Apparatus and method for processing an instruction matrix specifying parallel and dependent operations

Information

  • Patent Grant
  • 10289605
  • Patent Number
    10,289,605
  • Date Filed
    Friday, December 22, 2017
    6 years ago
  • Date Issued
    Tuesday, May 14, 2019
    5 years ago
Abstract
A matrix of execution blocks form a set of rows and columns. The rows support parallel execution of instructions and the columns support execution of dependent instructions. The matrix of execution blocks process a single block of instructions specifying parallel and dependent instructions.
Description
BACKGROUND

The invention relates generally to computer architectures. More particularly, the invention relates to a computer architecture to process matrix instructions specifying parallel and dependent operations.


Improving computer architecture performance is a difficult task. Improvements have been sought through frequency scaling, Single Instruction Multiple Data (SIMD), Very Long Instruction Word (VLIW), multi-threading and multiple processor techniques. These approaches mainly target improvements in the throughput of program execution. Many of the techniques require software to explicitly unveil parallelism. In contrast, frequency scaling improves both throughput and latency without requiring software explicit annotation of parallelism. Recently, frequency scaling hit a power wall so improvements through frequency scaling are difficult. Thus, it is difficult to increase throughput unless massive explicit software parallelization is expressed.


In view of the foregoing, it would be desirable to improve computer architecture performance without reliance upon frequency scaling and massive explicit software parallelization.


SUMMARY

A matrix of execution blocks form a set of rows and columns. The rows support parallel execution of instructions and the columns support execution of dependent instructions. The matrix of execution blocks process a single matrix of instructions specifying parallel and dependent instructions.





BRIEF DESCRIPTION OF THE DRAWINGS

The invention is more fully appreciated in connection with the following detailed description taken in conjunction with the accompanying drawings, in which:



FIG. 1 illustrates an architecture to support the execution of parallel and dependent instructions in accordance with an embodiment of the invention.



FIG. 2A illustrates the mapping of serial instructions to produce parallel and dependent operations in an execution matrix of the invention.



FIG. 2B illustrates the mapping of operations to an execution matrix of the invention.



FIG. 3 illustrates a row of execution blocks that may be utilized in accordance with an embodiment of the invention.



FIG. 4A illustrates execution blocks and supporting register files and buffers that may be utilized in accordance with an embodiment of the invention.



FIG. 4B illustrates a register file configured in accordance with an embodiment of the invention.



FIG. 5 illustrates various data configurations that may be utilized with a buffer of the invention.



FIG. 6 illustrates a pipeline that may be utilized in accordance with an embodiment of the invention.



FIG. 7 illustrates matrix instruction processing in accordance with an embodiment of the invention.



FIG. 8 illustrates the mapping of operations to an execution block of the invention.



FIG. 9 illustrates a matrix buffer utilized in accordance with an embodiment of the invention.



FIG. 10A illustrates a universal unit to implement operations of the invention.



FIG. 10B illustrates a one bit cell of a carry look-ahead adder used in the 4-bit adder in FIG. 10A.



FIG. 11 illustrates a Time-Lag Sliced Architecture (TLSA) unit configured in accordance with an embodiment of the invention.



FIG. 12 illustrates multiple TLSA units in a staggered configuration in accordance with an embodiment of the invention.



FIG. 13 illustrates a prior art multiplication technique.



FIG. 14 illustrates a time-lag multiplication technique utilized in accordance with an embodiment of the invention.



FIG. 15 illustrates prior art Booth encoded multiplication.



FIG. 16 illustrates logic to implement the Booth encoded multiplication of FIG. 15.



FIG. 17 illustrates Booth encoded multiplication in accordance with an embodiment of the invention.



FIG. 18 illustrates logic to implement the Booth encoded multiplication of FIG. 17.



FIG. 19 illustrates a memory/register file data block configured in accordance with an embodiment of the invention.



FIG. 20 illustrates a time slice memory configured in accordance with an embodiment of the invention.



FIG. 21 illustrates a TLSA architecture with a permute/shift unit configured in accordance with an embodiment of the invention.



FIG. 22 illustrates a floating point multiply accumulate unit configured in accordance with an embodiment of the invention.





Like reference numerals refer to corresponding parts throughout the several views of the drawings.


DETAILED DESCRIPTION OF THE INVENTION

It is highly beneficial to allow software that is not explicitly parallelized to execute on single processor hardware that is capable of processing massive numbers of instructions in a short latency pipeline. To give a current perspective on current solutions; super scalar processors can practically process 4-5 instructions in a cycle at peak instants, which is similar to what a good VLIW compiler can achieve at peak instants. It is well recognized that scaling super scalar processors to schedule 10's of instructions in a single cycle/instant is not practically achievable. Similarly, compliers that try to parallelize general programs for VLIW architectures with 10's of slots end up leaving a lot of those slots unfilled.


The invention provides architecture and processor implementations enabling massive parallelism allowing large number of instructions is to be fetched, scheduled, decoded, and executed in a short pipeline, achieving an impressive improvement in the throughput of execution, while maintaining a much optimized latency of operations in single processor pipeline with efficient timing, power, area and routing.


In this new architecture, named Ultra Large Instruction Matrix (ULIM), fixed size instruction matrix templates are scheduled to be executed in the hardware as a matrix of parallel and dependent groups of instructions. In contrast to VLIW where only parallel instructions are scheduled using the Very Long Instruction width template, the template of the ULIM architecture encapsulates a group of instructions that have both parallel and dependent instructions. This can be viewed as a 2 dimensional template matrix where parallel instructions are allocated horizontally while dependent instructions are allocated only vertically. This template is sent as one instruction matrix to the execution hardware, where each execution block processes an instruction matrix.



FIG. 1 illustrates such a template where if an instruction is put in slot 101 then another instruction that can execute in parallel to it can be put in any of the parallel slots 1 to N in that same row. However, an instruction that depends on the one placed at slot 101 cannot be placed in the same row and has to be placed on a following row (e.g., parallel slot 0 of serial slot 1) 102. The slot noted by 102 can receive as an input either the result produced by 101 or an external input operand or a combination of both. The execution model of such an instruction template is that instructions at any row will execute before those in the next row.


The ULIM instructions' grouping can be scheduled statically by a ULIM compiler or dynamically by a ULIM hardware composition unit. The significance of this architecture is clear if it is compared to a traditional architecture. In a traditional architecture, one row of N.sub.1 parallel instructions can be put in a template, such as VLIW or SIMD template. This means each cycle, N.sub.1 instructions can be executed (all have to be insured to be parallel which is a serious constraint for a large N). On the other hand, the ULIM architecture can execute N.sub.1*N.sub.2 instructions each cycle by pipelining execution at each row boundary. In spite of executing N.sub.1*N.sub.2 instructions each cycle, the ULIM architecture imposes only the same constraint of insuring that N.sub.1 instructions execute in parallel.


The instruction matrix template can be constructed by the programmer or by a compiler/hardware formatter where neither of them need to be constrained by finding only parallel instructions to schedule every cycle. Available parallel instructions can be picked and placed horizontally in rows. The parallel instructions can be augmented by dependent instructions that are placed in subsequent rows. A matrix can execute in a single or multiple cycles. A matrix can localize storage of operands near the execution hardware to optimize interconnect complexity, area, speed and power.


The invention is more fully appreciated in connection with the example of FIG. 2A. FIG. 2A illustrates an example of an instruction sequence 200 presented by a single serial program flow. The figure also shows how the instructions are grouped to form a single instruction matrix with both serial and parallel slots utilized in the matrix template. The matrix template is applied to an execution block 201. The execution block 201 includes a multiplication unit 202, a floating point add unit 204, a load unit 206, a multiple accumulate (MAC) unit 208, a logic unit (e.g., an ALU) 210, and another logic unit 212.


Thus, an instruction matrix refers to an instruction group template with parallel and serial instructions. An execution block refers to a group of execution units that execute an instruction matrix. Execution units are individual computation units (e.g., both complex and simple units) within an execution block.


Straight arrows, such as 214, indicate a dependency between instructions. The mapping can be done by the compiler, by the front end hardware or by a run time environment. FIG. 2A also depicts a formatted operation map showing the relative physical location of the instructions in the matrix as they will be executed on the corresponding hardware locations with parallel and serial dependency indicators.


As shown in FIG. 2A, the single stream program is reformulated into a matrix of instructions that statically determines serial execution, as well as instruction parallelism. For example, in the serial single program flow in FIG. 2A, the last instruction uses R3 as a source while the fourth instruction writes R3 as a result. This is mapped in the matrix template by placing the last instruction in a row that is subsequent to the row that the fourth instruction occupies. Line 214 illustrates this dependency.


The encoded instructions and their sources and destinations for the template shown in FIG. 2A are illustrated in FIG. 2b, where the instruction matrix template includes the opcode for the instructions and specifies the operands and result registers. Sources and destinations are separate from opcodes. This simplifies the decoding stage, the dependency resolution stage, and the register/memory read stage.


Several instruction matrices can be issued simultaneously, as shown in FIG. 3. FIG. 3 illustrates the instruction matrix operation map of 201, represented here as 301, along with alternately configured instruction matrices operation maps 300, 302 and 304. Simultaneous issuance may be implemented using one of the following models:


1—MIMD or SIMD: Software/compiler glues multiple matrices into a super matrix.


2—Threaded model: Each matrix belongs to a separate software or hardware thread.


3—Dynamic execution: Matrices from a single stream can be dynamically issued by the hardware if no dependency exists between them.


The instruction matrix templates represented by their operational maps in FIG. 3 are executed on a hardware that maps those instruction slots into execution units (inside the execution blocks) with a one to one correspondence. Granularity of the matrix allows forming a baseline matrix and combining those matrices to form a super matrix. This is illustrated in FIG. 4A, where 4 base-line instruction matrices execute in parallel on four execution blocks 301, 300, 302, and 304. Each execution block consists of 2 rows of complex units. The first row has 3 complex units (e.g., 402, 404, and 406) and another row with 3 complex units (e.g., 408, 410, and 412). Each complex unit can be operated to compute complex operations like a multiply, floating point add, or multiply-accumulate operations. Thus, for example, complex unit 402 may correspond to 202 of FIG. 2, complex unit 404 may correspond to 204 of FIG. 2, etc.


A complex unit can be operated to compute up to 4 simple operations, such as ALU operations. Such a complex unit is thus shown to have multiple operands and multiple outputs. The units can be arranged to compute parallel operations or be sequenced to perform dependent operations. Each of the base-line instruction matrices can be run independent of other matrices in a threaded mode or a number of them can be combined in a group that can be run in the same cycle as a super instruction matrix composing a MIMD architecture. The whole matrix can be executed in one cycle or could be pipelined over multiple cycles.


As an example of operating the execution engine shown in FIG. 4A to execute the ULIM instruction template of FIG. 3, instruction MAC 208 is executed in complex unit 408, while the pair of simple Logical and ALU operations 210 are executed in a pair of units of 408. FIG. 4A illustrates the similarities and differences with a VLIW architecture. If in FIG. 4A we use the top 3 slots (402, 404, 406) to execute 3 parallel instructions, then these 3 slots in the ULIM template would resemble an equivalent VLIW instruction. Using the next row of simple units (408, 410, 412) to execute 3 more parallel instructions will mean that we are executing another equivalent of a VLIW that depends on the previous one. Thus, the ULIM architecture can be viewed as executing in space and with a fixed lag of time a fixed number of multiple VLIW instructions that are dependent on each other. In addition, the architecture allows executing a single complex instruction or multiple simple instructions in one single slot, which is not allowed in VLIW templates.


The 4 ULIM matrices indicated by operation maps 301, 300, 302, and 304 in FIG. 3 can be executed on the hardware in FIG. 4A. This may implemented in one of 3 execution modes: either by being grouped together by the compiler/programmer to form a MIMD super instruction matrix, or each matrix can be executed independently in a threaded mode where separate threads execute simultaneously on each of the 4 hardware sections (301, 300, 302, and 304). The last execution mode possible is the ability to dynamically execute 4 different instruction matrices from a single thread using a hardware dependency check to insure no dependency exists between those different matrices that execute simultaneously on the 4 different hardware sections in FIG. 4A.


The register files 420 in FIG. 4A may be alternately configured depending upon the execution mode. In one mode, the register files are viewed as either an MIMD sectioned register file serving a MIMD width of 4 sections or they serve as 4 individual register files, each serving a separate thread. The register files can also support a dynamic execution mode where the 4 sections are one unified register file where data written to any register in a particular section is accessible by all units in the other sections. Switching between those modes can be seamless as different executing modes can alternate between individual thread baseline instruction matrix and MIMD super instruction matrix threads.


Each single instruction matrix is a mix of parallel and dependent instructions. Also, each individual instruction can be a scalar or SIMD instruction. At the finest granularity, the instruction can resemble variable data-width SIMD operating on multiple bytes/words or a single scalar entity.


In a multithread execution mode, each register file and its execution unit that executes a thread is totally independent of other register files and their threads. This is similar to each thread having its own register state. However, dependency between those threads can be specified. Each matrix that belongs to a thread will execute in the execution unit of that thread's register file. If only one thread or non-threaded single program is executed on the hardware in FIG. 4A, then the following method is used to allow parallel matrices belonging to that single thread/program to be able to access the results written into the registers in the other sections. The way this is done is by allowing any matrix writing results into any one of the 4 register file sections to generate copies of those registers in the other register file sections. Physically this is done by extending the write ports of each section into the remaining sections. However, this is not scalable, as we cannot build an efficient register file with each memory cell having as many as 4 times the write ports as needed for one section alone. We present a mechanism where the register file is built such that it will not be impacted with such single thread register-broadcast extension. Such a mechanism is shown in FIG. 4B.



FIG. 4B shows one section of the register file consisting of 24 registers where a matrix that belongs to a single thread is storing the results of execution in that section's 24 entry register file. At the same time, 3 other parallel matrices are executing on the other 3 sections of FIG. 4A and the results of their execution are broadcasted to this register file section.


The way that the write ports are configured to enable single thread register broadcast is by limiting the results of each matrix to non-overlapping 6 register groups. This is implemented by having sectioned write ports where each write port writes into a separate group of registers 430. The write ports 440 coming from other sections will write into different non-overlapping groups of registers.


