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70 results about "Design Validation" patented technology

Split and merge design flow concept for fast turnaround time of circuit layout design

A method and system is disclosed to improve the turnaround time to provide adequate time to meet project schedules in the event that adjustments or modifications to the design are necessary. A method for improving a turnaround time for design verification of a process database representing a semiconductor design includes the steps of (a) deriving a timing database and a (DNE) database from the process database; (b) performing, using the timing database, one or more design changes and one or more timing verifications and corrections to generate a modified timing database; (c) initiating, using the process database, physical validation of the semiconductor design prior to completion of step (b) to generate a modified DNE database; (d) merging the modified timing database with the modified DNE database to form a modified process database; and (e) performing, using the modified process database, one or more design verification checks of the semiconductor design.
Owner:BELL SEMICON LLC

Partial Timing Modeling for Gate Level Simulation

Various apparatuses, methods and systems for creating an integrated circuit and performing a gate level simulation of a circuit are disclosed herein. For example, some embodiments of the present invention provide a system for performing a gate level simulation of a circuit including a computer system, a design verification tool and an output device. The design verification tool, executable on the computer system, includes a simulator and a partial timing model generator. The partial timing model generator is operable to generate a representation of the circuit for simulation by cutting a first portion of a circuit out of a full gate level netlist for the circuit and leaving a second portion of the circuit represented by the full gate level netlist, and to overlay a simplified representation of the first portion of the circuit over the representation of the circuit. The first portion of the circuit is cut out at timing paths. The simulator is operable to perform a gate level simulation of the circuit based on the representation of the circuit. The output device is connected to the computer system and is operable to provide an indication of a result of the gate level simulation of the circuit.
Owner:TEXAS INSTR INC

Facilitating structural coverage of a design during design verification

One embodiment of the present invention provides a method and a system that facilitates structural coverage of a design during a design verification process. During operation, the system receives a hardware description of the design, which contains one or more module instances and a set of structural coverage targets for a set of structures in the design. The system then extracts a control flow, the set of structural coverage targets, and a set of structural coverage metrics for the hardware description, and creates a shadow module with the same control flow as the hardware description. This shadow module contains a set of parallel structures that correspond to the set of structural coverage targets in the control flow of the hardware description and serve as targets for formal methods used to analyze the design. The system also generates a set of cross-module references to link the set of parallel structures in the shadow module with signals from the set of structures in the hardware description. The system then applies a formal verification tool to the design, including the shadow module and the cross-module references in an attempt to achieve the desired structural coverage.
Owner:SYNOPSYS INC

On-chip power supply network verification method for side channel attack

ActiveCN106817215AIntuitive and usable attack defense capability evaluation resultsLow costEncryption apparatus with shift registers/memoriesPlaintextValidation methods
The invention discloses an on-chip power supply network verification method for a side channel attack. The method comprises: logical synthesis and physical design processing is carried out on a register transmission level netlist file of a chip to obtain a transistor level netlist file; according to the obtained transistor level netlist file, a circuit model including a power supply network and a load is established; according to a generated plaintext-ciphertext data pair and a corresponding secret key, a logic process for encryption operation execution on the chip is simulated to obtain a current waveform file of the load; on the basis of the circuit model and the current waveform file of the load, a physical process for encryption operation execution on the chip is simulated to obtain a power consumption curve of the chip; according to the obtained power consumption curve, a side channel attack is carried out on the chip to obtain a guess secret key of the attack; and on the basis of the obtained guess secret key, a side channel attack result is analyzed and an anti-side channel attack capability of the power supply network is verified. The method has advantages of low cost, high accuracy, and reduced design verification period.
Owner:TSINGHUA UNIV

Composite material structural design verification method for airworthiness certification

