76 results about "General purpose software" patented technology

A method for automatically installing a software image onto an information handling system. The method includes reading an order for an information handling system, reading an image manifest, installing an image specified by the image manifest onto the information handing system as installed software, and automatically configuring the installed software.

A flight control computer system includes a plurality of computing channels (11, 21, and 31) where each computing channel further includes a main processor (113) and a monitor processor (114) under control of distinct operating systems. When the main processor and the monitor processor miscompare, cross-channel failure discretes (131) are transmitted to the other computing channels and a local generic fault discrete is armed. When the local generic fault discrete is armed and cross-channel failure discretes (141, 142) are received from the other computing channels, a program interrupt (133) is issued causing the main processor to execute a minimal fully tested ‘get home’ software package (150).

The invention discloses an industrial radio control system semi-physical security experiment platform. The platform comprises a simulation module, a controller host computer, a monitoring site, a programmable logic controller (PLC), an industrial radio communication device and a universal software radio peripheral (USRP) for simulating attacks. The simulation module is used for erecting a virtual controlled object and simulating different industrial scenes. The controller host computer is used for simulating different control algorithms. The monitoring site monitors in real time state signals, control signals and the like in a system operation process and stores correlation data in a database. The USRP is used for simulating a typical industrial radio attack mode. According to the experimental platform, through simulating a typical industrial object and a control algorithm, an attack on an industrial radio channel is simulated by use of the USRP, and the security of an industrial radio protocol and the control system performance under a typical attack are analyzed. The industrial radio control system semi-physical security experiment platform is low in system cost and can be applied to simulation of a typical industrial control object and a corresponding control algorithm and evaluation of the influence of a typical industrial radio attack on an industrial control system.

An information processing apparatus is disclosed, which is used while being incorporated in other device and provides a predetermined function to the other device in which the information processing apparatus is incorporated. The information processing apparatus includes first loading means for loading a general-purpose software which provides a general-purpose function to an execution environmental area and mounting the general-purpose software in a predetermined directory at the time of starting up a system; second loading means for loading a dedicated software which provides a function intrinsic to the other device to the execution environmental area and mounting the dedicated software in a predetermined directory at the time of starting up a system; and integrating means for integrating a first setting file containing general-purpose setting information which is included in the general-purpose software which is loaded by the first loading means and a second setting file containing general-purpose setting information which is included in the dedicated software which is loaded by the second loading means and reflects the presence of the dedicated software.

There is described a method and system for developing for an automation process a screen viewable on a target computer that has user interface objects. A development computer has a set of common design time components from a general purpose software development kit that also has a databinding facility and a set of customization components. Those components have an interface that allows access to the available for use automation process data objects and a process object picker that act as a user interface to the databinding facility to allow the browsing of a subset of the available for use data objects and selecting of one or more of the objects in the subset for binding by the databinding facility either to one or more members of the user interface objects or one or more of the user interface objects or a combination of the same.

There is described a method and system for developing for an automation process a screen viewable on a target computer that has user interface objects. A development computer has a set of common design time components from a general purpose software development kit that also has a databinding facility and a set of customization components. Those components have an interface that allows access to the available for use automation process data objects and a process object picker that act as a user interface to the databinding facility to allow the browsing of a subset of the available for use data objects and selecting of one or more of the objects in the subset for binding by the databinding facility either to one or more members of the user interface objects or one or more of the user interface objects or a combination of the same.

The invention belongs to the field of computer automatic testing, and provides an implementation method of a universal virtual instrument interface. In the method, a universal software interface layer is added between a common instrument driver and a application program, the application program is completely separated from the calling of the actual instrument, and a unified calling interface function and a universal software interface description file are defined, thereby replacing the instruments in the testing system under the conditions of not changing application program codes and not recompiling a source program; a testing software pack can adapt to the existing or even future testing systems composed of different types of instrument hardware and buses; and the testing codes can be transplanted to different instruments without being modified. In addition, the method can be used for realizing data communication functions among different software program modules.