If this is a threaded mode or MIMD mode, then all the write ports that go to those non-overlapping groups are used by the results of this section to utilize and write to the full 24 entry register file and no broadcasting is done since other sections have independent code that uses independent registers (which means local section registers will need all registers to use). On the other hand, if a single thread is in use, then all the sections are cooperating on doing useful work for this single thread. The total registers in this case will be only 24, thus registers across the remaining sections (24 entries*3 sections) can be used to hold copies among each other. This group assignment of the registers can be assigned by the compiler using analysis to determine if matrices could be parallelized and thus assign those matrices that have a chance of executing in parallel non-overlapping group of registers.


Even though the results are being written from all 4 sections, each memory cell in the register file only has ports to support one section. In traditional register files it has to have support for 4 sections, a four fold increase as illustrated in the following example.


The data parallelism in the ULIM is implemented in these architectures on top of the base line format of the ULIM. This is done by allowing each instruction in the ULIM template to be a SIMD/MIMD instruction. In the previous figure each parallel slot can support an internal replicated SIMD structure, while the MIMD is supported by the different parallel/serial slots.


The memory/register or matrix buffer being accessed by an instruction can be viewed differently depending on the intended access nature. For example, the data matrix could be viewed as MIMD of wide data elements, SIMD of small data elements or MIMD of mixed data width SIMD instructions.


In FIG. 5 there are 2 views of the memory/register matrix buffer layout of the data. The one on the right represents orthogonal data elements in each row and column. This supports different combination of MIMD/SIMD data. The view on the left represents different elements on each position of any row, but the column represents the remaining bits of a larger data size element. For example, the view on the right can represent 4 MIMD instructions each operating on 4 different SIMD bytes, where each is a byte of parallel data elements. While the one on the left represents 4 MIMD instructions, where each of these instructions operates on an element of 32-bits laid out vertically (actual physical layout will differ from the logical representation shown). Moreover, if the view is a MIMD view, then all belong to one single MIMD register of 4 sections, but if the view is non-MIMD view, then those registers are 4 independent registers laid out vertically.


The significance of this memory and register file view and its corresponding execution mode is that it enables the execution unit to morph to execute a wide MIMD/SIMD instruction (glue all register sections to form 4-way MIMD/SIMD), but at the same time the 4 register file sections and corresponding execution units attached can execute as 4 independent units acting on 4 different scalar registers, allowing single and multiple threaded execution within the execution unit at the lowest level of granularity.


The ULIM architecture has fixed size instruction templates similar to VLIW or MIMD templates. In contrast to VLIW or MIMD templates, the ULIM templates allow one to specify both parallel instructions as well as dependent instructions. It follows the same Von Neumann architecture of instructions writing into registers and dependency of instructions within a matrix communicated through register name dependency. One more noteworthy aspect of the ULIM architecture is that each instruction in the matrix has a fixed predetermined location in the matrix and executes in a fixed timing relative to other instructions in the matrix. The width of the ULIM matrix resembles the width of a corresponding VLIW template. Actually, it is always possible to transform serial flow of dependent VLIW instructions into a ULIM template by placing one VLIW instruction at one row of the horizontal rows of the ULIM template. It is not possible to resemble all possible ULIM templates using a flows of VLIW instructions because the ULIM template can include in the same row one complex instruction in one slot and multiple simple instructions in the horizontally adjacent slot.


The advantages of utilizing the matrix architecture composing a matrix of instructions as opposed to executing individual instructions as traditional architectures do are numerous. The following discussion illustrates mechanisms enabling and utilizing the invention's instruction matrix and execution block architecture to build and implement a massively-parallel single processor pipeline.



FIG. 6 illustrates a possible processor pipeline that takes advantage of a ULIM architecture. The invention utilizes a mechanism to simplify the fetch stage 600, branch resolution and decoding stage 608. The fetch unit 600 steps forward while fetching the code on an instruction matrix basis as opposed to an instruction basis. The program counter for such an architecture is incremented by the size of the matrix instead of being incremented by the instruction size. This means that in each cycle a large number of instructions are fetched. To be able to do that, the ULIM matrix will not allow a branch to exist within the ULIM matrix, but branches can exist between ULIM matrices. Branch resolution is done on 2 levels. Within the ULIM matrix, the branches are replaced with conditional execution, conditional moves and prediction. Across matrices, the branches are handled by path prediction and branch coloring. This allows large numbers of instructions grouped into matrices to be moved forward across the pipeline fetch and branch resolution stages.


Executing dependent instructions along side parallel instructions within a single matrix relieves the compiler from the difficulty of constructing all-parallel instructions slot code. It also simplifies the data dependence checking in the score board hardware 602 dispatch unit 604 or hardware scheduling unit. This is achieved by using the matrix number as a utility to enforce score boarding and dependency maintenance between matrices as opposed to using individual registers or individual instructions. In the example of FIG. 7, the score board characterizes the dependency precedence of matrix 8 by only referencing matrix numbers 2, 4 and 5, which means matrix 8 needs to read data results from those matrices. The score board dependency checking does not need to reference the individual register or instruction information to maintain the dependency score boarding. The matrix number carries that information and is enough to maintain correctness of dependency checking. Instructions within a matrix that depend on other matrices can be issued when those matrices are executed. The whole matrix is prevented from being dispatched when the matrices it depends on stalls (e.g., for a cache miss). In one embodiment of the ULIM pipeline implementation, the decode stage 608 is delayed until the stage just before execution, and it is done in parallel with the register read stage 606.



FIG. 8 illustrates one implementation for encoding the instruction template of the ULIM architecture. The key is the encoding and organization of the operands (results and sources registers). The registers specifying instruction results and source operands are specified in a separate section of the ULIM template regardless of the opcode of the instructions and regardless of the fact that the instructions are complex operations or pairs of simple instructions. This matrix format that lists the sources and destinations in an explicit section of the matrix enables the source and destination registers to be extracted independent of the decoding of instructions within the matrix. It will thus be able to implement a delayed decode stage, where actual decoding of the individual instruction opcodes is delayed until just prior to the execution stage and will proceed in parallel with register read to enable execution on the next cycle. It also simplifies dependency resolution and scoreboard implementation.


If a slot includes a complex instruction, such as “Multiply accumulate” (MAC) then it requires 4 sources and writes back two results. If the same slot includes two simple instructions, such as a Logic and an ALU, then each requires 2 sources and writes back one result, which both combined requires 4 sources and generates two results. This makes the number of sources and results independent of the type of operation.


Processor execution hardware as shown in FIG. 4A includes register read and write mechanisms where a matrix operand buffer can assemble the required register sources and destinations based on physical location of where each source will execute on the respected hardware element of the matrix. This reduces the number of read and write ports and the bandwidth requirement on the register file. Using this characteristic of the matrix architecture, the bypassing mechanism is simplified where buffering the sources and/or the destinations in a matrix buffer that is close by or attached to each execution unit can provide shorter access time and larger source and results port bandwidth than a traditional register file, especially in the case of large size register file that needs to support so many individual execution units.



FIG. 9 illustrates the concept of a matrix buffer of the invention. The figure shows the instruction matrix operand buffer 900 connected to the execution units 902. In this example, the instruction matrix operand buffer 900 buffers sources and destinations for 3 different matrices. Particularly important is the fact that write ports 904 are architected such that each write port writes to different memory cells. This means the matrix operand buffer memory cells are single ported even though there are 6 results that are written at the same time, which is equivalent to a traditional register file that is 6-way ported. Moreover, each write port has a fan out (cells that it needs to drive) equal to the number of matrices in the matrix buffer (only 3 in this example). These features have a lot of advantages in area, power and access speed, making this buffer design very scalable and attractive for high bandwidth high speed register file alternatives.


The following method describes how the registers are written and accessed from the matrix operand buffer. Each matrix is allocated to any available matrix space in the matrix buffer just in time or a short time before the matrix is ready for execution. Remote sources (e.g., sources that are not in other matrices storage within this matrix buffer) that the matrix needs to be able to start executing can be temporarily staged in this matrix storage.


After executing the matrix, results are written into the area allocated for this matrix storage (in one of the 3 matrix locations in the matrix buffer of FIG. 9). Each result is written into the corresponding location accessed by that result write port regardless of the result register number. This location along with the matrix location is communicated to the consuming matrices similar to the score board mechanism shown in FIG. 7, such that each matrix that depends on this matrix will annotate its register sources with the location of the matrix that those sources come from and location of each of the sources within the matrix. The result location within the matrix can be communicated at execution time by the execution hardware or can be embedded in the matrix instruction template alongside the source register number by the software since the matrix template is fixed at compile time.


The basic idea is to build a scalable design of sources and result buffers alongside register files where those buffers are connected to the execution units to allow higher bandwidth and speed by holding data temporary in a matrix location-based identification method establishing an intermediate medium between regular register files and execution units. Values in those matrix buffers can be accessed using the matrix location and the location of the source inside the matrix. For example, register 5 written by matrix 20 can be accessed by recording where that matrix is allocated in the matrix buffer and indexing that matrix's own storage by the entry number that the register 5 result physically occupies inside that matrix. However, after the matrix is de-allocated from the matrix buffer, then all the entries holding register values within the matrix will be written back into the actual register file and accessed by the register number from that moment onwards. The same location-based identification and access method discussed earlier for a register file using a matrix data buffer can be applied to memory accesses using a memory buffer cache.


The matrix architecture can be easily constructed by a compiler if the underlying hardware is uniform and replicated. It also allows for greater efficiency in utilizing the power and silicon area. Here we introduce the concept of a universal unit that is constructed from basic building elements, such as small adders, logical gates, multiplexers, and booth cells.


The architecture of the universal unit allows it to perform all functions/operations inside every single universal unit. This means each universal unit is capable of performing addition, multiplication, shift, permute, etc. The way it is able to perform such universal functionality is its composition out of basic building elements that are used to perform the simple ALU operations. On the other hand, those simple elements are cascaded to perform the complex operations. It also can process floating point and integer data. The universal unit concept is facilitated by the ideas described above, but it achieves an important advantage by simplifying the scheduling and utilizing the machine throughput to the maximum. In regular architectures, a separate unit is used to perform each operation or function. They share the same port of execution. Thus, when one unit is used, the rest are not utilized. Moreover, the latency in traditional architectures varies among them making it difficult for the scheduler to schedule them. In contrast, in this universal unit, latency is unified for the whole unit and the scheduler sees a symmetric instantiation of the universal unit.



FIG. 10A shows part of this universal unit. Each universal unit can perform different execution units' functions, such as a multiplier, adder, shifter, permuter, etc. This embodiment shows the structure with carry save adders and/or generic adders 1000. The Unit is composed of basic constructs, each one with 4 rows of adders (could be more or less adders) capable of adding 8 inputs in parallel (4 parallel/serial add operations). These adders are then structured in groups. Each adder in a row can be either connected to the same location adder in the row below (to perform serial ALU operation) or be connected to the adder to its right in the row below to perform a multiply operation. The operations can be C*B+A, or A OP B, in each row forming 4 parallel/serial ALU operations. In addition, it is possible for these groups of adders to have different data sizes. This structure of adders allows for a tree to perform multiple operand addition, multiplication, multiply accumulate, sum of difference, shifting and rotating. Additionally, multiplexers (not shown in the figure) will align/permute/shift the input or intermediate outputs to obtain the required operation, including shift and permute operations. Booth cells/bit multiply cells 1002 are added to the adders to enable multiplication. Other specific logic, state, memory, or LUT elements are added to provide expanded functionalities.


The universal unit allows the permute/shift unit to be implemented using the same structure that is used to perform the multiply operation or the structure that is used to do the floating point add or floating point multiply accumulate. This advantage allows less routes/area to implement a permute/shift logic. The way the shift or rotate is performed in a multiply structure is by performing a multiplication by 2.sup.x where x is the shift count. Performing left shift, right shift or rotate is done by selecting the upper product of the multiply result or lower part or performing the OR function between lower and upper multiply result, respectively.


Each of the elements compose a group of bits using a basic 2-input adder structure. Carry-save-adders can also be built with logic and MUXES. For example, to build 32*32 elements, the basic groups can be constructed of 8 bits or 4 bits of basic adders and MUXES, and be able to perform logic functions using the modified carry look ahead adder cell internal logic gates.



FIG. 10B shows the modified basic one bit cell of a carry look-ahead adder used in the 4-bit adder in FIG. 10A to produce either an adder output or a selected logic output. Modification is shown by connections 1010 and two 4:1 multiplexers 1012 that are not in the critical path of the adder. The original adder bit structure (marked as 1014) includes carry look ahead and sum logic. This figure is for logical representation, actual circuit may differ.


The 4-bit (or 8-bits) groups facilitate the execution of various size SIMD widths as well as 16-bit operations. By the same concept, those 16-bit tiles can be cascaded for larger width data operations, such as 64-bit operations, while still facilitating 8-bit, 16-bit and 32-bit SIMD operations of addition and multiple operand addition, shifting, rotating and multiplication.


The basic concept behind this organization is to be able to execute a combination of parallel and serial instructions on the same structure. For example, the first row of constructs can execute a single 32-bit ALU that can be followed by either a dependent or independent ALU on the 2.sub.nd row and so on. The 4 rows together can execute up to four 32-bit ALU serial/parallel operations or a single 32-bit multiply operation. It can also perform partial width SIMD operations on the sub matrices. The instructions and operands scheduled on this universal unit come as one group, particularly within the matrix data and instructions section.


The ability to pipeline instructions within one cycle is possible using the instruction matrix architecture because we pipeline the dependent instructions to be scheduled within the same cycle or on the following cycle depending on the required frequency. There are multiple ways to take advantage of the ULIM architectures. The system allows for Ultra Large Instruction Matrix scheduling. Parallel instructions as well as dependent instructions are scheduled as a matrix (this is in contrast to VLIW where only parallel instructions can be scheduled). Each instruction or dependent instruction in this matrix can be scalar or SIMD.


The invention may be implemented in any number of ways. For example, multiple dependent instructions may be staged within a clock cycle. In this embodiment of the invention, multiple dependent and parallel instructions can be staged within one clock cycle. Multiple dependent instructions can start within one cycle; this reduces the optimum critical path of the program execution. Multiple dependent instructions may be pipelined with state elements, separating each basic operation in a unit from the following operation. This increases the rate of pipeline execution. However, the power of the design will increase because of clock speed and extra state elements. The state elements may stay constant, but the rate of data pumped through the design increases using wave pipelining.


The invention also includes a Time-Lag Sliced Architecture (TLSA) that accelerates the latency of dependent instructions. The basic idea behind the time lagged sliced architecture is that an operation produces its result digit slice by digit slice. Each slice is produced earlier than the next slice with a time lag between slices. Once the first slice is produced, the next computation can start execution and produce its own slice. The sliced architecture described here is an overall architecture that applies to computational units as well as register files and memories. The architecture applies to all arithmetic, shift, integer and floating point operations.


