control test system, which consists of a front-end photoelectric conversion module, a measurement and control front-end equipment module, a central processing unit module, a display terminal module and a console module, wherein the front-end photoelectric conversion module is an external hardware interface of the ground overall controltest system and a tested system, and is internally connected with the measurement and control front-end equipment module; the measurement and control front-end equipment module finishes data interaction with the front-end photoelectric conversion module, and a rear end communicates with the central processing unit module and the console module; the central processing unit module receives downlinktelemetry data from the measurement and control front-end equipment module, finishes classifying and storing the data, forwards the data to the display terminal module, and simultaneously, is required to finish storing the uplink remote control information of the console module; the display terminal module receives the telemetry data from the central processing unit module, and finishes work in areal-time analysis way and a delay analysis way; and the console module transmits an uplink remote control instruction to the measurement and control front-end equipment module, and forwards uplink instruction information to the central processing unit module for filing.

The invention discloses a general rapid intelligent charger and a charging method thereof, mainly comprising a power module, a battery test analysis module, a charging parameter regulation and dynamic control module, an integrated control test module, a charging module and an indication module. Adopting a single chip as a control unit, the charger incorporates four storage battery charging control processes of pre-charging control, rapid charging control, supplementary charging control and trickle charging control to realize the whole process control of charging execution circuit, thus greatly improving the charging effect and effectively prolonging the actual life of battery. The charger can also identify different battery types, adjust the charging procedures of the controller according to the optimum charging curve automatically and charge different types of storage batteries.

A method for testing audio device includes setting at least one test mode according to test mode supported by tested audio device, controlling tested audio device to make ergodic on each test mode, processing input audio signal of tested audio device to obtain output audio signal under each test mode, carrying out waveform comparison on input and output audio signals under each test mode and obtaining test result of tested audio device at each test mode according to waveform comparison result. The system and audio device both being used for realizing said method is also disclosed.

The present invention discloses a system to test performance of gas sensors or semiconductor elements, which comprises a gas supply unit to provide gas of controllable concentration and even mixing for performance test of gas sensor sensitivity and discharge test gas upon completion of the test for gas sensor sensitivity, a heating unit to control test temperature and meet demands of performance test of gas sensors or semiconductor elements for different temperature conditions, a test unit to test voltage characteristic variation of the gas sensor or the semiconductor element in test gas of different temperatures and concentrations to realize test for performance of the gas sensor or semiconductor element. The present invention fulfills test for sensitivity performance of the gas sensor and electric performance of the semiconductor element at high temperature and meets demands for research and test of gas sensors and semiconductor elements.

The invention relates to a test platform and method for simulating intelligent flexible space panel structure vibration active control. The test platform includes a mechanical clamping device, a vibration flexible plate, a signal generator, a high-performance DSP board, an oscillator, a computer, a display device, a vibrator, a plurality of charge amplifier, a plurality of low-pass filter, a plurality of piezoelectric power amplifier, a piezoelectric plate sensing network and a piezoelectric driving network. The invention which uses piezoelectric ceramic element as basic materials of sensor network and driver network, DSP measuring element as core of signal detection, arithmetic operation and output control signal, PC machine as test control platform and observing interface provides a test platform and test method based on analog piezoelectric intelligent flexible space panel structure vibration active control research.

A test access circuit (TAC) for use in controlling test resources including child test access circuits (TACs) and/or test controllers, in an integrated circuit, comprises an enable input for enabling or disabling access to the test resources, a test port associated with each test resource, each test port including a test port enable output for connection to an enable input of an associated test resource; and an input for receiving a serial output of the associated test resource; and means for selecting a test resource for communication therewith.

The invention relates to a sealed bearing comprehensive performance simulation testing machine and belongs to the field of bearing performance testing. The sealed bearing comprehensive performance simulation testing machine comprises a bearing test unit, a driving unit, a loading unit, an environment simulation system and a control system. The bearing test unit is arranged in the environment box of the environment simulation system, is arranged on the same plate with the driving unit, and is connected with the loading unit. The driving unit is arranged on the left side of the environment box. The loading unit comprises a radial loading mechanism and an axial loading mechanism. The environment simulation system comprises the environment box, a high-temperature simulation unit, a low-temperature simulation unit, a humidity simulation unit and a dust simulation unit. The control system is connected with the driving unit, the loading unit, and the environment simulation system, and controls test rotating speed, test load, test ambient temperature, and test ambient humidity, and test environment dust concentration. The sealed bearing comprehensive performance simulation testing machine is reasonable in structure, complete in simulated working conditions, good in test results, and easy to operate, and satisfies the evaluation demands of sealed bearing comprehensive performance.