Object oriented design strategies and patterns are applied to financial data processing systems for processing and modeling of financial products (also referred to as financial instruments) with an emphasis being on derivative products. The system employs valuation independent, well-defined financial components (also referred to as financial events) that can be combined to build new financial structures. A general purpose software model is provided for representing the structure and characteristics of these products. A declarative specification language is provided to describe financial instruments in a consistent manner that lends itself to processing in such an object oriented system. A general traversal process is provided that can be applied to the macro structure of a financial instrument to implement various functions that produce results based on such information, such as the stream of financial events associated with the instrument, or the pricing or valuation of the instrument. Techniques including double dispatch and other mechanisms are further provided to provide flexible means of associating the appropriate processing methods with the diverse range of instrument characteristics that are encountered in a typical financial institution's course of business.

A system of base station includes a common controller platform to integrate a controller specific softwares of at least two technologies, a common transport platform to integrate a transport specific softwares of at least two technologies, a common base station software to interface with the common controller platform and the common transport platform, a generic hardware to execute the common controller platform and the common transport platform, and a plurality of hardware specific API to interface and communicate between the common software base station and the generic hardware. The common base station software includes, a common controller interface module to generate communication between the plurality of hardware specific API and the common controller platform, and a common transport interface module to generate communication between the plurality of hardware specific API and the common transport platform.

The method is realized using general software. It comprises: starting up the test; establishing a link state routing protocol session with the tested device; getting the link state information; packaging the link state information as a link state message which is transmitted to the tested device in order to test the performance of the tested device.

A system and method provide for synchronous operation of linked command objects in a general purpose software application. The software application provides a user with a variety of operations that manipulate available data objects. The software application manages the data objects in a number of contexts. Each context manages the existence and execution of a number of command objects. Each command object operates on one or more data objects in its context. To support synchronous operations that affect the state of data objects in more than one context, command objects are linked to each other. When one command object is executed, the context of the command object identifies a command object linked to the executed command object and initiates the execution of the linked command object via the context that manages that command object. This synchronization allows for synchronous undo and redone operations. The delete states of the command objects are also synchronized. Deleting a command object destroys it, and prevents it from being undone. When one command object is deleted the command object linked thereto is also deleted, thereby preventing the linked command object from being independently undone resulting in an inconsistent state of the contexts.

The invention relates to a universal software installation system and a universal software installation method under Windows domain authority management. The system comprises an installation service end, n installation clients and a universal software installation platform. An installation user set is configured on the service end, thereby managing software installation users. The authority of the installation client is arranged in the client. A disposition mode of firstly mounting the service end and then mounting the client is adopted in the universal software installation platform. Unified disposition of all to-be-installed software is realized at the service end according to a universal software mounting platform rule in an installation strategy package manner. The installation clients perform application software installing, upgrading and uninstalling on a PC. The universal software installation system and the universal software installation method greatly simplify installing, upgrading and uninstalling on the PC. High convenience in use, concise structure and easy maintenance are realized. Furthermore the system and the method settle the problems of high safety risk and high workload in software installing in a current Windows domain environment.

An integrated technology platform includes multiple hardware and software components that enable any application of autonomous agricultural equipment operation in an agricultural or other off-road setting, within a common software structural architecture. The integrated technology platform represents a technology stack that is a modular architecture that can be leveraged across multiple use cases and vehicle types. The integrated technology platform includes a vehicle interface component responsible for the physical interface to agricultural equipment, a telematics component that enables stable in-field communications between all aspects of the integrated technology platform, and a perception component that operates as a safety mechanism and includes object detection and classification. Additionally, a cloud-side application performs account management and field setup and as well as syncing of field equipment and operating systems in a common operating system. The integrated technology platform also includes an executive control layer that enables rapid porting from one platform to another, so that software applications in the integrated technology platform can work with hardware of any manufacture.