The TLSA is used to implement an entire system architecture, including memory and computations. The digit slices are not necessarily equal sized digits. The invention can operate with both operands arriving in a digit sliced manner. The invention can implement a booth encoded multiplier, variable shifters, permute engines, as well as floating point adders and multipliers.


In designing execution units, the common methodology is to synchronize the digits or bits of a digit of the output result of an arithmetic/logical or shifter unit as one single output result. This result is either latched into a storage element or staged synchronously as one piece to a receiving element. However, in this architecture fine grain execution is provided with or without coarse grain synchronous execution. The basic philosophy is to formulate the arithmetic or permute/shift operation in such an organization of time lag logic slices that are staged in time and/or space. The execution hardware is connected in a time delay flow, where early slices execute faster and produce slices of the output results faster, while later slices need more time to execute and produce results in a delay relative to earlier slices. It is worth mentioning that the slices are done on fine granularity of bits/digits within even a single execution unit, like an adder or permuter. This architecture can utilize such organization of digit/bit logic slices to optimize logic timing critical paths and/or number of signal routing paths and/or arca for performing arithmetic, permute, shift, etc. for both integer and/or floating point operations. The slices can be of equal number of bits/digits or different number of bits/digits. One particular advantage of this architecture is the ability to start executing dependent instructions before all the output result slices of the source instruction are finalized.



FIG. 11 illustrates a TLSA unit 1100 where data flows in and out of slices 1102A-1102C. Each slice output has a lag time delay (d) with respect to a previous slice. This time-lag nature allows the unit to be pipelined such that state elements of the different slices are not synchronized to one time, as is typical for row/stage flip flops.


The architecture of FIG. 11 includes a basic adder stage structure that computes basic computation tasks, such as multiple operand addition or sub-block multiplication. Those computations are cascaded using staging elements 1104A-1104C that are not part of the critical path of the basic task. The staging elements can be adders, multiplexers, or logical gates, depending upon the basic computational task that is being sliced. The delay of these staging elements 1104 is minimal and equal to time “d”, which is the delay between each slice output and the next slice output.


The staging element is chosen to have the smallest delay possible, as it also establishes the delay of the input operand slices between themselves. The basic computational task in FIG. 11 can use arbitrary levels of adders. Those adders can be any type, e.g., binary or Carry Save Adders (CSA). The architecture of FIG. 11 has the advantage of producing the first slice of the result earlier than the final result. The first slice is forwarded to subsequent operations.



FIG. 12 illustrates one embodiment of the invention where multiple time-lag sliced units are staggered back to back. In this embodiment, each diagonal slice represents an instruction computation unit divided into slices. Here each slice starts execution at a lag in time with respect to a previous slice. Each unit feeds a subsequent unit. This embodiment shows four units back to back. The notation SU1.sub.−0 refers to Slice number 0 of unit number 1. SU4.sub.−7 refers to Slice number 7 of unit number 4.


The architecture shown in FIG. 12 allows (if desired) for multiple TLSA units to process data in a single cycle (or in multiple cycles). A low slice of a first unit feeds the low slice of a second unit and this in turn feeds the third and then the third feeds the forth, etc. It is also important to notice that in addition to the first slice of the first unit feeding the first slice of the second unit, it also feeds the second slice of its own unit (the 1.sub.st unit). FIG. 12 illustrates the following concepts:


1—Sub-cycle/multi-cycle execution in TLSA [0092] TLSA allows for the execution of the arithmetic/shift/logic operations within one cycle. FIG. 12 illustrates this where 4 units are executed in one cycle, where each slice has a delayed version of that clock cycle. By the same token, the pipelining can be done at the output of each unit slice (instead of output of 4) to increase the throughput and execute in multiple cycles.


2—Asynchronous/Synchronous/Wave TLSA topologies [0094] The TLSA can be designed in at least 3 different topologies or combinations of those topologies: [0095] A—Asynchronous: where slices' inputs/outputs are communicating with each other within the cycle time without synchronous state elements (e.g., flops). This allows for removal of internal pipeline state elements and enables power friendly slower clock domains. [0096] B—Synchronous: each slice is clocked into a state element (Flop/Latch/domino, etc). This allows for a higher clock throughput and pipelining rate. [0097] C—Wave: in this topology, the data is fed into the unit slice by slice, with the next input data coming at a rate that is faster than the normal pipelining rate. Normal pipeline rate is determined by the maximum time of logic paths between two state elements. Wave pipeline is determined by minimum time of logic paths between two state elements. One interesting combination of topologies is Fine Grain Asynchronous-Coarse Grain Synchronous (FGA-CGS). In this scheme, the TLSA is implemented using time lag slices that are connected asynchronously, where fine grain asynchronous execution is provided with or without coarse grain synchronous execution. The basic philosophy is to formulate the arithmetic or permute/shift operation in such an organization of sliced staged processing where the execution of the different slices of the execution hardware is asynchronously connected in a time delay flow where early slices have less inputs and execute faster and produce their output results faster. Later slices have more inputs, thus need more time to execute and produce results in a delay relative to earlier slices. Each slice is then clocked in a synchronous (or asynchronous) element that has a time lag with respect to the previous slice.



FIG. 12 illustrates multiple TLSA units staggered within one cycle (4 back to back units within 1 clock), at the same time the implementation illustrates a FGA-CGS implementation where unit slices communicate with each others in an asynchronous manner (fine granularity asynchronous), while each slice or back to back slices are synchronized at the output to a state element clock. Each output of the slices may be synchronized to a different clock (delayed version).


The TLSA architecture supports the Ultra Large Instruction Matrix (ULIM) architecture. In this TLSA embodiment, a whole instruction group is scheduled where multiple parallel and dependent instructions are scheduled on instantiation of the TLSA cluster shown above. Each unit can also support SIMD data where duplicates of the data slices are instantiated, but controlled by the same instruction excitation. Additionally, multiples of this assembled structure of SIMD Universal Units can be instantiated horizontally to implement a MIMD architecture on top of a single unit. This way a whole instruction template containing both parallel variations of SIMD instructions and dependent instructions is scheduled in a cycle.



FIG. 13 illustrates a traditional multiplication technique. In particular, each B digit is multiplied against the set of A digits, each of those digits must be available at the multiplication execution unit at the initiation of multiplication. The results are then summed. In contrast, with the present invention, as shown in FIG. 14, operands arrive digit by digit. It can be seen that each row of FIG. 14 represents a partial product of the multiplication operation, but contains only current arriving and previously arrived digits with respect to digit slice arrival times.


To demonstrate how to build the logic structure that uses Booth encoded multiplication to execute the time delay sliced architecture, FIG. 15 illustrates a traditional Booth encoded 32-bit regular multiplier. The Booth encoder groups consecutive multiplier bits together to generate a digit. This grouping can reduce the maximum digit value that represents those bits by considering the signed combinations of the 2 consecutive digits in the number. For example, a 3-bit digit has a maximum value of 7, but by adding 1 to the value of the digit to its left, then the digit 7 is now equivalent to −1. Using signed representations of the digits allows values of those encoded digits to reach a maximum value of ½ of the original digit values.



FIG. 16 implements the traditional logic structure of the regular Booth multiplication shown in FIG. 15 using radix-4 digits. The selectors 1600A, 1600B choose which multiple of the multiplicand to use out of the possible signed values (0, 1, −1, 2, −2); the choice is determined by the Booth encoding of the multiplier bits



FIGS. 17 and 18 show the new Booth encoded scheme and the new TLSA logic structure to implement it. Notice that a traditional multiplier has a continuous encoding of the stream of bits, while the TLSA Booth encoder inserts 0's in the stream at the boundaries of the digit slices (in this example a digit of 8 bits). The inserted zeros do not change regardless of the sign of the multiplication (the last 2 bits represent the sign).



FIG. 18 shows how to implement the new modified time-lag sliced Booth encoded 32-bit multiplier. This implementation resembles the generic TLSA structure shown in FIG. 11. FIG. 18 implements sub-multiplication operations illustrated in FIG. 14 and FIG. 17.


The data parallelism in the TLSA is implemented in these architectures on top of the base line format of the TLSA. This is done by allowing each instruction in the TLSA data format of the SIMD/MIMD to be organized in an orthogonal dimension to the TLSA slices. FIG. 19 shows a configuration where a memory/register file data block is accessed by an instruction that can be viewed differently depending on the intended access nature. For example, the data block could be viewed as MIMD of wide data elements, SIMD of small data elements, MIMD of mixed data width SIMD instructions, etc. FIG. 19 illustrates an architecture to execute such combinations. The slices within the unit can operate independently to perform sub-operations. For example, each slice of 8 bits can perform independent 8-bit multiplication, while the group of slices that construct one 32-bit multiplier unit can also be operated as a 4-way SIMD byte multiplier. On the other hand, the group of units can be operated as a MIMD multiplier.



FIG. 20 illustrates a memory that is accessed in a sliced manner. In traditional memory architectures, a single operand (e.g., a 64-bit integer or floating point operand) is fetched as a whole. After the address decoding is finished, all the bits are read through the read port, which has to buffer the read enable across the whole width of the operand size in memory. In the TLSA architecture, after the decoding of the address occurs, the data read and/or write occurs on a time lag model of a slice following a previous slice with a time delay in between. The benefit of this model is the fast memory response when it is not necessary to decode and drive the whole data width at once.



FIG. 21 illustrates a TLSA architecture with a permute/shift unit that takes advantage of the time lag between data slices. This advantage allows faster time to produce early result slices and/or less routes/area to implement a permute/shift logic. In FIG. 21, a right shifter is constructed to take the time lag arrival of a 32-bit operand sliced in 8-bit digits. The first slice (digit) of the 32-bit input arrives at time T.sub.0, while the last slice arrives at time T.sub.0+3d, where d is one MUX delay. The bits (0 to 5) shown vertically on the right side represent the shift count (maximum of 32, any value>32 generates an output of zero, basically all data is shifted out). The execution starts with the arrival of the first low order digit from the right side of the shifter. The unit then waits for the next input digit to arrive. One of the digits is selected to the lower digit position depending on the value of bit 3 of the shift count, which will determine if the number will be shifted by 8 bits to the right. Then the next most significant digit arrives and a choice is made to select this new digit or pass the data that was selected in the upper multiplexer levels using the next bit in the shift count and so on. Any multiplexer position where the shift count will zero out that location will implement a zero override to its output. When the last digit arrives, it goes through the least number of multiplexer levels and thus will have a minimum delay “d” with respect to the previous digit to enable a fast propagation of the last digit to the output.


A left shifter can be constructed with the structure of FIG. 21 mirrored about a vertical line where left slices have larger stacks of multiplexers and right slices have smaller stacks of multiplexers. The most significant digit passes through the least number of multiplexer levels.


The sliced architecture universal unit can be a universal unit similar to the one described in FIGS. 10A-10B. It uses the same techniques of the sliced architecture (TLSA) and/or fine grain asynchronous concepts. It performs all functions/operations inside every single universal unit. This means each universal unit is capable of performing addition, multiplication, shift, permute, etc. The way it is able to perform this universal functionality with low latency is the ability to process the individual slices one at a time in a time lag fashion. It also can process floating point and integer data. The universal unit concept is facilitated by the ideas described above, but it achieves an important advantage by simplifying the scheduling and utilizing the machine throughput to the maximum. In regular architectures, a separate unit is used to perform each operation or function. They share the same port of execution. Therefore, when one unit is used the rest is not utilized. Moreover, the latency varies among them making it difficult for the scheduler to schedule them. In contrast, in this universal unit, latency is unified for the whole unit and the scheduler sees a symmetric instantiation of the universal unit.


Each universal unit can perform different execution units' functions, such as a multiplier, adder, shifter, etc. In addition, it is possible for these slices to have different data sizes. In this particular illustration, each slice is larger in data width than the previous slice. This structure of adders allows for a tree of slices to perform multiple operand addition, multiplication, multiply accumulate, sum of difference, etc. Multiplexers (not shown in the figure) align/permute/shift the input or intermediate outputs to obtain the required operation, including shift and permute operation using the universal structure of adders/multiplexers. Booth cells/bit multiply cells are added to the adders to enable multiplication. Other specific logic, state, memory, or LUT elements are added to provide expanded functionalities.


The ULIM architecture can be time sliced using the disclosed TLSA techniques. One other way to construct a Universal unit is to configure it as a Floating point multiply accumulate unit (MAC). The functions used in building this unit are Multiplier, Right Shifter, Adder, and Left shifter. Such a structure as disclosed in FIG. 22. A Universal unit can utilize such a structure to perform any one or combinations of those functions that construct the FP-MAC.


Each one of those functions has been described earlier and therefore can be implemented individually as TLSA structures and then be combined to operate as a floating point multiple accumulate TLSA structure. Such a structure can also operate as a consecutive sliced ALU or multiply followed by an ALU or shift, etc.


An embodiment of the present invention relates to a computer storage product with a computer-readable medium having computer code thereon for performing various computer-implemented operations. The media and computer code may be those specially designed and constructed for the purposes of the present invention, or they may be of the kind well known and available to those having skill in the computer software arts. Examples of computer-readable media include, but are not limited to: magnetic media such as hard disks, floppy disks, and magnetic tape; optical media such as CD-ROMs, DVDs and holographic devices; magneto-optical media; and hardware devices that are specially configured to store and execute program code, such as application-specific integrated circuits (“ASICs”), programmable logic devices (“PLDs”) and ROM and RAM devices. Examples of computer code include machine code, such as produced by a compiler, and files containing higher-level code that are executed by a computer using an interpreter. For example, an embodiment of the invention may be implemented using Java, C++, or other object-oriented programming language and development tools. Another embodiment of the invention may be implemented in hardwired circuitry in place of, or in combination with, machine-executable software instructions.


The foregoing description, for purposes of explanation, used specific nomenclature to provide a thorough understanding of the invention. However, it will be apparent to one skilled in the art that specific details are not required in order to practice the invention. Thus, the foregoing descriptions of specific embodiments of the invention are presented for purposes of illustration and description. They are not intended to be exhaustive or to limit the invention to the precise forms disclosed; obviously, many modifications and variations are possible in view of the above teachings. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, they thereby enable others skilled in the art to best utilize the invention and various embodiments with various modifications as are suited to the particular use contemplated. It is intended that the following claims and their equivalents define the scope of the invention.

