21 results about "Electronic computer" patented technology

This invention provides a satellite photoelectric guidance method and system for space observation. The method includes: First, a photoelectric sensing device senses targets around the satellite, completes target measurement and orbit calculation, and after orbit recursion, matches the target data with a ground-based target database to update the target database and preliminarily search for and identify potential collision sources and interference sources; Second, an onboard integrated electronic computer requests target observation data from the photoelectric sensing device and receives the target observation data; Third, the onboard integrated electronic computer filters and sorts the received targets, locating collision sources and interference sources requiring key attention; Finally, the onboard integrated electronic computer programmatically activates the optical payload equipment and electronic payload equipment, and sends angle information to the optical payload equipment and electronic payload equipment to achieve detailed observation of space targets.

HIGH-STABILITY, HIGH-AGILITY THREE-SAILING SURFACE AIRCRAFT The three-sail aircraft (1), (2), and (3) is equipped with movable flaps (6), (7), and (8) on each of the lifting surfaces. The flaps of the upstream lifting surface (6) are connected to the flaps of the main wing (7) by a rigid linkage with a deflection angle ratio of 50%. The forces on the downstream lifting surface (horizontal tail) (3) reverse between takeoff (negative lift) and cruise (positive lift). Stabilizing fins (5) are positioned at the rear of the fuselage in the lower section at an angle of 30° to the aircraft's centerline. A weighted control rod (22) located in the vertical tail (4) provides stabilization for the aircraft in the presence of severe turbulence.The propulsion system is located at the rear of the fuselage and consists of either a piston engine driving a multi-bladed propeller, one or two turboshaft engines driving a multi-bladed propeller or two contra-rotating propellers, a turbojet engine, or one or two electric motors driving a multi-bladed propeller or two contra-rotating propellers. This aircraft can be piloted either by a human pilot on board or by an electronic computer controlled from the ground or autonomously.

Method for determining the use of a vehicle safety belt (4) comprising a webbing (5), a tongue (6) held on the webbing (5), and a buckle (7), and assigned to a seat (3) of a vehicle, wherein a sensor device (8) of the buckle (7) detects a closed state of the buckle (8) resulting from the insertion of an element into the buckle (7), characterized in that: - by means of an electronic computing device (9), a second time interval (Z2) is determined within a first time interval (Z1) extending from a first time point (t1), at which the closed state of the buckle (7) beginning at the first time point (t1) is detected by the sensor device (8), to a second time point (t2), at which a first event is detected, during which the closed state of the buckle (7) is continuously detected by the sensor device (8).which extends from a third time point (t3) between the first time point (t1) and the second time point (t2), at which a second event is recorded, up to the second time point (t2); - the first event includes the opening of a vehicle door; - the second event includes the unoccupancy of the seat (3); - the second time period (Z2) is compared with a threshold value by means of the electronic computing device (9); and - a feigned use of the seat belt (4) is determined by means of the electronic computing device (9) if the comparison of the second time period (Z2) with the threshold value determines that the second time period (Z2) exceeds the threshold value.

The objective is to develop a system and method for determining the weights of consensus odds among sportsbooks. [Solution] The system includes a function to calculate consensus odds based on the odds of each wager at each wagering venue, and each wager's odds at each wagering venue has a weight relative to the consensus odds that is proportional to the total amount wagered at each wagering venue among multiple wagering venues in the market.

A system for supporting activities in a shipyard during construction of a ship has at least one local electronic computer installed in a watchtower of the ship and operatively connected to at least one central electronic computer remote from the ship, a first plurality of electronic apparatuses operatively connected by respective wired connection backbone cables to form one or more tree network topologies, each electronic apparatus representative of a root node of a respective tree network topology being operatively connected to the at least one local electronic computer, and a plurality of sensors adapted to detect information representative of the shipyard and operatively connected by respective wired connection cables to form one or more network topologies from one or more electronic apparatuses. Each electronic apparatus is configured to manage network connectivity and safety of the shipyard based on the information representative of the shipyard detected by the plurality of sensors.

The article to which this design relates is a smartphone-type electronic computer. It has the function of remotely controlling a passenger car. In the reference front view, the area indicated by leader line 1 is the area that displays the state and status of the passenger car being remotely controlled. The area indicated by leader line 2 is the area where operation buttons for frequently performed operations such as opening and closing door locks are located. The area indicated by leader line 3 is the area for performing other operations. The operation buttons in the area indicated by leader line 2 can slide left and right, and change as shown in the front view in the changed state.