A system and method provide for synchronous operation of linked command objects in a general purpose software application. The software application provides a user with a variety of operations that manipulate available data objects. The software application manages the data objects in a number of contexts. Each context manages the existence and execution of a number of command objects. Each command object operates on one or more data objects in its context. To support synchronous operations that affect the state of data objects in more than one context, command objects are linked to each other. When one command object is executed, the context of the command object identifies a command object linked to the executed command object and initiates the execution of the linked command object via the context that manages that command object. This synchronization allows for synchronous undo and redone operations. The delete states of the command objects are also synchronized. Deleting a command object destroys it, and prevents it from being undone. When one command object is deleted the command object linked thereto is also deleted, thereby preventing the linked command object from being independently undone resulting in an inconsistent state of the contexts.

Disclosed is a software library reconstruction device which extracts program elements which are used for the execution of a function from among program elements which construct a general-purpose software library 2a, verifies whether or not an error is found in each of the program elements extracted thereby, optimizes a program comprised of program elements each of which the software library reconstruction device has verified does not have any error, and constructs a software library 2b which is customized to the function executed thereby by using the program elements of the program optimized thereby.

Object oriented design strategies and patterns are applied to financial data processing systems for processing and modeling of financial products (also referred to as financial instruments) with an emphasis being on derivative products. The system employs valuation independent, well-defined financial components (also referred to as financial events) that can be combined to build new financial structures. A general purpose software model is provided for representing the structure and characteristics of these products. A declarative specification language is provided to describe financial instruments in a consistent manner that lends itself to processing in such an object oriented system. A general traversal process is provided that can be applied to the macro structure of a financial instrument to implement various functions that produce results based on such information, such as the stream of financial events associated with the instrument, or the pricing or valuation of the instrument. Techniques including double dispatch and other mechanisms are further provided to provide flexible means of associating the appropriate processing methods with the diverse range of instrument characteristics that are encountered in a typical financial institution's course of business.

The invention relates to the technical field of software deployment, and discloses a software remote deployment management method and a system, and the method comprises the following steps: obtaininga configuration file of to-be-installed software, and obtaining to-be-configured parameters and an installation script of the to-be-installed software according to the configuration file; generating aparameter configuration interface according to the to-be-configured parameters, and obtaining configuration parameters input by a user through the parameter configuration interface; transmitting theconfiguration parameters into the installation script, and remotely executing the installation script on a to-be-deployed host machine to realize software deployment; and in the process of executing the installation script, obtaining an installation log of a to-be-deployed host machine, and transmitting the installation log to an installation page for display. The method has the technical effectsthat the method is suitable for remote deployment of different general software, and a visual deployment interface is provided.

The invention discloses a firewall setting method, apparatus and device, and a storage medium, and supports a user to call a firewall service interface through a client, create a firewall model containing logic firewall information, translate the logic firewall information into logic flow table information, and send the logic flow table information to the client. The logic flow table information is logic firewall information recorded in a flow table form, the logic flow table information is translated into an instruction which can be executed by the switch, and the instruction is executed by the switch so as to realize a firewall function. The logic firewall information is realized by adopting the flow table, and the firewall function can be realized through the flow table by only needingfew resources, so that the resource occupancy rate is greatly reduced compared with the existing general software firewall. Moreover, when a new firewall rule appears, only a piece of new flow table information needs to be added for the newly-added rule, and the new flow table information can be executed by the switch after translation, and the existing firewall does not need to be redeployed, sothat the firewall is simpler and quicker to update.

The invention discloses a general purpose module integration method based on ScadeDisplay software and belongs to the field of unmanned aerial vehicle control platform technology. The method comprises the steps that first, the appearance of a display control module is designed and drawn, and display associated variables are set; second, a resource file and an interface code are created; third, a new general purpose software project is created; fourth, a header file and a library file are added into the newly created project; fifth, the resource file and the interface code are imported into the newly created general purpose software project; sixth, module integration and display are completed according to the order of application for resources, variable setting, interface refreshing and state saving. The ScadeDisplay software is utilized to design the module and generate the code, and is integrated into unmanned aerial vehicle ground station software to improve the software reuse rate; a solution to ground station code modularization and generalization is provided, software development and test pressure and operation difficulty for operators are lowered, and training time is shortened.