Claims
  • 1. An apparatus for executing instruction matrices, comprising: a memory to store a plurality of instruction matrices; anda plurality of matrices of execution units to execute the plurality of instruction matrices, wherein each of the plurality of instruction matrices includes rows and columns, wherein instructions in a same row of an instruction matrix are to be executed in parallel and instructions that are dependent upon instructions in a row of an instruction matrix are in a subsequent row of the instruction matrix, wherein the plurality of matrices of execution units is configurable to operate in different execution modes including a first execution mode, a second execution mode, and a third execution mode, wherein in the first execution mode, the plurality of matrices of execution units simultaneously executes a group of instruction matrices that form a super instruction matrix,wherein in the second execution mode, the plurality of matrices of execution units simultaneously executes instructions matrices belonging to separate threads, andwherein in the third execution mode, the plurality of matrices of execution units simultaneously executes non-dependent instruction matrices from a single thread.
  • 2. The apparatus of claim 1, further comprising: a register file having a plurality of register segments to store results for subsequent processing by the plurality of matrices of execution units, wherein the register file is configurable to support different execution modes including the first execution mode, the second execution mode, and the third execution mode, wherein in the first execution mode, the plurality of register segments forms a single register file where each register segment stores sources and results of a Multiple Instructions Multiple Data (MIMD) super instruction issuing simultaneous instructions where each individual instruction is a scalar or Single Instruction Multiple Data (SIMD) instruction,wherein in the second execution mode, the plurality of register segments forms individual independent register files with individual register state to support simultaneous processing of separate threads, wherein each instruction is associated with a separate thread and a separate register file segment, andwherein in the third execution mode, the plurality of register segments forms a single thread register file, wherein register segments are duplicated in multiple register segments of the register file to store results of simultaneously executed non-dependent instructions that are dynamically issued from a single thread instruction sequence.
  • 3. The apparatus of claim 1, wherein a matrix of execution units of the plurality of matrices of execution units includes a first row of execution units and a second row of execution units, wherein execution units in the first row of execution units operate in parallel and execution units in the second row of execution units operate in parallel and operate in dependency upon the execution units in the first row of execution units.
  • 4. The apparatus of claim 3, wherein each instruction matrix of the plurality of instruction matrices includes a first row of instructions and a second row of instructions, wherein instruction in the first row of instructions are executed in parallel by a subset of execution units of the first row of execution units, and wherein instructions in the second row of instructions are executed in parallel by a subset of execution units of the second row of execution units.
  • 5. The apparatus of claim 1, wherein the super instruction matrix is formed by a compiler.
  • 6. The apparatus of claim 1, wherein the plurality of instruction matrices is formed by a run-time system.
  • 7. The apparatus of claim 1, wherein the plurality of instruction matrices is formed by hardware.
  • 8. The apparatus of claim 1, wherein the plurality of instruction matrices is formed by a compiler.
  • 9. The apparatus of claim 1, wherein the plurality of matrices of execution units supports floating point, integer, Single Instruction Multiple Data (SIMD), and Multiple Instruction Multiple Data (MIMD) operations.
  • 10. The apparatus of claim 9, wherein an instruction matrix of the plurality of instruction matrices includes Single Instruction Multiple Data (SIMD) instructions.
  • 11. The apparatus of claim 9, wherein an instruction matrix of the plurality of instruction matrices includes Multiple Instruction Multiple Data (MIMD) instructions.
  • 12. The apparatus of claim 9, wherein an instruction matrix of the plurality of instruction matrices includes a combination of Single Instruction Multiple Data (SIMD) instructions and Multiple Instruction Multiple Data (MIMD) instructions.
  • 13. The apparatus of claim 1, wherein each of the plurality of instruction matrices is assigned a matrix number to enforce dependency maintenance between the plurality of instruction matrices.
  • 14. The apparatus of claim 13, further comprising a scheduler, wherein the scheduler uses matrix numbers to track register references.
  • 15. The apparatus of claim 1, wherein an instruction matrix of the plurality of instruction matrices specifies source operands and destination operands in fixed locations regardless of opcode.
  • 16. The apparatus of claim 1, the non-dependent instruction matrices from the single thread are determined to be non-dependent using a hardware dependency check.
  • 17. A method by a processor for executing instruction matrices, comprising: fetching a plurality of instruction matrices, wherein each of the plurality of instruction matrices includes rows and columns, wherein instructions in a same row of an instruction matrix are to be executed in parallel and instructions that are dependent upon instructions in a row of an instruction matrix are in a subsequent row of the instruction matrix; andexecuting the plurality of instruction matrices in a first execution mode, a second execution mode, and a third execution mode, wherein in the first execution mode, a plurality of matrices of execution units of the processor simultaneously executes a group of instruction matrices that form a super instruction matrix,wherein in the second execution mode, the plurality of matrices of execution units simultaneously executes instructions matrices belonging to separate threads, andwherein in the third execution mode, the plurality of matrices of execution units simultaneously executes non-dependent instruction matrices from a single thread.
  • 18. The method of claim 17, further comprising: storing a result of executing the plurality of matrices of execution units in a register file having a plurality of register segments, wherein the register file is configurable to support the first execution mode, the second execution mode, and the third execution mode, wherein in the first execution mode, the plurality of register segments forms a single register file where each register segment stores sources and results of a Multiple Instructions Multiple Data (MIMD) super instruction issuing simultaneous instructions where each individual instruction is a scalar or Single Instruction Multiple Data (SIMD) instruction,wherein in the second execution mode, the plurality of register segments forms individual independent register files with individual register state to support simultaneous processing of separate threads, wherein each instruction is associated with a separate thread and a separate register file segment, andwherein in the third execution mode, the plurality of register segments forms a single thread register file, wherein register segments are duplicated in multiple register segments of the register file to store results of simultaneously executed non-dependent instructions that are dynamically issued from a single thread instruction sequence.
  • 19. The method of claim 17, wherein a matrix of execution units of the plurality of matrices of execution units includes a first row of execution units and a second row of execution units, wherein execution units in the first row of execution units operate in parallel and execution units in the second row of execution units operate in parallel and operate in dependency upon the execution units in the first row of execution units.
  • 20. The method of claim 19, wherein each instruction matrix of the plurality of instruction matrices includes a first row of instructions and a second row of instructions, wherein instruction in the first row of instructions are executed in parallel by a subset of execution units of the first row of execution units, and wherein instructions in the second row of instructions are executed in parallel by a subset of execution units of the second row of execution units.
CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No. 14/733,827 filed Jun. 8, 2015 (now U.S. Pat. No. 9,886,416 issued Feb. 6, 2018), which is a continuation of U.S. application Ser. No. 13/691,609 filed Nov. 30, 2012 (now U.S. Pat. No. 9,053,292 issued Jun. 9, 2015), which is a continuation of U.S. application Ser. No. 12/296,919 filed Dec. 19, 2008 (now U.S. Pat. No. 8,327,115 issued Dec. 4, 2012), which is the National Stage of International Application No. PCT/US2007/066536 filed Apr. 12, 2007, which claims priority to U.S. Provisional Application No. 60/792,219 filed Apr. 14, 2006 and U.S. Provisional Application Nos. 60/791,782 and 60/791,649 filed Apr. 12, 2006, which are hereby incorporated by reference.