A system for controlling actuators in an aircraft. The system including at least a first actuator and a second actuator. Each of the actuators including a movement member, at least one measurement sensor, and a computing member internally connected to the movement member and configured to be connected to at least one electronic computer of the aircraft. The computing member having a function for controlling the movement member, the measurement sensor of the first actuator being externally connected to the computing member of the second actuator, the computing member of the second actuator also having a monitoring function for monitoring the movement member of the first actuator.

This invention provides a satellite telemetry scheduling and processing method and system suitable for spread spectrum hopping mode, comprising: collecting telemetry source packets from various satellite subsystems; performing secondary screening on all telemetry source packets and recombining important telemetry parameter packets in spread spectrum hopping mode; grouping important telemetry parameter packets in spread spectrum hopping mode into virtual channel data units according to the virtual channel identifier of spread spectrum hopping mode; scrambling the virtual channel data units according to the selected scrambling polynomial and initial phase; adding frame synchronization words to group channel access data units; performing frame selection processing under different modes according to different telemetry rate switching modes; dividing the selected telemetry frames into equal parts and inserting the equally divided telemetry data into different spread spectrum hopping downlink measurement frames for transmission. This invention effectively meets the compatibility processing requirements of integrated electronic computers for conventional noncoherent spread spectrum mode and spread spectrum hopping mode, ensures the transmission of important telemetry in spread spectrum hopping mode, and facilitates ground processing.

An avionics electronic computer with a virtual machine management hypervisor, and an aircraft comprising such a computer. This avionics electronic computer on board an aircraft comprises a group of computing electronic card(s) (25) having computing resources and storage resources (40); a set of microservices executed independently of each other, with at least a part of the resources; a set of software application(s) to call one or more of the microservices; and a set of orchestrator(s) (55, 56) to implement the set of microservices by allocating at least a part of the resources.The orchestrator set includes several orchestrators (55, 56), and the computing card group comprises at least two virtual machines (50) and a virtual machine management hypervisor (45), common to the computing card group and configured to distribute at least some of the resources among the virtual machines (50), each hosting one of the orchestrators and making its resources available to that orchestrator. See Figure 2 for abbreviations.

1. Name of the product in this design: Mouse (G75). 2. Purpose of this design: This design is used to assist in the operation and control of electronic computers. 3. The key design features of this product are the combination of shape and pattern. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

The invention relates to an avionic electronic computer installed on board an aircraft, the electronic computer comprising a group of electronic computing card(s) (25) comprising computing resources and storage resources (40); a batch of micro-services executed independently of one another, with at least part of the resources; a set of software application(s) for calling one or more of the micro-services; and a set of orchestrator(s) (55, 56) for implementing the batch of micro-services by allocating at least part of the resources. The set of orchestrator(s) includes a plurality of orchestrators (55, 56), and the group of electronic computing card(s) comprises at least two virtual machines (50) and a hypervisor (45) for managing the virtual machines, the hypervisor being common to the group of electronic computing card(s) and configured to distribute at least part of the resources between the virtual machines (50), each virtual machine hosting one of the orchestrators and making its resources available to the orchestrator.

Avionics computer for on-board flight operations in an aircraft comprising a microprocessor- or microcontroller-based computing unit (1) having a plurality of microprocessor- or microcontroller-based computing modules (10, 11, 12, 13), wherein each computing module (10, 11, 12, 13) has a microprocessor- or microcontroller-based processor and a main memory divided into several main memory segments, each of which is exclusively assigned to a specific processor of the computing modules (10, 11, 12, 13), and wherein the computing unit (1) of the avionics computer is configured such that the processors have read access to all main memory segments of the main memory of their respective computing modules (10, 11, 12, 13) and have write access to the main memory segments assigned to them.

1. The name of the design product: the fitting part of the battery for portable electronic computer. 2. The use of the design product: the design product as a whole is the battery for portable electronic computer; the part claimed for protection is the fitting part for fitting with other parts to make electrical connection. 3. The design points of the design product: the shape of the part claimed for protection shown in the perspective view 1. 4. The picture or photo best indicating the design points: the perspective view 1. 5. Other circumstances needing explanation Other explanation: the design is a partial design; the part shown in solid line is the part claimed for protection as a partial design; the A-A sectional view is the view omitting the internal mechanism.