The invention provides a megawatt wind power generation adjustable blade bearing friction moment numerical control testing machine and a testing method. The tested bearing outer ring is fixed on the machine rack; a main axis is equipped, one end of the bearing inner ring is fixed on the bearing inner ring, the other end is equipped with a radial and axial loading mechanism, in which the radial and axial load cylinder are separately pressured, and is equipped with variable-frequency motor of torque sensor, the driving pinion is meshed with the tested bearing inner ring, which form the loading and transmission system. The testing machine is determined by force analysis and analog loading principle, which is reasonable and reliable, and has simple structure and small size. The closed-loop numerical control system, which is composed of an industrial computer, a hydraulic pressure control member, a hydro cylinder, a feedback element and other components, can realize overall monitor, data collection, analysis, process, and number and graph double output; the size, direction, variation period of the load are accurate, the curves of the load output and friction torque are intuitive, the testing process is highly automatic. And the invention can be matched with manual adjustment. The machine is shutdown automatically if any failure happens. The test provides data support for the bearing wind turbines, which assures that the machine can meet the test need after loading.

The invention relates to a performance testing device and method for seawater hydraulic pump in deep sea high back pressure environment. The performance testing device mainly comprises a deep sea stimulation cabin, a pressurizing system, a circulating water cooling pipeline, and a monitoring and controlling system; the deep sea stimulation cabin provides back pressures to be borne in environments at different water depths for the performance test of the seawater hydraulic pump through the pressurizing system; stimulation load of the seawater hydraulic pump is freely adjusted by a high-pressure flow control valve which is mounted in the circulating water cooling pipeline; the circulating water cooling pipeline can prevent temperature rise of water in the cabin caused by transformation of the hydraulic energy generated by the working seawater hydraulic pump to the heat energy after the high-pressure flow control valve is uploaded; the monitoring and controlling system can control test working conditions of the seawater hydraulic pump and acquire test parameters such as temperature, pressure and flow. The testing device can stimulate the back pressure environment at an appointed sea depth and realize performance test on the seawater hydraulic pump.

The invention provides a testing device and a method applicable for spacecraft high-stability pointing control. The testing device comprises a base, an air bearing, an instrument platform, a spacecraft pointing unit, a spacecraft attitude control unit, a platform data instruction transmitting-receiving system, a mark point, a target measuring head unit, a reflection prism, a counteractive momentum wheel system, an image processing unit, a photoelectric auto-collimator, a laser tracker, an off-platform data instruction transmitting-receiving system and a camera. According to the device and the method, the characteristics of a micro-interference moment environment are simulated by fully using the air bearing; as the high-precision position and attitude measuring techniques of equipment such as the image measuring unit, the laser tracker and the photoelectric auto-collimator are combined, the goal of spacecraft high-stability pointing control test can be realized; the precision is high; the stability is good; and the engineering realization is facilitated. The device and the method can be used for a high-precision pointing control test on spacecraft such as various high-precision weather and military reconnaissance satellites and space-based offense and defense platforms.

The invention discloses a system and a method of testing a micromotion contact resistance. The system comprises a microchecker unit, a micromotion contact resistance test unit, a data acquisition unit and a computer unit. The method has the following steps that a test micromotion contact resistance system is started for initialization, and the micromotion and control command parameter information is set in the computer unit and sent to the microchecker unit; the microchecker unit carries out micromotion according to the received micromotion and control command parameter information and adjusts the micromotion amplitude according to the self-formed micromotion feedback information; the micromotion contact resistance test unit carries out contact resistance test for a connector contact pair in micromotion, and the data acquisition unit samples the contact voltage signal and outputs the sampled signal to the computer unit for data storage, processing and graphic display. The system and the method of measuring a micromotion contact resistance are capable of regulating and controlling test parameters according to requirements, widening the test channel of the micromotion contact resistance and improving the accuracy of micromotion contact resistance test.

The invention relates to a multi-functional and one-stop type remote control design, the simulation system and method thereof wherein the system comprises: a first remote operation control station, a second remote operation control station, a system general control station, a high-dimensional dynamic simulation server, a rigid mechanical arm, a joint control computer, a virtual reality 3D simulation and video acquisition server, a flexible mechanical arm, another joint control computer, a visual system and a circular screen. The invention can work in four modes: mathematic simulation tests based on manual simulation manual remote control, simulation tests based on the manual remote operation control of mechanical arms on real ground, space robot capturing the inserted collision dynamics and control tests, and performance verification of flexible mechanical arms and the flexible parameter identifying tests. According to the invention, one-stop solutions can be provided to the design, simulation and test of remote operation control.