US Referenced Citations (463)
Number Name Date Kind
727487 Swan May 1903 A
4075704 O'Leary Feb 1978 A
4245344 Richter Jan 1981 A
4356550 Katzman et al. Oct 1982 A
4414624 Summer, Jr. et al. Nov 1983 A
4524415 Mills, Jr. et al. Jun 1985 A
4527237 Frieder et al. Jul 1985 A
4577273 Hopper et al. Mar 1986 A
4597061 Cline et al. Jun 1986 A
4600986 Scheuneman et al. Jul 1986 A
4633434 Scheuneman Dec 1986 A
4682281 Woffinden et al. Jul 1987 A
4727487 Masui et al. Feb 1988 A
4816991 Watanabe et al. Mar 1989 A
4835680 Hogg et al. May 1989 A
4920477 Colwell et al. Apr 1990 A
4930066 Yokota May 1990 A
4943909 Huang Jul 1990 A
5197130 Chen et al. Mar 1993 A
5294897 Notani et al. Mar 1994 A
5317705 Gannon et al. May 1994 A
5317754 Blandy et al. May 1994 A
5339398 Shah et al. Aug 1994 A
5404470 Miyake Apr 1995 A
5469376 Abdallah Nov 1995 A
5471593 Branigin Nov 1995 A
5509130 Trauben et al. Apr 1996 A
5517651 Huck et al. May 1996 A
5524090 Iwamura Jun 1996 A
5548742 Wang et al. Aug 1996 A
5559986 Alpert et al. Sep 1996 A
5574878 Onodera et al. Nov 1996 A
5581725 Nakayama Dec 1996 A
5590084 Miyano et al. Dec 1996 A
5634068 Nishtala et al. May 1997 A
5649136 Shen et al. Jul 1997 A
5675759 Shebanow et al. Oct 1997 A
5699537 Sharangpani et al. Dec 1997 A
5710902 Sheaffer et al. Jan 1998 A
5724565 Dubey et al. Mar 1998 A
5751982 Morley May 1998 A
5752260 Liu May 1998 A
5754818 Mohamed May 1998 A
5761476 Martell Jun 1998 A
5787494 Delano et al. Jul 1998 A
5793941 Pencis et al. Aug 1998 A
5802602 Rahman et al. Sep 1998 A
5806085 Berliner Sep 1998 A
5813031 Chou et al. Sep 1998 A
5819088 Reinders Oct 1998 A
5829028 Lynch et al. Oct 1998 A
5835951 McMahan Nov 1998 A
5852738 Bealkowski et al. Dec 1998 A
5860146 Vishin et al. Jan 1999 A
5864657 Stiffler Jan 1999 A
5872985 Kimura Feb 1999 A
5881277 Bondi et al. Mar 1999 A
5901294 Tran et al. May 1999 A
5903750 Yeh et al. May 1999 A
5905509 Jones et al. May 1999 A
5911057 Shiell Jun 1999 A
5918251 Yamada et al. Jun 1999 A
5956753 Glew et al. Sep 1999 A
5974506 Sicola et al. Oct 1999 A
5978906 Tran Nov 1999 A
5983327 Achilles et al. Nov 1999 A
6016533 Tran Jan 2000 A
6016540 Zaidi et al. Jan 2000 A
6021484 Park Feb 2000 A
6065105 Zaidi et al. May 2000 A
6073230 Pickett et al. Jun 2000 A
6075938 Bugnion et al. Jun 2000 A
6085315 Fleck et al. Jul 2000 A
6088780 Yamada et al. Jul 2000 A
6092172 Nishimoto et al. Jul 2000 A
6101577 Tran Aug 2000 A
6108769 Chinnakonda et al. Aug 2000 A
6115809 Mattson, Jr. et al. Sep 2000 A
6134634 Marshall, Jr. et al. Oct 2000 A
6138226 Yoshioka et al. Oct 2000 A
6157998 Rupley, II et al. Dec 2000 A
6167490 Levy et al. Dec 2000 A
6170051 Dowling Jan 2001 B1
6178482 Sollars Jan 2001 B1
6185660 Mulla et al. Feb 2001 B1
6205545 Shah et al. Mar 2001 B1
6209085 Hammond et al. Mar 2001 B1
6212542 Kahle et al. Apr 2001 B1
6212613 Belair Apr 2001 B1
6216215 Palanca et al. Apr 2001 B1
6226732 Pei et al. May 2001 B1
6247097 Sinharoy Jun 2001 B1
6253316 Tran et al. Jun 2001 B1
6256727 McDonald Jul 2001 B1
6256728 Witt et al. Jul 2001 B1
6260131 Kikuta et al. Jul 2001 B1
6260138 Harris Jul 2001 B1
6269439 Hanaki Jul 2001 B1
6272616 Fernando et al. Aug 2001 B1
6272662 Jadav et al. Aug 2001 B1
6275917 Okada Aug 2001 B1
6282583 Pincus et al. Aug 2001 B1
6282638 Dowling Aug 2001 B1
6308323 Douniwa Oct 2001 B1
6321298 Hubis Nov 2001 B1
6327650 Bapst et al. Dec 2001 B1
6332189 Baweja et al. Dec 2001 B1
6339822 Miller Jan 2002 B1
6341324 Caulk, Jr. et al. Jan 2002 B1
6345357 Sato Feb 2002 B1
6360311 Zandveld et al. Mar 2002 B1
6408367 Achilles et al. Jun 2002 B2
6437789 Tidwell et al. Aug 2002 B1
6449671 Patkar et al. Sep 2002 B1
6457120 Sinharoy Sep 2002 B1
6473833 Arimilli et al. Oct 2002 B1
6490673 Heishi et al. Dec 2002 B1
6502187 Miyagawa Dec 2002 B1
6529928 Resnick et al. Mar 2003 B1
6542984 Keller et al. Apr 2003 B1
6557083 Sperber et al. Apr 2003 B1
6557095 Henstrom Apr 2003 B1
6594755 Nuechterlein et al. Jul 2003 B1
6604187 McGrath et al. Aug 2003 B1
6609189 Kuszmaul et al. Aug 2003 B1
6615340 Wilmot, II Sep 2003 B1
6658549 Wilson et al. Dec 2003 B2
6668316 Gorshtein et al. Dec 2003 B1
6681395 Nishi Jan 2004 B1
6704860 Moore Mar 2004 B1
6721874 Le et al. Apr 2004 B1
6728866 Kahle et al. Apr 2004 B1
6775761 Wang et al. Aug 2004 B2
6829698 Arimilli et al. Dec 2004 B2
6850531 Rao et al. Feb 2005 B1
6882177 Reddy et al. Apr 2005 B1
6907600 Neiger et al. Jun 2005 B2
6912644 O'Connor et al. Jun 2005 B1
6920530 Musumeci Jul 2005 B2
6944744 Ahmed et al. Sep 2005 B2
6948172 D'Souza Sep 2005 B1
6950927 Apisdorf et al. Sep 2005 B1
6954846 Leibholz et al. Oct 2005 B2
6985591 Graunke Jan 2006 B2
6988183 Wong Jan 2006 B1
7007108 Emerson et al. Feb 2006 B2
7020879 Nemirovsky et al. Mar 2006 B1
7047322 Bauman et al. May 2006 B1
7111145 Chen et al. Sep 2006 B1
7117347 Col et al. Oct 2006 B2
7139855 Armstrong et al. Nov 2006 B2
7143273 Miller et al. Nov 2006 B2
7149872 Rozas et al. Dec 2006 B2
7150021 Vajjhala et al. Dec 2006 B1
7171535 Naoi Jan 2007 B2
7203824 Bean et al. Apr 2007 B2
7206925 Jacobson et al. Apr 2007 B1
7213106 Koster et al. May 2007 B1
7213248 Arimilli et al. May 2007 B2
7231106 Basavanhally et al. Jun 2007 B2
7257695 Jiang et al. Aug 2007 B2
7278030 Chen et al. Oct 2007 B1
7284092 Nunamaker et al. Oct 2007 B2
7290261 Burky et al. Oct 2007 B2
7313775 Casey et al. Dec 2007 B2
7343476 Floyd et al. Mar 2008 B2
7373637 Dewitt et al. May 2008 B2
7380096 Rozas et al. May 2008 B1
7383427 Yamazaki Jun 2008 B2
7398347 Pechanek et al. Jul 2008 B1
7406581 Southwell et al. Jul 2008 B2
7418579 Guibert et al. Aug 2008 B2
7418582 Iacobovici et al. Aug 2008 B1
7441110 Puzak et al. Oct 2008 B1
7493475 Colavin Feb 2009 B2
7539879 Terechko et al. May 2009 B2
7546420 Shar et al. Jun 2009 B1
7577820 Wentzlaff et al. Aug 2009 B1
7613131 Decasper et al. Nov 2009 B2
7617384 Coon et al. Nov 2009 B1
7634637 Lindholm et al. Dec 2009 B1
7647483 Bates et al. Jan 2010 B2
7680988 Nickolls et al. Mar 2010 B1
7681019 Favor Mar 2010 B1
7707397 Henry et al. Apr 2010 B2
7707578 Zedlewski et al. Apr 2010 B1
7711929 Burky et al. May 2010 B2
7716460 Stempel et al. May 2010 B2
7757065 Jourdan et al. Jul 2010 B1
7770161 Mitran et al. Aug 2010 B2
7783868 Ukai Aug 2010 B2
7783869 Grandou et al. Aug 2010 B2
7809925 Mejdrich et al. Oct 2010 B2
7848129 Deshpande et al. Dec 2010 B1
7856530 Mu Dec 2010 B1
7861060 Nickolls et al. Dec 2010 B1
7877582 Gschwind et al. Jan 2011 B2
7913058 Rozas et al. Mar 2011 B2
7925869 Kelsey et al. Apr 2011 B2
8044951 Brown et al. Oct 2011 B1
8046775 Kang et al. Oct 2011 B2
8082420 Comparan et al. Dec 2011 B2
8108545 Arimilli et al. Jan 2012 B2
8145844 Bruce Mar 2012 B2
8145880 Cismas et al. Mar 2012 B1
8145882 Kishore et al. Mar 2012 B1
8200949 Tarjan et al. Jun 2012 B1
8219996 Morris Jul 2012 B1
8230423 Frigo et al. Jul 2012 B2
8239656 Rozas et al. Aug 2012 B2
8301847 Dantzig et al. Oct 2012 B2
8316435 Varadhan et al. Nov 2012 B1
8327115 Abdallah Dec 2012 B2
8438366 Akizuki et al. May 2013 B2
8522253 Rozas et al. Aug 2013 B1
8539486 Cain, III et al. Sep 2013 B2
8645965 Zimmer et al. Feb 2014 B2
8756329 Reynolds et al. Jun 2014 B2
8868838 Glasco et al. Oct 2014 B1
8930674 Avudaiyappan et al. Jan 2015 B2
9047178 Talagala et al. Jun 2015 B2
9135003 Suh et al. Sep 2015 B2
9811342 Abdallah et al. Nov 2017 B2
9811377 Abdallah et al. Nov 2017 B2
9823930 Abdallah et al. Nov 2017 B2
20010016901 Topham Aug 2001 A1
20010032303 Pechanek et al. Oct 2001 A1
20010049782 Hsu et al. Dec 2001 A1
20020029308 Babaian et al. Mar 2002 A1
20020062435 Nemirovsky et al. May 2002 A1
20020069326 Richardson et al. Jun 2002 A1
20020082824 Neiger et al. Jun 2002 A1
20020083312 Sinharoy Jun 2002 A1
20020099913 Steely et al. Jul 2002 A1
20020126657 Frouin et al. Sep 2002 A1
20020129085 Kubala et al. Sep 2002 A1
20020174321 John et al. Nov 2002 A1
20020188833 Henry et al. Dec 2002 A1
20030035422 Hill Feb 2003 A1
20030065887 Maiyuran et al. Apr 2003 A1
20030088752 Harman May 2003 A1
20030093776 Hilton May 2003 A1
20030101322 Gardner May 2003 A1
20030101444 Wu et al. May 2003 A1
20030126408 Vajapeyam et al. Jul 2003 A1
20030131335 Hamlin Jul 2003 A1
20030149862 Kadambi Aug 2003 A1
20030163642 Borkenhagen et al. Aug 2003 A1
20030169626 Burk et al. Sep 2003 A1
20030200396 Musumeci Oct 2003 A1
20030200412 Peinado et al. Oct 2003 A1
20030202530 Jenkins et al. Oct 2003 A1
20030225938 Glasco et al. Dec 2003 A1
20030226001 Moyer et al. Dec 2003 A1
20030233394 Rudd et al. Dec 2003 A1
20040034762 Kacevas Feb 2004 A1
20040044850 George et al. Mar 2004 A1
20040064668 Kjos et al. Apr 2004 A1
20040073909 Arimilli et al. Apr 2004 A1
20040078538 Dutt et al. Apr 2004 A1
20040093483 Nguyen et al. May 2004 A1
20040098567 Hansen et al. May 2004 A1
20040103251 Alsup May 2004 A1
20040117593 Uhlig et al. Jun 2004 A1
20040117594 Vanderspek Jun 2004 A1
20040122887 Macy Jun 2004 A1
20040138857 Souza et al. Jul 2004 A1
20040139441 Kaburaki et al. Jul 2004 A1
20040143727 McDonald Jul 2004 A1
20040158822 Sandham et al. Aug 2004 A1
20040172523 Merchant et al. Sep 2004 A1
20040187123 Tremblay et al. Sep 2004 A1
20040193857 Miller et al. Sep 2004 A1
20040202158 Takeno et al. Oct 2004 A1
20040205296 Bearden Oct 2004 A1
20040215886 Cargnoni et al. Oct 2004 A1
20040216105 Burky et al. Oct 2004 A1
20040216120 Burky et al. Oct 2004 A1
20040225872 Bonanno et al. Nov 2004 A1
20050005085 Miyanaga Jan 2005 A1
20050027961 Zhang Feb 2005 A1
20050044547 Gipp Feb 2005 A1
20050055504 Hass et al. Mar 2005 A1
20050060457 Olukotun Mar 2005 A1
20050066131 Biles et al. Mar 2005 A1
20050108480 Correale, Jr. et al. May 2005 A1
20050108715 Kanai et al. May 2005 A1
20050114603 Buti et al. May 2005 A1
20050120191 Akkary et al. Jun 2005 A1
20050120194 Kissell Jun 2005 A1
20050132145 Dybsetter et al. Jun 2005 A1
20050154867 Dewitt et al. Jul 2005 A1
20050204118 Jen et al. Sep 2005 A1
20050216920 Tewari et al. Sep 2005 A1
20050251639 Vishin et al. Nov 2005 A1
20050251649 Yamazaki Nov 2005 A1
20050262270 Latorre et al. Nov 2005 A1
20050289299 Nunamaker et al. Dec 2005 A1
20050289530 Robison Dec 2005 A1
20060004964 Conti et al. Jan 2006 A1
20060026381 Doi et al. Feb 2006 A1
20060026408 Morris et al. Feb 2006 A1
20060036516 Glebe Feb 2006 A1
20060080380 Aizu et al. Apr 2006 A1
20060094446 Duan May 2006 A1
20060095720 Biles et al. May 2006 A1
20060143390 Kottapalli Jun 2006 A1
20060161421 Kissell Jul 2006 A1
20060161921 Kissell Jul 2006 A1
20060179257 Chu et al. Aug 2006 A1
20060179281 Jensen et al. Aug 2006 A1
20060179289 Floyd et al. Aug 2006 A1
20060190707 McIlvaine et al. Aug 2006 A1
20060212687 Chen et al. Sep 2006 A1
20060230243 Cochran et al. Oct 2006 A1
20060230253 Codrescu et al. Oct 2006 A1
20060230409 Frigo et al. Oct 2006 A1
20060236074 Williamson et al. Oct 2006 A1
20060236080 Doing et al. Oct 2006 A1
20060242365 Ali et al. Oct 2006 A1
20060242384 Ahmed et al. Oct 2006 A1
20060256641 Johnstone Nov 2006 A1
20060277365 Pong Dec 2006 A1
20060282839 Hankins et al. Dec 2006 A1
20070006231 Wang et al. Jan 2007 A1
20070074005 Abernathy et al. Mar 2007 A1
20070198665 De Matteis et al. Aug 2007 A1
20070214343 Lindholm et al. Sep 2007 A1
20070226722 Chou Sep 2007 A1
20070262270 Huang et al. Nov 2007 A1
20080016507 Thomas et al. Jan 2008 A1
20080040724 Kang et al. Feb 2008 A1
20080046666 Termaine et al. Feb 2008 A1
20080052432 Wilson et al. Feb 2008 A1
20080077813 Keller et al. Mar 2008 A1
20080091880 Vishin Apr 2008 A1
20080104598 Chang May 2008 A1
20080109611 Liu et al. May 2008 A1
20080126643 Higuchi May 2008 A1
20080126771 Chen et al. May 2008 A1
20080148237 Jiang et al. Jun 2008 A1
20080184211 Nickolls et al. Jul 2008 A1
20080195844 Shen et al. Aug 2008 A1
20080215865 Hino et al. Sep 2008 A1
20080225987 Fazzi et al. Sep 2008 A1
20080235500 Davis et al. Sep 2008 A1
20080250227 Linderman et al. Oct 2008 A1
20080250232 Nakashima Oct 2008 A1
20080256278 Thomas et al. Oct 2008 A1
20080256330 Wang et al. Oct 2008 A1
20080270758 Ozer et al. Oct 2008 A1
20080270774 Singh et al. Oct 2008 A1
20080282037 Kusachi et al. Nov 2008 A1
20080320476 Wingard et al. Dec 2008 A1
20090019264 Correale, Jr. et al. Jan 2009 A1
20090031104 Vorbach et al. Jan 2009 A1
20090070554 Wang et al. Mar 2009 A1
20090113170 Abdallah Apr 2009 A1
20090119457 Latorre et al. May 2009 A1
20090138659 Lauterbach May 2009 A1
20090138670 Mutlu et al. May 2009 A1
20090150647 Mejdrich et al. Jun 2009 A1
20090150890 Yourst Jun 2009 A1
20090157980 Bruce Jun 2009 A1
20090158017 Mutlu et al. Jun 2009 A1
20090164733 Kim et al. Jun 2009 A1
20090164766 Suggs et al. Jun 2009 A1
20090165007 Aghajanyan Jun 2009 A1
20090172344 Grochowski et al. Jul 2009 A1
20090240919 Alexander et al. Sep 2009 A1
20090241084 Malley et al. Sep 2009 A1
20090249026 Smelyanskiy et al. Oct 2009 A1
20090251476 Jiao et al. Oct 2009 A1
20090282101 Lim et al. Nov 2009 A1
20090287912 Sendag Nov 2009 A1
20090307450 Lee Dec 2009 A1
20090313462 Emma et al. Dec 2009 A1
20090328053 Dice Dec 2009 A1
20100058033 Abernathy et al. Mar 2010 A1
20100064121 Alexander et al. Mar 2010 A1
20100082912 Lesartre et al. Apr 2010 A1
20100088443 Riocreux et al. Apr 2010 A1
20100100690 Rajamani et al. Apr 2010 A1
20100100704 Hill et al. Apr 2010 A1
20100100707 Mejdrich et al. Apr 2010 A1
20100115167 Tardieux et al. May 2010 A1
20100115244 Jensen et al. May 2010 A1
20100138607 Hughes et al. Jun 2010 A1
20100154042 Miyamoto et al. Jun 2010 A1
20100161948 Abdallah Jun 2010 A1
20100169578 Nychka et al. Jul 2010 A1
20100169611 Chou et al. Jul 2010 A1
20100205603 Merten et al. Aug 2010 A1
20100211746 Tsukishiro Aug 2010 A1
20100280996 Gross, IV et al. Nov 2010 A1