The new pressure gas bearing belongs to the field of gas bearings. The bearing consists of a stepped shaft, a bearing, and left and right end caps. The working principle of the new pressure gas bearing is the same as that of a dynamic pressure gas bearing under environmental conditions. It uses the dynamic pressure effect of the pressurized gas in the large shaft clearance to carry radial load. This invention aims to solve two technical problems. First, it aims to substantially solve the world problem of "sealing the pressurized gas inside the bearing". By using a pressure-sealed container and assembling twice, the pressurized gas can be sealed inside the bearing. Second, it aims to completely solve the hidden danger of the gas bearing seizing the shaft. For this purpose, two measures are adopted: 1. The outer clearances (2) and (17) of the small shafts on both sides of the stepped shaft are absolutely unequal. 2. Improve the hardness of the bearing surface at high temperature, or spray a layer of hard material on the bearing surface. This invention returns the air compressor that was required for the operation of the pressure gas bearing from the West to the Western world. It does not require a throttle, and the bearing performance is better than that of the air compressor. The new pressure gas bearing is widely used in inertial navigation gyroscopes, precision machine tool spindles, high-speed power head bearings: boring heads, milling heads, high-speed magnetic heads of electronic computers, etc.

1. Name of the designed product: computer support frame. 2. Use of the designed product: support for electronic computer display screen. 3. Design points of the designed product: in shape. 4. Picture or photo best indicating the design points: perspective view 1.

The invention relates to programmable microelectronic systems, in particular to non-volatile solid electrolyte memory cells based on glassy chalcogenides and can be used in electronic devices including programmable memory circuits in the form of binary data, which are widely required in automation systems for control and execution devices, as in electronic computers of all types.The non-volatile memory cell and the process for its realization include a substrate (1), on which is grown an insulating film of SiO2(2), on which are consecutively deposited a passive metal electrode (3) of Pt, a solid electrolyte layer (4), made of glassy chalcogenide with the self-organized structure Ge7,7As15,3S77-Ag and an electrochemically active electrode of Ag (5), the cell is equipped with a voltage pulse generator (6), and a recording device (7).

This specification discloses a method, apparatus, storage medium, and device for acquiring three-dimensional CT images. The method includes: acquiring images of the target object from at least two different acquisition angles using a computed tomography (CT) device in the default coordinate system of the CT device, obtaining a reference image for each acquisition angle; identifying a target region in each reference image, and determining, based on the identification result, the projection plane of the target region in the direction perpendicular to the acquisition angle corresponding to the reference image, as the vertical projection plane of the reference image; determining the position information corresponding to the center point of the target region based on the vertical projection plane corresponding to each reference image; and adjusting the CT device based on the position information to acquire a three-dimensional CT image of the target region using the adjusted CT device. This solution achieves automatic centering of the CT device, improving centering efficiency and accuracy.

A method and program for visualizing sound effect adjustment. The method can be applied to a program for visualizing sound effect adjustment, and causes an electronic computer to perform the following steps, including: capturing a first audio; identifying a first sound element from the first audio, and displaying a first representative icon and a first volume setting icon corresponding to the first sound element; determining whether to adjust the volume setting of the first sound element; after adjusting the volume setting of the first sound element, capturing a second audio, and separating the first sound element from the second audio; and re-producing the second audio with the first sound element having the adjusted volume setting.

Electronic computer research apparatus

The application discloses a performance optimization method and device for a big data plug-in, equipment and a storage medium, relates to the field of electronic computers, and instantiates a data operation object of the big data plug-in when receiving a data operation request sent by a target application, and initializes the instance object. Since the initialization includes creating a log aggregator and reading log parameters for the instance object, and the instance object can collect operation logs in the process of executing a target data operation, when the instance object is called to execute a data operation, the log aggregator can count and print the operation logs output by the instance object based on the log parameters. Based on the instance object, the application can realize automatic collection of data operation logs, and based on the log aggregator and the log parameters, the application can realize automatic counting and printing of the data operation logs, thereby solving the problem in the prior art that operation logs of the big data plug-in cannot be automatically collected and counted.