An integrated circuit including operational circuitry operable in response to at least one control signal asserted to an external node from an external source, and test circuitry coupled to the external node and the operational circuitry. In response to data asserted to the external node from an external source, the test circuitry enters a test mode in which it tests, configures, or reconfigures the operational circuitry. The test circuitry also asserts to the operational circuitry each control signal received at the external node (or an amplified or translated version thereof). Other aspects of the invention include test circuitry for use in a circuit having an access node and methods for performing on-chip testing, configuration, and control of operational circuitry within a chip in response to test data and at least one control signal asserted from an external source to an external node.

The invention provides a hub motor driving automobile integrative design and cooperative control test platform and an implementation method. The platform comprises a whole vehicle control system, an active distributed driving system, an EMB electronic mechanical braking system, an active steering system, a power battery pack, a battery management system, a whole vehicle frame structure and a suspension module; the whole vehicle control system comprises a whole vehicle controller, a control mechanism sensor and a communication system; the active distributed driving system comprises four motor controllers, four hub motors, four wheels, an accelerator pedal and a hub motor sensor; the EMB electronic mechanical braking system comprises an EMB controller, four EMB brakes, a brake pedal sensor,a wheel cylinder pressure sensor and an EMMB brake angle and displacement sensor; the active steering system comprises a steering system control mechanism, a steering execution structure, a steering controller, and a steering knuckle angle and torque sensor. The whole vehicle frame is simple in structure, simple in process and high in expansibility.

The invention discloses an automatic nonstandard control testing method and device and belongs to the field of computers. The automatic nonstandard control testing method includes acquiring an image user interface image of a nonstandard control to be tested of software to be tested in advance; determining the practical display position of the image user interface image of the nonstandard control to be tested in a current screen according to the image user interface image of the nonstandard control to be tested acquired in advance; simulating users to operate the image user interface image of the nonstandard control to be tested at the practical display position so as to test the nonstandard control to be tested. The automatic nonstandard control testing device comprises an acquiring module, a determining module and a simulating module. The automatic nonstandard control testing method and device can save resources.

In one example of the invention a patient display is provided on which a fixation graphic or video is shown in substantially the centre of the display, and then target graphics or video are shown at different positions on the display about the centre. A test subject is positioned in front of the patient display a known distance therefrom, and a camera captures an image of the test subject's eyes, to allow gaze direction determination to be performed. The captured images are displayed to a clinician user by a controlling test application, the clinician making a determination based on the images as to whether the test subject saw a target graphic or video when it was displayed. The clinician user then makes an appropriate input into the controlling test application, which also logs the position at which the target image was displayed. By displaying target graphics at multiple locations on the screen and logging the clinician inputs, the controlling test application is able to build up a plot of the peripheral vision field of the test subject. This plot can then be graphically displayed to the clinician user, and stored with the test results for future clinical use.

The invention discloses an automatic confirmation testing method and system for embedded software. The testing method comprises the following steps that: customizing a testing process, managing testing data, parsing the testing process, analyzing tested software, analyzing a testing result, carrying out network communication, controlling a testing interface, controlling a testing time sequence and reading tested platform software environment. The testing system comprises a testing process customization module, a testing data management module, a testing process parsing module, a tested software analyzer, a testing result analysis module, a network communication module, a testing interface control module, a testing time sequence control module and a tested platform software environment reader. By use of the method, the problems of the accurate input of a test case and the real-time collection of the output of tested software in an embedded software testing process are solved, the operation situation of the tested software is tracked under a situation that the code bloat rate of the tested software is almost not changed, and a full-automatic and visual corresponding relational graph of the test case and the operation situation of the tested software can be provided for testing personnel.

The invention discloses a batch testing method for finished products of bluetooth earphones, aiming to provide a batch testing method for finished products of bluetooth earphones with high test efficiency and favorable for the batch production of bluetooth earphones. The computer controls the scanning device to scan the bluetooth address of the bluetooth headset, and controls the automatic pairing and automatic connection of the bluetooth adapter and the bluetooth headset according to the scanned bluetooth address; automatically controls the artificial mouth and the artificial ear to the speaker output frequency of the bluetooth headset through the test computer. Test the sound and echo sound; output the test result and display it. The invention also discloses a batch testing system for finished products of bluetooth earphones. The invention can be used for batch testing of finished products of bluetooth earphones.