20100286976 Gao et al. Nov 2010 A1
20100299671 Kinsey Nov 2010 A1
20100306503 Henry et al. Dec 2010 A1
20100325394 Golla et al. Dec 2010 A1
20100332805 Blasco et al. Dec 2010 A1
20110010521 Wang et al. Jan 2011 A1
20110055479 West et al. Mar 2011 A1
20110067016 Mizrachi et al. Mar 2011 A1
20110082980 Gschwind et al. Apr 2011 A1
20110082983 Koktan Apr 2011 A1
20110093857 Sydow et al. Apr 2011 A1
20110119660 Tanaka May 2011 A1
20110153955 Herrenschmidt et al. Jun 2011 A1
20110225588 Pollock et al. Sep 2011 A1
20120005462 Hall et al. Jan 2012 A1
20120023318 Xing et al. Jan 2012 A1
20120042105 Maeda et al. Feb 2012 A1
20120042126 Krick et al. Feb 2012 A1
20120066483 Boury et al. Mar 2012 A1
20120089812 Smith Apr 2012 A1
20120096204 Auerbach et al. Apr 2012 A1
20120198209 Abdallah et al. Aug 2012 A1
20120246450 Abdallah et al. Sep 2012 A1
20120246657 Abdallah et al. Sep 2012 A1
20120278593 Clark et al. Nov 2012 A1
20130019047 Podvalny et al. Jan 2013 A1
20130036296 Hickey et al. Feb 2013 A1
20130046934 Nychka et al. Feb 2013 A1
20130086417 Sivaramakrishnan et al. Apr 2013 A1
20130097369 Talagala et al. Apr 2013 A1
20130238874 Avudaiyappan et al. Sep 2013 A1
20130283286 Lee et al. Oct 2013 A1
20130304991 Boettcher et al. Nov 2013 A1
20130311759 Abdallah et al. Nov 2013 A1
20130339671 Williams, III et al. Dec 2013 A1
20130346699 Walker Dec 2013 A1
20140032844 Avudaiyappan et al. Jan 2014 A1
20140032845 Avudaiyappan et al. Jan 2014 A1
20140032856 Avudaiyappan et al. Jan 2014 A1
20140075168 Abdallah Mar 2014 A1
20140108730 Avudaiyappan et al. Apr 2014 A1
20140123145 Barrow-Williams et al. May 2014 A1
20140156947 Avudaiyappan Jun 2014 A1
20140181833 Bird et al. Jun 2014 A1
20140281242 Abdallah et al. Sep 2014 A1
20140281411 Abdallah Sep 2014 A1
20140281412 Abdallah et al. Sep 2014 A1
20140281416 Abdallah Sep 2014 A1
20140281426 Abdallah et al. Sep 2014 A1
20140281427 Abdallah Sep 2014 A1
20140281428 Abdallah et al. Sep 2014 A1
20140281436 Abdallah Sep 2014 A1
20140282592 Abdallah et al. Sep 2014 A1
20140282601 Abdallah Sep 2014 A1
20140317387 Abdallah et al. Oct 2014 A1
20140344554 Abdallah Nov 2014 A1
20140373022 Chan et al. Dec 2014 A1
20150039859 Abdallah Feb 2015 A1
20150046683 Abdallah Feb 2015 A1
20150046686 Abdallah Feb 2015 A1
20150186144 Abdallah Jul 2015 A1
20160041908 Avudaiyappan et al. Feb 2016 A1
20160041913 Avudaiyappan et al. Feb 2016 A1
20160041930 Avudaiyappan Feb 2016 A1
20160154653 Abdallah Jun 2016 A1
20160210145 Abdallah Jul 2016 A1
20160210176 Abdallah Jul 2016 A1
20160371188 Abdallah Dec 2016 A1
Foreign Referenced Citations (59)
Number Date Country
1214666 Apr 1999 CN
1305150 Jul 2001 CN
1451115 Oct 2003 CN
1214666 Aug 2005 CN
1713137 Dec 2005 CN
1774709 May 2006 CN
1841314 Oct 2006 CN
1841332 Oct 2006 CN
1848095 Oct 2006 CN
1881223 Dec 2006 CN
101114218 Jan 2008 CN
101151594 Mar 2008 CN
101241428 Aug 2008 CN
101344840 Jan 2009 CN
101449256 Jun 2009 CN
101582025 Nov 2009 CN
101627365 Jan 2010 CN
101916180 Dec 2010 CN
102105864 Jun 2011 CN
0596636 May 1994 EP
0706133 Apr 1996 EP
2616928 Jul 2013 EP
2343270 May 2000 GB
2000330790 Nov 2000 JP
20010050794 Jun 2001 KR
20010053622 Jun 2001 KR
20100003309 Jan 2010 KR
200707284 Mar 1995 TW
539996 Jul 2003 TW
544626 Aug 2003 TW
200401187 Jan 2004 TW
200405201 Apr 2004 TW
591530 Jun 2004 TW
200422949 Nov 2004 TW
I233545 Jun 2005 TW
I281121 May 2007 TW
200813766 Mar 2008 TW
200844853 Nov 2008 TW
200941339 Oct 2009 TW
I315488 Oct 2009 TW
200949690 Dec 2009 TW
I329437 Aug 2010 TW
I331282 Oct 2010 TW
I352288 Nov 2011 TW
201227520 Jul 2012 TW
201241744 Oct 2012 TW
201305819 Feb 2013 TW
9750031 Dec 1997 WO
9919793 Apr 1999 WO
0125921 Apr 2001 WO
2004114128 Dec 2004 WO
2007027671 Mar 2007 WO
2008021434 Feb 2008 WO
2008061154 May 2008 WO
2009012296 Jan 2009 WO
2009101563 Aug 2009 WO
2010049585 May 2010 WO
2012135031 Oct 2012 WO
2012135050 Oct 2012 WO
Non-Patent Literature Citations (369)
Entry
Abandonment from U.S. Appl. No. 13/824,013, dated Mar. 3, 2015, 1 page.
Advisory Action from U.S. Appl. No. 12/296,919, dated Aug. 26, 2011, 3 pages.
Advisory Action from U.S. Appl. No. 14/214,280, dated May 15, 2017, 3 pages.
Barham P., et al., “Xen and the Art of Virtualization,” Proceedings of the ACM Symposium on Operating Systems Principles, XP002298786, Oct. 2003, pp. 164-177.
Communication pursuant to Article 94(3) EPC for European Application No. 070864410, dated Mar. 16, 2012, 4 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 070864410, dated Nov. 14, 2012, 4 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 07811845, dated Apr. 16, 2014, 5 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 07811845, dated Dec. 21, 2015, 3 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 07811845, dated Feb. 3, 2014, 5 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 07811845, dated Feb. 16, 2011, 6 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 07811845, dated Jan. 27, 2012, 7 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12150513, dated Apr. 16, 2013, 5 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12150513, dated Dec. 21, 2015, 4 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12150513, dated May 9, 2014, 8 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12174228, dated Jun. 11, 2013, 3 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12764627, dated Oct. 4, 2016, 4 pages.
Communication pursuant to Article 94(3) EPC for European Application No. 12788989.7, dated Jun. 22, 2017, 6 pages.
Communication pursuant to Rules 161(2) and 162 EPC for Application No. 12763717, dated Nov. 22, 2013, 3 pages.
Communication pursuant to Rules 70(2) and 70a(2) EPC for Application No. 12763717, dated Oct. 10, 2014, 1 page.
Communication pursuant to Rules 70(2) and 70a(2) EPC for European Application No. 11876314.3, dated Jul. 1, 2016, 1 page.
Cooperman, “Cache Basics,” Winter 2003, downloaded from http://www.ccs.neu.edu/course/com3200/parent/NOTES/cache-basics.html on Sep. 24, 2015, 3 pages. (no publication month available).
Decision to Grant a Patent for European Application No. 07811845, dated Jun. 16, 2016, 2 pages.
Decision to Grant a Patent for European Application No. 12150513, dated Jun. 16, 2016, 2 pages.
Decision to Grant a Patent for European Application No. 12174228, dated Dec. 13, 2013, 5 pages.
Decision to Grant a Patent for Korean Application No. KR1020137027843, dated Apr. 29, 2016, 2 pages.
Decision to Grant a Patent for Korean Patent Application No. 20137027842, dated Mar. 31, 2016, 2 pages.
Decision to grant a patent from foreign counterpart Korean Patent Application No. 10-2014-7016774, dated Jul. 25, 2016, 2 pages.
Decision to Grant a Patent from foreign counterpart Korean Patent Application No. 20137033565, dated Apr. 29, 2016, 2 pages.
Decision to Grant a Patent from foreign counterpart Korean Patent Application No. 20137033566, dated Apr. 29, 2016, 2 pages.
Decision to Grant a Patent from foreign counterpart Korean Patent Application No. KR1020157029107, dated Apr. 25, 2017, 2 pages.
Examination Report for European Application No. 12763717, dated Nov. 28, 2016, 5 pages.
Extended European Search Report for Application No. 07811845.2, dated Nov. 2, 2009, 7 pages.
Extended European Search Report for Application No. 07864410, dated Feb. 19, 2010, 8 pages.
Extended European Search Report for Application No. 11876314.3, dated Jun. 14, 2016, 6 pages.
Extended European Search Report for Application No. 12150513, dated Jun. 19, 2012, 8 pages.
Extended European Search Report for Application No. 12174228, dated Oct. 16, 2012, 4 pages.
Extended European Search Report for Application No. 12174229, dated Jul. 4, 2014, 10 pages.
Extended European Search Report for Application No. 12788989, dated May 12, 2016, 9 pages.
Extended European Search Report for Application No. 12789667, dated Feb. 26, 2016, 7 pages.
Extended European Search Report for Application No. 14769411.1, dated Apr. 5, 2017, 8 pages.
Extended European Search Report for Application No. 14769450.9, dated Feb. 21, 2017, 16 pages.
Extended European Search Report for Application No. 14770976.0, dated Jul. 3, 2017, 9 pages.
Extended European Search Report for Application No. 16196777.3, dated Mar. 20, 2017, 6 pages.
Extended European Search Report for Application No. EP11826042, dated Jan. 24, 2014, 6 pages.
Extended European Search Report for Application No. EP11876128, dated Jun. 21, 2016, 8 pages.
Extended European Search Report for Application No. EP11876130, dated Jun. 1, 2016, 7 pages.
Extended European Search Report for Application No. EP12763717, dated Sep. 24, 2014, 5 pages.
Extended European Search Report for Application No. EP12764627, dated Jul. 10, 2014, 5 pages.
Extended European Search Report for Application No. EP12764838, dated Jul. 10, 2014, 5 pages.
Final Office Action from U.S. Appl. No. 12/296,919, dated Jun. 14, 2011, 7 pages.
Advisory Action from U.S. Appl. No. 14/212,203, dated Apr. 5, 2018, 8 pages.
Communication pursuant to Article 94(3) EPC for Application No. 14770976.0, dated Mar. 16, 2018, 4 pages.
Non-Final Office Action from U.S. Appl. No. 15/862,496, dated Apr. 5, 2018, 151 pages.
Notice of Allowance from U.S. Appl. No. 14/216,493, dated Apr. 2, 2018, 22 pages.
Communication pursuant to Article 94(3) EPC for Application No. 11876128.7, dated Feb. 5, 2018, 9 pages.
Communication pursuant to Article 94(3) EPC for Application No. 11876130.3, dated Feb. 5, 2018, 9 pages.
Communication pursuant to Article 94(3) EPC for Application No. 11876314.3, dated Feb. 5, 2018, 8 pages.
Communication pursuant to Article 94(3) EPC for Application No. 12789667.8, dated Feb. 21, 2018, 4 pages.
Corrected Notice of Allowance from U.S. Appl. No. 13/475,708, dated Feb. 14, 2018, 27 pages.
Corrected Notice of Allowance from U.S. Appl. No. 13/475,708, dated Feb. 26, 2018, 31 pages.
Corrected Notice of Allowance from U.S. Appl. No. 15/357,943, dated Apr. 2, 2018, 4 pages.
First Office Action and Search Report from foreign counterpart Chinese Patent Application No. 201480024528.0, dated Jan. 26, 2018, 19 pages.
First Office Action and Search Report from foreign counterpart Chinese Patent Application No. 201480024832.5, dated Feb. 6, 2018, 15 pages. (Translation available only for office action).
Intention to grant from foreign counterpart European Patent Application No. 12788989.7, dated Feb. 23, 2018, 47 pages.
Notice of Allowance from U.S. Appl. No. 15/082,359, dated Mar. 21, 2018, 9 pages.
Notice of Allowance from U.S. Appl. No. 15/219,063, dated Mar. 19, 2018, 28 pages.
Notice on Grant of Patent Right for Invention from foreign counterpart Chinese Patent Application No. 201180076248.0, dated Feb. 27, 2018, 6 pages.
Notice on Grant of Patent Right for Invention from foreign counterpart Chinese Patent Application No. 201280024012.7, dated Mar. 12, 2018, 4 pages.
Advisory Action from U.S. Appl. No. 14/360,282, dated Jan. 23, 2018, 2 pages.
Final Office Action from U.S. Appl. No. 15/082,359, dated Jan. 31, 2018, 22 pages.
Non-Final Office Action from U.S. Appl. No. 13/824,013, dated Feb. 7, 2018, 141 pages.
Notice of Allowance from foreign counterpart Korean Patent Application No. 10-2017-7002379, dated Dec. 20, 2017, 3 pages.
Notice of Allowance from foreign counterpart Korean Patent Application No. 10-2017-7002473, dated Dec. 20, 2017, 6 pages.
Notice of Allowance from U.S. Appl. No. 15/082,867, dated Dec. 22, 2017, 25 pages.
Notice of Allowance from U.S. Appl. No. 15/357,943, dated Jan. 16, 2018, 16 pages.
Notice of Allowance from U.S. Appl. No. 14/216,493, dated Aug. 4, 2017, 95 pages.
Notice of Allowance from U.S. Appl. No. 14/216,859, dated Dec. 1, 2017, 113 pages.
Notice of Allowance from U.S. Appl. No. 14/216,859, dated Jan. 24, 2017, 17 pages.
Notice of Allowance from U.S. Appl. No. 14/360,284, dated Jun. 14, 2017, 100 pages.
Notice of Allowance from U.S. Appl. No. 14/733,827, dated Sep. 22, 2017, 30 pages.
Notice of Allowance from U.S. Appl. No. 15/019,920, dated Dec. 6, 2017, 24 pages.
Notice of Allowance from U.S. Appl. No. 15/019,920, dated Jul. 14, 2017, 100 pages.
Notice of Allowance from U.S. Appl. No. 15/082,867, dated Jul. 7, 2017, 98 pages.
Notice of Allowance from U.S. Appl. No. 15/257,593, dated Oct. 11, 2017, 95 pages.
Notice of Final Rejection from foreign counterpart Korean Patent Application No. 10-2015-7029262, dated May 23, 2017, 7 pages.
Notice of Preliminary Rejection from foreign counterpart Korean Patent Application No. 10-2016-7017150, dated Apr. 20, 2017, 5 pages.
Notice on Grant of Patent Right for Invention from foreign counterpart China Application No. 201180076244.2, dated Aug. 28, 2017, 4 pages.
Notice on Grant of Patent Right for Invention from foreign counterpart Chinese Patent Application No. 201280024054.0, dated Dec. 1, 2017, 4 pages.
Notice on Grant of Patent Right for Invention from foreign counterpart Chinese Patent Application No. 201280024095.X, dated Nov. 7, 2017, 6 pages.
Notification of Reason for Refusal from Foreign Counterpart Korean Patent Application No. 10-2013-7027842, dated Sep. 18, 2015, 7 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 10-2014-7016774, dated Jan. 28, 2016, 4 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 10-2015-7029262, dated Oct. 17, 2016, 12 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 10-2017-7002379, dated May 26, 2017, 6 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 10-2017-7002473, dated May 26, 2017, 7 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 20137027841, dated Sep. 18, 2015, 10 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 20137033565, dated Sep. 30, 2015, 6 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. 20137033566, dated Sep. 30, 2015, 9 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. KR1020137027843, dated Sep. 30, 2015, 8 pages.
