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183 results about "External memory interface" patented technology

An external memory interface is a bus protocol for communication from an integrated circuit, such as a microprocessor, to an external memory device located on a circuit board. The memory is referred to as external because it is not contained within the internal circuitry of the integrated circuit and thus is externally located on the circuit board.

Digital signal processor containing scalar processor and a plurality of vector processors operating from a single instruction

A digital data processor integrated circuit (1) includes a plurality of functionally identical first processor elements (6A) and a second processor element (5). The first processor elements are bidirectionally coupled to a first cache (12) via a crossbar switch matrix (8). The second processor element is coupled to a second cache (11). Each of the first cache and the second cache contain a two-way, set-associative cache memory that uses a least-recently-used (LRU) replacement algorithm and that operates with a use-as-fill mode to minimize a number of wait states said processor elements need experience before continuing execution after a cache-miss. An operation of each of the first processor elements and an operation of the second processor element are locked together during an execution of a single instruction read from the second cache. The instruction specifies, in a first portion that is coupled in common to each of the plurality of first processor elements, the operation of each of the plurality of first processor elements in parallel. A second portion of the instruction specifies the operation of the second processor element. Also included is a motion estimator (7) and an internal data bus coupling together a first parallel port (3A), a second parallel port (3B), a third parallel port (3C), an external memory interface (2), and a data input/output of the first cache and the second cache.
Owner:CUFER ASSET LTD LLC

Airborne distributed inertial attitude measurement system and transfer alignment method of airborne distributed inertial attitude measurement system

The invention relates to an airborne distributed inertial attitude measurement system and a transfer alignment method of the airborne distributed inertial attitude measurement system. The airborne distributed inertial attitude measurement system comprises a master inertial navigation system, a main control computer, and six slave inertial navigation systems connected with the main control computer, wherein each slave inertial navigation system respectively comprises an inertial measurement unit and an attitude measurement processing board, each inertial measurement unit is connected with an RS_422 interface of the corresponding attitude measurement processing board, each RS_422 interface is connected with an FPGA (Field Programmable Gate Array) chip through a UART (Universal Asynchronous Receiver / Transmitter) control chip, each FPGA chip is connected with a DSP (Digital Signal Processor) chip through an EMIF (External Memory Interface) bus and also connected with the master inertial navigation system through a CAN (Control Area Network) controller and a CAN transceiver, and the main control computer is connected with the master inertial navigation system. The transfer alignment method between the master inertial navigation system and each slave inertial navigation system of the airborne distributed inertial attitude measurement system comprises the steps of: by taking the speed information error and the attitude information error of the master inertial navigation system and the slave inertial navigation systems as measuring variables, correcting speed information and attitude information calculated by the slave inertial navigation systems after carrying out Kalman filtering iteration, and finally obtaining stable and accurate navigation attitude information.
Owner:NANJING UNIV OF SCI & TECH

Embedded type navigation information processor based on DSP (digital signal processor) and FPGA (field programmable gata array)

The invention discloses an embedded type navigation information processor based on a DSP (digital signal processor) and an FPGA (field programmable gata array). The navigation information processor comprises a data acquisition module, a logic control management module, a navigation data processing module, a navigation data output module and a Flash program solidification module. The DSP of the navigation data processing module is connected with a Flash, an SDRAM (synchronous dynamic random access memory) and the FPGA outside the DSP through an EMIF (external memory interface). The Flash program solidification module is connected with an external development computer through a serial port. The data acquisition module acquires data and synchronizing signals output by an IMU (inertial measurement unit) and a GNSS (global navigation satellite system). Address decoding and time synchronization are carried out through the logic control management module, and the results are input to an SDRAM (synchronous dynamic random access memory) of the DSP. Strapdown calculating and filtering algorithm are carried out by the navigation data processing module. Navigation information data are sent to other application devices in the form of network messages through the navigation data processing module. The navigation information processor is a special navigation information processor hardware platform applicable to a strapdown inertial navigation system, and meets the requirements for miniaturization, low power consumption and high accuracy of an SINS (ship's inertial navigation system)/ GNSS integrated navigation system.
Owner:SOUTHEAST UNIV

Special ASIC (Application Specific Integrated Circuit) chip system for spaceflight

ActiveCN102929836AHigh degree of integrationReduce mass volume power consumptionGeneral purpose stored program computerArea networkAdvanced Microcontroller Bus Architecture
The invention relates to a special ASIC (Application Specific Integrated Circuit) chip system for spaceflight. The special ASIC chip system comprises a MIPS (Million Instructions Per Second) nucleus, a PCI (Programmable Communications Interface) bus interface, an ISA (Internet Security And Acceleration) bus interface, a 1553B bus terminal interface, a 1553B protocol processor, a network interface, a CAN (Controller Area Network) interface, an EMI (External Memory Interface), AD acquisition control logic, OC door control logic, UART (Universal Asynchronous Receiver/Transmitter) serial port, PWM (Pulse Width Modulation) interface, a pulse counter PPC, PCM (Pulse Code Modulation) telemetry remote control module and a general input/output module, wherein the MIPS nucleus, the PCI bus interface, the ISA bus interface, the 1553B bus terminal interface, the 1553B protocol processor, a network interface, the CAN interface and the EMI are connected to an AMBA AXI (Advanced Microcontroller Bus Architecture Advanced eXtensible Interface) bus; and the AD acquisition control logic, the OC door control logic, the UART serial port, the PWM interface, the pulse counter PPC, the PCM telemetry remote control module and the general input/output module are connected to an AMBA APB (All Points Bulletin) bus; and the AMBA AXI bus is connected with the AMBA APB bus through an AXI/APB bridge.
Owner:NAT SPACE SCI CENT CAS

Off-chip Nor Flash bus interface hardware encryption device

The invention relates to an off-chip Nor Flash bus interface hardware encryption device which comprises an EMI (external memory interface), a data reading decryption passage, a data reading bypass passage, a data writing passage and an AES (advanced encryption standard) encryption engine, wherein the EMI is used for CPU (central processing unit) extensible external memories, the three passages connects the EMI with external Nor Flash memories, the AES encryption engine is connected between a CPU and the data reading decryption passage and used for plaintext data encryption, and the data reading decryption passage comprises an address analyzing unit, an address comparing unit, an indication control unit, a cipher text buffer unit, an AES decryption engine, a plaintext buffer unit and a secret key storage unit. Hardware-software combination is used to provide data encryption for off-chip Nor Flash memories. The device supports a bypass function, data can be written into off-chip Nor Flash memories in plaintext and read in plaintext, so that data storage flexibility is achieved. By the device which is flexible in extensibility, easy to design, high in reliability and safety and the like, Nor Flash bus interface encryption is achieved.
Owner:福建睿矽微电子科技有限公司
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