The invention discloses a composite material structural design verification method for airworthiness certification. The composite material structural design verification method for airworthiness certification comprises the following steps that 1, the application positions of composite materials are determined, and airworthiness verification of the composite materials is performed; 2, the preliminary dimension of the typic structure is determined, the needed composite material is selected from the composite material system determined in the first step, and airworthiness verification is performed on design allowable values of the composite material in the structural state; 3, according to the design allowable values obtained in the second step, assembly-level detailed design and airworthiness verification of the composite material structure are performed; 4, according to the structural design of the assembly-level composite material in the third step, the detailed design and trial trip verification of the composite material of full-scale-level of an airplane are determined. The composite material structural design verification method has the advantages that the confidence coefficient of a result obtained through the experimental verification method is high, the requirement for experience of designers is low, different persons can follow the same verification method, the certification time is shortened, and the product development period is shortened.
Owner:XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA

Airborne system digital design verification system and method

The invention discloses an airborne system digital design verification system and method and belongs to the technical field of system engineering. The system disclosed by the invention comprises a top-layer digital design system and a domain engineering layered digital design system, wherein the top-layer digital design system comprises a demand analysis module, a top-layer analysis design module and a top-layer model test and verification module; and the domain engineering layered design system comprises a single-domain analysis design module, a single-domain test and verification module, multi-domain collaborative design module and a multi-domain model simulation verification module. The method disclosed by the invention comprises the following two steps: concept model machine design of an airborne system and virtual model machine design of the airborne system, wherein the former step comprises the following three sub-steps: demand analysis of the airborne system, system analysis of the airborne system and system design of the airborne system. The system and method disclosed by the invention can be used for supporting the digital analysis, design and verification of the airborne system, realizing 'design and verification first, implementation later' of the airborne system, avoiding the problems of long period, high cost, great risk and the like caused by the 'design and implementation first, verification later' of the traditional design method.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Method, System, and Program Product for Automated Verification of Gating Logic Using Formal Verification

As described herein the automated verification methodology parsing scripts auto generate test bench hardware design langaue, such as VHDL or Verilog, from the design source VHDL or Verilog. A formal verification model is then built comprising the testbench VHDL and the design under test. The resulting design verification tool then provides proofs and counterexamples for all of the rules, e.g., auto-generated rules, in the test bench.
Owner:GLOBALFOUNDRIES INC

Method and system for platform-independent VOIP dial plan design, validation, and deployment

A system and method for designing a dial plan for Voice over Internet Protocol (VoIP) systems includes generating an abstract dial plan design which is platform independent, the dial plan including rules for routing communications in a VoIP network structure. The dial plan is validated through simulations prior to deployment to evaluate the dial plan performance under simulated conditions. The dial plan design is translated to provide compatibility with a deployed network using platform specific configuration adaptors.
Owner:IBM CORP

Transformer and power supply device

InactiveCN108122667ASimplify Design DebugShorten Design Verification CycleUnwanted magnetic/electric effect reduction/preventionPower conversion systemsTransformerConductor Coil
The embodiment of the invention discloses a transformer and a power supply device. The transformer comprises a primary winding, a secondary winding, a shielding winding and an adjustable impedor; thefirst end or the second end of the primary winding is connected with the first end of the adjustable impedor, and the second end of the adjustable impedor is connected with the first end of the shielding winding; the adjustable impedor is a replaceable or adjustable impedance component; under the situation that the transformer is in access into a power supply circuit, when a switching tube of thepower supply circuit is switched between disconnecting and closing states, the direction of current produced by the shielding winding is opposite to the direction of the common mode current of the primary winding and the secondary winding, the adjustable impedor is used for adjusting the size of the current produced by the shielding winding, and the current produced by the shielding winding is equal to the sum of the common mode current produced by the primary winding and the secondary winding; wherein the number of turns of the shielding winding is a fixed value and larger than the thresholdvalue of the number of turns. According to the transformer and the power supply device, design and commissioning of the transformer can be simplified, the design validation cycle of the transformer isshortened, and the production cost is reduced.
Owner:HUAWEI DIGITAL TECH SUZHOU
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