Notification of Reason for Refusal from foreign counterpart Korean Patent Application No. KR1020157029107, dated Oct. 13, 2016, 11 pages.
Notification of Reason for Refusal from Korean Application No. 10-2014-7016763, dated Apr. 29, 2016, 11 pages.
Notification of Reason for Refusal from Korean Application No. 10-2015-7028745, dated May 23, 2016, 8 pages.
Notification to Grant Patent Right for Invention from foreign counterpart China Patent Application No. 201180076245.7, dated Nov. 2, 2016, 3 pages.
Notification to Grant Patent Right for Invention from foreign counterpart China Patent Application No. CN201280034725, dated Aug. 12, 2016, 3 pages.
Notification to Grant Patent Right for Invention from foreign counterpart China Patent Application No. CN201310589048, dated May 5, 2016, 3 pages.
Nuth, et al., “The Named-State Register File: Implementation and Performance,” High-Performance Computer Architecture, First IEEE Symposium, Jan. 22-25, 1995, 10 pages.
Office Action and Search Report from foreign counterpart Taiwan Patent Application No. 100142885, dated Jan. 23, 2017, 12 pages.
Office Action and Search Report from foreign counterpart Taiwan Patent Application No. 101117854, dated Mar. 30, 2017, 7 pages.
Office Action from foreign counterpart Chinese Patent Application No. 200780046679, dated May 21, 2013, 14 pages.
Office Action from foreign counterpart Chinese patent application No. 201280024012, dated Feb. 3, 2017, 20 pages.
Office Action from foreign counterpart Chinese patent application No. 201280024095, dated Feb. 4, 2017, 31 pages.
Office Action from foreign counterpart European Patent Application No. EP12764838, dated Oct. 4, 2016, 4 pages.
Office Action from foreign counterpart Taiwan Patent Application No. 20140109479, dated Nov. 28, 2016, 7 pages.
Partial European Search Report for Application No. 12174229, dated Oct. 10, 2012, 7 pages.
Partial Supplementary European Search Report for Application No. 14769450.9, dated Oct. 11, 2016, 8 pages.
Partial Supplementary European Search Report for Application No. EP14770976.0, dated Mar. 24, 2017, 7 pages.
Restriction Requirement from U.S. Appl. No. 12/296,919, dated Feb. 8, 2011, 4 pages.
Restriction Requirement from U.S. Appl. No. 12/514,303, dated Oct. 15, 2012, 4 pages.
Restriction Requirement from U.S. Appl. No. 14/360,282, dated Jul. 28, 2016, 4 pages.
Rixner, et al., “Register Organization for Media Processing,” HPCA-6—Proceedings of the 6th International Symposium on High-Performance Computer Architecture, Jan. 8-12, 2000, IEEE, Toulouse, France, pp. 375-386.
Rotenberg, et al., “Trace Cache: a Low Latency Approach to High Bandwidth Instruction Fetching,” MICRO 29—Proceedings of the 29th annual ACM/IEEE international symposium on Microarchitecture, IEEE Computer Society, Apr. 11, 1996, 48 pages.
Santos, et al., “The 2D-VLIW Architecture,” Technical Report IC-06-006, Instituto de Computacao, Universidad Estadual de Campinas, Mar. 2006, 13 pages.
Sassone et al., “Dynamic Strands: Collapsing Speculative Dependence Chains for Reducing Pipeline Communication,” Microarchitecture, IEEE, 37th International Symposium on Portland, USA Dec. 2004, pp. 7-17, Piscataway, NJ, USA.
Search Report for Chinese Application No. CN201280024012, dated May 19, 2016, 2 pages.
Second Office Action from foreign counterpart China Patent Application No. 201180076248.0, dated Oct. 20, 2016, 25 pages.
Second Office Action from foreign counterpart China Patent Application No. 201480024463.X, dated Nov. 14, 2017, 34 pages.
Second Office Action from foreign counterpart China Patent Application No. CN201280034725, dated Apr. 14, 2016, 8 pages.
Second Office Action from foreign counterpart China Patent Application No. CN201280034739, dated Jun. 23, 2016, 44 pages.
Second Office Action from foreign counterpart Chinese Patent Application No. 201280024054.0, dated Dec. 26, 2016, 11 pages.
Second Office Action with search report from foreign counterpart Chinese Patent Application No. 201180076244, dated Nov. 18, 2016, 21 pages (Translation available only for Office Action).
Summons to attend Oral Proceedings for European Application No. 070864410, dated Apr. 3, 2013, 3 pages.
Sun, et al., “Modeling of FPGA Local/Global Interconnect Resources and Derivation of Minimal Test Configuration,” Proceedings of the 17th IEEE International Symposium on Defect and Fault Tolerance in VLSI Systems (DFT'02), IEEE Computer Society, Nov. 6-8, 2002, 9 pages.
Third Office Action and Search report from foreign counterpart China Patent Application No. 201180076248.0, dated May 2, 2017, 27 pages.
Third Office Action from foreign counterpart China Patent Application No. 201280024054.0, dated Jul. 28, 2017, 8 pages.
Third Office Action from foreign counterpart Chinese Patent Application No. 201180076244.2, dated May 2, 2017, 20 pages.
Third Office Action from foreign counterpart Chinese Patent Application No. 201280024012.7, dated Nov. 6, 2017, 8 pages.
Third Office Action from foreign counterpart Chinese Patent Application No. 201280034739, dated Dec. 27, 2016, 18 pages.
Wallace, et al.,“Multiple Branch and Block Prediction,” Third International symposium on High-Performance Computer Architecture, IEEE, Feb. 1997, pp. 94-103.
Written Opinion for Application No. PCT/US2007/066536, dated Jul. 30, 2008, 5 pages.
Ye, et al., “A New Recovery Mechanism in Superscalar Microprocessors by Recovering Critical Misprediction,” IEICE Transactions on Fundamentals of Electronics, Communications and Computer Sciences, The Institute of Electronics, Information and Communication Engineers, Dec. 1, 2011, vol. E94-A (12), pp. 2639-2648.
Yeh, et al., “Increasing the Instruction Fetch Rate Via Multiple Branch Prediction and a Branch Address Cache,” ICS 93, Proceedings of the 7th International Conference on Supercomputing, ACM, New York, NY, Jul. 19-23, 1993, pp. 67-76.
Grant of Patent for Korean Application No. 10-2014-7016763, dated Oct. 31, 2016, 2 pages.
Grant of Patent for Korean Application No. 10-2015-7028745, dated Nov. 30, 2016, 2 pages.
Hu, et al., “An Approach for Implementing Efficient Superscalar CISC Processors,” High Performance Computer Architecture, 2006, Twelfth International Symposium on Austin, Texas Feb. 11-15, 2006, pp. 40-51.
Intel “Programming on Intel® Platform,” The edition team of Intel® Software College course book, Shanghai Jiao Tong University Press, published Jan. 31, 2011, pp. 175-180.
Intention to Grant a patent for European Application No. 07811845, dated Mar. 31, 2016, 58 pages.
Intention to Grant a patent for European Application No. 12150513, dated Mar. 15, 2016, 59 pages.
International Preliminary Report on Patentability and for Application No. PCT/US2007/084710, dated May 19, 2009, 4 pages.
International Preliminary Report on Patentability and Written Opinion for Application No. PCT/US2007/066536, dated Oct. 14, 2008, 6 pages.
International Preliminary Report on Patentability and Written Opinion for Application No. PCT/US2012/038711, dated Nov. 20, 2013, 5 pages.
International Preliminary Report on Patentability and Written Opinion for Application No. PCT/US2012/038713, dated Nov. 20, 2013, 5 pages.
International Preliminary Report on Patentability for Application No. PCT/US2011/051992, dated Mar. 28, 2013, 8 pages.
International Preliminary Report on Patentability for Application No. PCT/US2011/061940, dated Jun. 5, 2014, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2011/061953, dated Jun. 5, 2014, 7 pages.
International Preliminary Report on Patentability for Application No. PCT/US2011/061957, dated Jun. 5, 2014, 7 pages.
International Preliminary Report on Patentability for Application No. PCT/US2012/030383, dated Oct. 10, 2013, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2012/030409, dated Oct. 10, 2013, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2012/30360, dated Oct. 10, 2013, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024276, dated Sep. 24, 2015, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024608, dated Sep. 24, 2015, 8 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024677, dated Sep. 24, 2015, 7 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024722, dated Sep. 24, 2015, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024775, dated Sep. 24, 2015, 6 pages.
International Preliminary Report on Patentability for Application No. PCT/US2014/024828, dated Sep. 24, 2015, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2007/084710, dated May 22, 2008, 6 pages.
International Search Report and Written Opinion for Application No. PCT/US2011/051992, dated Mar. 28, 2012, 11 pages.
International Search Report and Written Opinion for Application No. PCT/US2011/061940, dated Jul. 20, 2012, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2011/061953, dated Jul. 24, 2012, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2011/061957, dated Jul. 20, 2012, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2012/030383, dated Oct. 25, 2012, 8 pages.
International Search Report and Written Opinion for Application No. PCT/US2012/030409, dated Oct. 12, 2012, 7 pages.
International Search Report and Written opinion for Application No. PCT/US2012/038711, dated Nov. 28, 2012, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2012/038713, dated Oct. 29, 2012, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2012/30360, dated Oct. 29, 2012, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024276, dated Jul. 31, 2014, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024608, dated Jul. 31, 2014, 9 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024677, dated Jun. 30, 2014, 9 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024722, dated Jun. 27, 2014, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024775, dated Jun. 2, 2014, 7 pages.
International Search Report and Written Opinion for Application No. PCT/US2014/024828, dated Jul. 28, 2014, 9 pages.
International Search Report for Application No. PCT/US2007/066536, dated Jul. 30, 2008, 2 pages.
Jacobson, et al., “Path-based Next Trace Prediction,” MICRO 30—Proceedings of the 30th Annual IEEE/ACM International Symposium on Microarchitecture, Dec. 1-3, 1997, IEEE Computer Society, Washington, D.C., 1997, pp. 14-23.
Kozyrakis, et al., “A New Direction for Computer Architecture Research,” Computer, IEEE Computer Society Press, Los Alamitos, CA, Nov. 1, 1998, vol. 31 (11), pp. 24-32.
Mogul, et al., “Potential Benefits of Delta Encoding and Data Compression for HTTP,” Oct. 1, 1997, ACM, SIGCOMM '97, pp. 181-194.
Nagarajan, et al., “A Design Space Evaluation of Grid Processor Architectures,” 34th ACM/IEEE International Symposium, Piscataway, NJ, Dec. 1-5, 2001, pp. 40-51.
Nanda, et al., “The Misprediction Recovery Cache,” International Journal of Parallel Programming—Special issue: MICRO-29, 29th annual IEEE/ACM international symposium on microarchitecture, Plenum Press, New York, NY, Aug. 1998, vol. 26 (4), pp. 383-415.
Non-Final Office Action from U.S. Appl. No. 12/296,919, dated Apr. 7, 2011, 8 pages.
Non-Final Office Action from U.S. Appl. No. 12/296,919, dated Jun. 14, 2010, 7 pages.
Non-Final Office Action from U.S. Appl. No. 12/296,919, dated Mar. 7, 2012, 7 pages.
Non-Final Office Action from U.S. Appl. No. 12/514,303, dated Jun. 27, 2013, 7 pages.
Non-Final Office Action from U.S. Appl. No. 12/514,303, dated May 10, 2012, 9 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,438, dated Apr. 24, 2014, 15 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,438, dated May 1, 2015, 12 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,440, dated Jun. 18, 2014, 16 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,440, dated May 4, 2015, 13 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,452, dated Apr. 23, 2015, 11 pages.
Non-Final Office Action from U.S. Appl. No. 13/428,452, dated Apr. 28, 2014, 21 pages.
Non-Final Office Action from U.S. Appl. No. 13/475,708, dated Feb. 11, 2015, 27 pages.
Non-Final Office Action from U.S. Appl. No. 13/475,708, dated Feb. 12, 2016, 37 pages.
Non-Final Office Action from U.S. Appl. No. 13/475,739, dated May 21, 2015, 14 pages.
Non-Final Office Action from U.S. Appl. No. 13/475,739, dated Sep. 2, 2014, 15 pages.
Non-Final Office Action from U.S. Appl. No. 13/691,609, dated Jan. 15, 2014, 5 pages.
Non-Final Office Action from U.S. Appl. No. 13/691,609, dated Sep. 5, 2013, 11 pages.
Non-Final Office Action from U.S. Appl. No. 14/194,589, dated Nov. 19, 2015, 12 pages.
Non-Final Office Action from U.S. Appl. No. 14/212,203, dated Mar. 24, 2017, 68 pages.
Non-Final Office Action from U.S. Appl. No. 14/212,203, dated Sep. 8, 2016, 52 pages.
Non-Final Office Action from U.S. Appl. No. 14/212,533, dated Apr. 20, 2017, 116 pages.
Non-Final Office Action from U.S. Appl. No. 14/212,533, dated Sep. 22, 2016, 52 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,115, dated Oct. 19, 2015, 24 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,115, dated Sep. 22, 2014, 19 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,135, dated May 14, 2015, 23 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,135, dated May 31, 2016, 14 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,218, dated Apr. 22, 2015, 22 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,218, dated Feb. 2, 2016, 17 pages.