The invention discloses a high-speed momentum wheel rotational speed test device and a method thereof, and the test device is mainly composed of a standard metal electromagnetic shielding chassis, an AT96 bus motherboard, an AT96 bus AC / DC power supply board, an AT96 bus CPU board, an AT96 bus momentum wheel pulse acquisition board. Momentum wheel rotational speed pulses are acquired by the AT96 bus motherboard, pulse signals are stored in registers, then data of all 24 registers of the acquisition board in a sampling period are respectively read by the AT96 bus CPU board, and the stable rotational speed value of a momentum wheel can be obtained by carrying out the arithmetic processing. The test device and the method have the advantages that the test device can prevent the electromagnetic interference; the board devices have strong universality and simple maintenance; the momentum wheel pulse acquisition board acquires the data, the bus CPU processes the data, thereby obtaining the stable rotational speed value of the momentum wheel; the rotational speed of the momentum wheel can be precisely calculated, thereby avoiding the errors caused by installation process errors; the test device has maintainability, replaceability and is compatible with standard common software, thereby facilitating the software development; the communication speed is high, thereby ensuring the timeliness of the obtained calculated data.

The invention discloses a thermoforming part performance reliability design method considering manufacturing factors. The invention belongs to the technical field of hot stamping forming. Hot stampingprocess parameters and hot stamping part structure parameters are comprehensively considered; According to the method, the probability of failure of the thermoformed part is fully considered, and onthe basis of a reliability optimization design method, under the condition that the mechanical property of the part is improved, the rejection rate of the part is greatly reduced, and the design development efficiency and the production efficiency of the part are improved. Meanwhile, the software used in the implementation process of the patent of the invention is universal CAE software, has the technical characteristics of fast calculation process, efficient mapping process, simple data extraction and the like, is easy to popularize and use on a large scale in the design and development of the automobile thermoforming part, and contributes to improving the part design level of the automobile thermoforming part. The design method is simple, practical and easy to implement, and has wide application prospects in the hot stamping forming design and development process of the automobile parts.

The invention discloses a system-linked comprehensive operation and maintenance system and method in a cloud mode, and the system comprises a general operation and maintenance management platform which is used for providing the public operation and maintenance management of the whole system-linked comprehensive operation and maintenance system; the infrastructure operation and maintenance platform is used for providing infrastructure resources of the cloud environment and monitoring and operation and maintenance management of a platform cluster; the universal software operation and maintenance platform is used for providing state monitoring and operation and maintenance management of universal software, services and middleware involved in the cloud environment; and the service system operation and maintenance platform is used for providing monitoring and operation and maintenance of the service application system deployed in the cloud environment. The system provides the comprehensive fault analysis capability from infrastructure to general service and then to business application from three dimensions of business application dimension, associated resource dimension and associated application dimension, and comprehensively improves the comprehensive operation and maintenance, troubleshooting and positioning, and fault analysis and early warning capabilities of a business application system and a cloud center.

The embodiment of the invention discloses a method for realizing cross-platform software development and operation, which comprises the following steps of: writing a general software code by using a standard development language according to a formulated cross-platform unified development standard, and obtaining the packaged software code by different platforms; and transcoding the software code into a code adapted to the platform by adopting a development framework technology applicable to a platform environment, completing installation or updating of the software, and running the software onthe platform. By means of the method, differences of different platforms can be covered only by compiling codes once, the development efficiency is greatly improved, the development cost is saved, and the development time is shortened.

A software interface for a system provides an interface to software components of the system through a plurality of interface areas that are related to each other in a hierarchical manner. Each interface area provides an interface to the software components through one or more interface methods. The interface methods are generically defined methods and include a data handling method, an action method, and a navigation method. The data handling method includes the methods for setting and retrieving a value of a parameter. The action method includes the methods for retrieving and executing a specific method for carrying out operations on the system through the software components. The navigation method includes methods for navigating to a specific interface area. A token is associated with each of the interface methods to specifically define the method that is to be carried out.

The invention relates to a method for designing a flight parameter system with a comprehensive alarm function, belongs to the field of computer automatic control, and is applied to the technical fieldof avionics. The invention relates to designing of a flight parameter system with a comprehensive alarm function, hardware is a universal platform, and software is divided into an airborne part and aground part. The airborne part is a universal software module, the realized functions of the airborne part are set by a flight parameter acquisition configuration file and an alarm output configuration file, and the design mode can be applied to output control of various alarm signals on an airplane, such as light alarm, voice alarm, picture alarm and the like. According to the invention, a flight parameter acquisition recording function and a comprehensive alarm function are fused, the problem that the alarm reason is difficult to find in the flight training process is solved, the aircraft maintainability is improved, and the cost and the weight are reduced.

Methods and systems are provided for a device of a communication control system. In one example, the apparatus includes a Distributed Component Interconnect Framework (DCIF) configured to enable communications between different software modules of a communications network based on already existing code. The DCIF allows simultaneous communication between a plurality of transport protocols.

An automatic piloting system intended for an aircraft comprising an aircraft signals acquisition module, a module for interfacing with the crew, and a module for processing the output signals, comprises: a generic software kernel for automatic piloting aboard the aircraft, comprising several parameterizable elementary cells, a parameterization tool for the generic software kernel, able to transform an operational need of the automatic piloting system, expressed by means of a configuration file in accordance with a predetermined configuration domain DC, into a database of binary parameters DB able to parameterize the generic software kernel; each cell being parameterized by the database DB, and means for loading and storage aboard the aircraft of the database DB.

An information processing apparatus includes a first loading unit that loads a general-purpose software which provides a general-purpose function to an execution environmental area and mounts the general-purpose software in a predetermined directory at the time of starting up a system. A second loading unit loads a dedicated software which provides a function intrinsic to the other device to the execution environmental area and mounts the dedicated software in a predetermined directory at the time of starting up a system. An integrating unit integrates a first setting file containing general-purpose setting information which is included in the general-purpose software and a second setting file containing general-purpose setting information which is included in the dedicated software.

The invention relates to the technical field of software testing. The invention discloses an automatic testing framework system for PYTHON general APP software. The system comprises a script maintenance module, a script generation module, a script execution module, a result verification module and a report generation module, the script generation module outputs a report by adopting a unittest framework + HtmlTestRunner, a test script can be automatically generated, and two automatic test modes of an interface automation module or a ui automation module are provided. According to the method, ascript generation module outputs a report by adopting a unittest framework and an HtmlTestRunner; automatically generating test scripts, according to the test script generation method which is efficient and low in maintenance cost, the system maintenance cost can be effectively reduced, the script execution module can independently execute one of two automatic test modes of the interface automation module and the ui automation module and can also execute the two automatic test modes at the same time, and therefore diversified automation methods are achieved.

The invention provides an aircraft wire harness automatic design method, which comprises the steps of establishing an aircraft wire harness design top layer design specification, defining a design criterion and a constraint principle, and forming aircraft wire harness automatic design constraint parameters; in combination with the aircraft wire harness automatic design constraint parameters, customized top definition is performed on general Capital software, and aircraft wire harness automatic design project management parameters and design style parameters are set; carrying out topological interaction design on the aircraft topological graph and the aircraft line graph by utilizing Capal software and adopting existing aircraft topological design constraint parameters to generate a wiringharness model; and utilizing existing three-dimensional model design parameters, and combining with an airplane wire harness automatic design criterion and an airplane wire harness Capal library fileto carry out die repairing and parameter labeling on the wire harness model to form an airplane wire harness graph.