Non-final Office Action from U.S. Appl. No. 14/213,692, dated Aug. 24, 2015, 30 pages.
Non-final Office Action from U.S. Appl. No. 14/213,692, dated Jun. 13, 2016, 17 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,730, dated Jan. 7, 2016, 27 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,854, dated Apr. 29, 2016, 13 pages.
Non-Final Office Action from U.S. Appl. No. 14/213,854, dated Jun. 19, 2015, 23 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,045, dated Apr. 1, 2016, 61 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,045, dated Dec. 19, 2016, 88 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,176, dated Jan. 6, 2017, 36 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,176, dated Mar. 25, 2016, 25 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,280, dated Jan. 6, 2017, 14 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,280, dated Jun. 16, 2016, 12 pages.
Non-Final Office Action from U.S. Appl. No. 14/214,280, dated Sep. 18, 2015, 18 pages.
Non-Final Office Action from U.S. Appl. No. 14/215,633, dated Oct. 22, 2015, 18 pages.
Non-final Office Action from U.S. Appl. No. 14/216,493, dated Apr. 4, 2016, 26 pages.
Non-Final Office Action from U.S. Appl. No. 14/216,493, dated Mar. 29, 2017, 18 pages.
Non-Final Office Action from U.S. Appl. No. 14/216,859, dated Jan. 28, 2016, 33 pages.
Non-Final Office Action from U.S. Appl. No. 14/360,280, dated Dec. 14, 2017, 25 pages.
Non-Final Office Action from U.S. Appl. No. 14/360,280, dated Feb. 23, 2017, 34 pages.
Non-Final Office Action from U.S. Appl. No. 14/360,282, dated Jun. 22, 2017, 97 pages.
Non-Final Office Action from U.S. Appl. No. 14/360,282, dated Oct. 21, 2016, 13 pages.
Non-final Office Action from U.S. Appl. No. 14/360,284, dated Oct. 21, 2016, 32 pages.
Non-Final Office Action from U.S. Appl. No. 14/733,827, dated Apr. 28, 2017, 99 pages.
Non-Final Office Action from U.S. Appl. No. 15/082,359, dated Aug. 11, 2017, 108 pages.
Non-Final Office Action from U.S. Appl. No. 15/219,063, dated May 30, 2017, 102 pages.
Non-Final Office Action from U.S. Appl. No. 15/257,593, dated Apr. 7, 2017, 37 pages.
Non-final Office Action from U.S. Appl. No. 15/354,742, dated Aug. 25, 2017, 152 pages.
Non-Final Office Action from U.S. Appl. No. 15/354,857, dated Sep. 12, 2017, 111 pages.
Final Office Action from U.S. Appl. No. 12/296,919, dated Oct. 22, 2010, 7 pages.
Final Office Action from U.S. Appl. No. 12/514,303, dated Jan. 24, 2013, 11 pages.
Final Office Action from U.S. Appl. No. 13/428,438, dated Dec. 24, 2014, 17 pages.
Final Office Action from U.S. Appl. No. 13/428,440, dated Dec. 24, 2014, 19 pages.
Final Office Action from U.S. Appl. No. 13/428,452, dated Dec. 24, 2014, 20 pages.
Final Office Action from U.S. Appl. No. 13/475,708, dated Jun. 9, 2016, 35 pages.
Final Office Action from U.S. Appl. No. 13/475,708, dated May 8, 2015, 23 pages.
Final Office Action from U.S. Appl. No. 13/475,739, dated Feb. 4, 2015, 12 pages.
Final Office Action from U.S. Appl. No. 13/475,739, dated Nov. 23, 2015, 28 pages.
Final Office Action from U.S. Appl. No. 14/194,589, dated Apr. 19, 2016, 7 pages.
Final Office Action from U.S. Appl. No. 14/212,203, dated Dec. 13, 2016, 20 pages.
Final Office Action from U.S. Appl. No. 14/212,203, dated Sep. 12, 2017, 84 pages.
Final Office Action from U.S. Appl. No. 14/212,533, dated Jan. 4, 2017, 27 pages.
Final Office Action from U.S. Appl. No. 14/212,533, dated Sep. 8, 2017, 69 pages.
Final Office Action from U.S. Appl. No. 14/213,115, dated Feb. 3, 2015, 11 pages.
Final Office Action from U.S. Appl. No. 14/213,115, dated Mar. 7, 2016, 18 pages.
Final Office Action from U.S. Appl. No. 14/213,135, dated Oct. 26, 2015, 20 pages.
Final Office Action from U.S. Appl. No. 14/213,218, dated Jul. 6, 2016, 24 pages.
Final Office Action from U.S. Appl. No. 14/213,218, dated Jul. 22, 2015, 16 pages.
Final Office Action from U.S. Appl. No. 14/213,692, dated Jan. 20, 2016, 18 pages.
Final Office Action from U.S. Appl. No. 14/213,730, dated May 11, 2016, 14 pages.
Final Office Action from U.S. Appl. No. 14/213,854, dated Nov. 9, 2015, 19 pages.
Final Office Action from U.S. Appl. No. 14/214,045, dated Aug. 29, 2016, 14 pages.
Final Office Action from U.S. Appl. No. 14/214,176, dated Aug. 29, 2016, 17 pages.
Final Office Action from U.S. Appl. No. 14/214,280, dated Mar. 6, 2017, 12 pages.
Final Office Action from U.S. Appl. No. 14/214,280, dated Mar. 11, 2016, 18 pages.
Final Office Action from U.S. Appl. No. 14/214,280, dated Oct. 24, 2016, 20 pages.
Final Office Action from U.S. Appl. No. 14/216,493, dated Aug. 30, 2016, 21 pages.
Final Office Action from U.S. Appl. No. 14/216,493, dated May 22, 2017, 17 pages.
Final Office Action from U.S. Appl. No. 14/216,859, dated Jun. 9, 2016, 16 pages.
Final Office Action from U.S. Appl. No. 14/360,280, dated Aug. 10, 2017, 103 pages.
Final Office Action from U.S. Appl. No. 14/360,282, dated Feb. 16, 2017, 10 pages.
Final Office Action from U.S. Appl. No. 14/360,282, dated Oct. 4, 2017, 22 pages.
Final Office Action from U.S. Appl. No. 14/360,284, dated Mar. 1, 2017, 10 pages.
Final Office Action from U.S. Appl. No. 15/219,063, dated Nov. 20, 2017, 27 pages.
Final Office Action from U.S. Appl. No. 15/354,742, dated Nov. 29, 2017, 20 pages.
Final Office Action from U.S. Appl. No. 15/354,857, dated Nov. 28, 2017, 23 pages.
First Office Action and Search report from foreign counterpart China Patent Application No. 201180076248.0, dated Mar. 17, 2016, 25 pages.
First Office Action and Search Report from foreign counterpart China Patent Application No. 201480024463.X, dated Apr. 1, 2017, 31 pages. (Translation available only for office action).
First Office Action and Search report from foreign counterpart Chinese Patent Application No. 201180076244.2, dated Mar. 22, 2016, 18 pages (Translation available only for Office Action).
First Office Action from foreign counterpart China Patent Application No. 201180076245.7, dated Mar. 21, 2016, 10 pages.
First Office Action from foreign counterpart China Patent Application No. 201280024012.7, dated May 30, 2016, 21 pages.
First Office Action from foreign counterpart China Patent Application No. CN201280034725, dated Oct. 26, 2015, 26 pages.
First Office Action from foreign counterpart China Patent Application No. CN201280034739, dated Nov. 3, 2015, 39 pages.
First Office Action from foreign counterpart China Patent Application No. CN201310589048, dated Feb. 2, 2016, 8 pages.
First Office Action from foreign counterpart Chinese Patent Application No. 201280024054.0, dated May 30, 2016, 24 pages.
First Office Action from foreign counterpart Chinese patent application No. 201280024095, dated May 26, 2016, 32 pages.
Fourth Office Action and Search report from foreign counterpart China Patent Application No. 201180076248.0, dated Nov. 9, 2017, 38 pages. (Translation available only for office action).
Franklin, et al., “The Expandable Split Window Paradigm for Exploiting Fine-Grain Parallelism,” ACM SIGARCH Computer Architecture News—Special Issue: Proceedings of the 19th annual international symposium on Computer architecture (ISCA '92), Association for Computing Machinery (ACM), New York, NY, vol. 20 (2), May 1992, pp. 58-67.
Garmany, J., “The Power of Indexing: Oracle Tips by Burleson Consulting,” Burleson Enterprises, Inc., archived on Mar. 9, 2009, retrieved Sep. 17, 2015 via Internet: web.archive.org/web/20090309201136/http://dba-oracle.com/t_indexing_power.htm, 7 pages.
Non-final Office Action from U.S. Appl. No. 15/357,943, dated Aug. 25, 2017, 111 pages.
Notice of Allowance and Search Report from foreign counterpart Taiwan Patent Application No. 103109479, dated Nov. 30, 2017, 4 pages. (Translation available only for Search report).
Notice of Allowance from foreign counterpart Chinese Patent Application No. 200780046679, dated Feb. 6, 2017, 8 pages.
Notice of Allowance from foreign counterpart Korean Patent Application No. 10-2015-7029262, dated Aug. 31, 2017, 3 pages.
Notice of Allowance from foreign counterpart Korean Patent Application No. 10-2016-7017150, dated Oct. 30, 2017, 3 pages.
Notice of Allowance from foreign counterpart Korean Patent Application No. 20137027841, dated Mar. 31, 2016, 2 pages.
Notice of Allowance from U.S. Appl. No. 12/296,919, dated Jul. 27, 2012, 6 pages.
Notice of Allowance from U.S. Appl. No. 12/514,303, dated Oct. 25, 2013, 12 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Apr. 13, 2017, 62 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Aug. 7, 2017, 42 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Aug. 10, 2016, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Dec. 29, 2016, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Mar. 4, 2016, 14 pages.
Notice of Allowance from U.S. Appl. No. 13/428,438, dated Nov. 6, 2015, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/428,440, dated Apr. 20, 2017, 46 pages.
Notice of Allowance from U.S. Appl. No. 13/428,440, dated Feb. 26, 2016, 10 pages.
Notice of Allowance from U.S. Appl. No. 13/428,440, dated Mar. 10, 2017, 52 pages.
Notice of Allowance from U.S. Appl. No. 13/428,440, dated Nov. 16, 2016, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/428,440, dated Nov. 20, 2015, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/428,452, dated Oct. 21, 2015, 9 pages.
Notice of Allowance from U.S. Appl. No. 13/475,708, dated Jun. 16, 2017, 51 pages.
Notice of Allowance from U.S. Appl. No. 13/475,708, dated Jun. 30, 2017, 53 pages.
Notice of Allowance from U.S. Appl. No. 13/475,708, dated Mar. 17, 2017, 55 pages.
Notice of Allowance from U.S. Appl. No. 13/475,708, dated Nov. 27, 2017, 24 pages.
Notice of Allowance from U.S. Appl. No. 13/475,708, dated Oct. 13, 2016, 17 pages.
Notice of Allowance from U.S. Appl. No. 13/475,739, dated Aug. 3, 2016, 11 pages.
Notice of Allowance from U.S. Appl. No. 13/475,739, dated Mar. 25, 2016, 25 pages.
Notice of Allowance from U.S. Appl. No. 13/691,609, dated Aug. 6, 2014, 11 pages.
Notice of Allowance from U.S. Appl. No. 13/691,609, dated Feb. 23, 2015, 16 pages.
Notice of Allowance from U.S. Appl. No. 14/194,589, dated Jul. 27, 2016, 7 pages.
Notice of Allowance from U.S. Appl. No. 14/213,115, dated Jun. 27, 2016, 9 pages.
Notice of Allowance from U.S. Appl. No. 14/213,115, dated Oct. 3, 2016, 20 pages.
Notice of Allowance from U.S. Appl. No. 14/213,135, dated Aug. 3, 2017, 103 pages.
Notice of Allowance from U.S. Appl. No. 14/213,135, dated Oct. 17, 2016, 17 pages.
Notice of Allowance from U.S. Appl. No. 14/213,218, dated Jun. 16, 2017, 89 pages.
Notice of Allowance from U.S. Appl. No. 14/213,692, dated Dec. 23, 2016, 19 pages.
Notice of Allowance from U.S. Appl. No. 14/213,692, dated Sep. 28, 2017, 112 pages.
Notice of Allowance from U.S. Appl. No. 14/213,730, dated Aug. 31, 2017, 96 pages.
Notice of Allowance from U.S. Appl. No. 14/213,730, dated Oct. 27, 2016, 16 pages.
Notice of Allowance from U.S. Appl. No. 14/213,854, dated Oct. 7, 2016, 19 pages.
Notice of Allowance from U.S. Appl. No. 14/214,045, dated Apr. 18, 2017, 88 pages.
Notice of Allowance from U.S. Appl. No. 14/214,045, dated Oct. 6, 2017, 137 pages.
Notice of Allowance from U.S. Appl. No. 14/214,176, dated May 10, 2017, 88 pages.
Notice of Allowance from U.S. Appl. No. 14/214,176, dated Oct. 19, 2017, 25 pages.
Notice of Allowance from U.S. Appl. No. 14/214,280, dated Jun. 29, 2017, 86 pages.
Notice of Allowance from U.S. Appl. No. 14/215,633, dated Jun. 30, 2017, 83 pages.
Notice of Allowance from U.S. Appl. No. 14/215,633, dated Mar. 23, 2017, 17 pages.
Notice of Allowance from U.S. Appl. No. 14/215,633, dated May 23, 2016, 9 pages.
Notice of Allowance from U.S. Appl. No. 14/215,633, dated Oct. 4, 2017, 15 pages.
Notice of Allowance from U.S. Appl. No. 14/215,633, dated Sep. 29, 2016, 13 pages.
Abandonment from U.S. Appl. No. 14/212,203, dated Jul. 26, 2018, 2 pages.
Abandonment from U.S. Appl. No. 14/212,533, dated Jun. 19, 2018, 3 pages.
Abandonment from U.S. Appl. No. 14/360,282, dated May 25, 2018, 2 pages.
Abandonment from U.S. Appl. No. 15/354,857, dated Jul. 30, 2018, 2 pages.
Corrected Notice of Allowance from U.S. Appl. No. 15/219,063, dated Jun. 28, 2018, 8 pages.
Final Office Action from U.S. Appl. No. 14/360,280, dated Jul. 24, 2018, 24 pages.
Non-Final Office Action from U.S. Appl. No. 15/712,017, dated May 7, 2018, 127 pages.
Notice of Allowance from U.S. Appl. No. 13/824,013, dated Jul. 23, 2018, 15 pages.
Notice of Allowance from U.S. Appl. No. 14/216,493, dated Aug. 1, 2018, 14 pages.
Notice of Allowance from U.S. Appl. No. 15/408,255, dated Jul. 25, 2018, 136 pages.
Notice of Preliminary Rejection from foreign counterpart Korean Patent Application No. 10-2018-7003058, dated Jun. 4, 2018, 10 pages.
First Examination Report from foreign counterpart Indian Patent Application No. 51/KOLNP/2012, dated Jul. 30, 2018, 7 pages.
Non-Final Office Action from U.S. Appl. No. 15/408,323, dated Oct. 9, 2018, 144 pages.
Non-Final Office Action from U.S. Appl. No. 15/866,323, dated Oct. 1, 2018, 121 pages.
Notice of Allowance from U.S. Appl. No. 15/862,496, dated Nov. 2, 2018, 23 pages.
Notice of Allowance from U.S. Appl. No. 14/213,135, dated Oct. 3, 2018, 34 pages.
Notice of Allowance from U.S. Appl. No. 14/360,284, dated Oct. 12, 2018, 45 pages.
Notice of Allowance from U.S. Appl. No. 15/408,311, dated Aug. 28, 2018, 138 pages.
Notice of Allowance from U.S. Appl. No. 15/712,017, dated Oct. 3, 2018, 16 pages.
Notice of Allowance from U.S. Appl. No. 15/408,269, dated Sep. 24, 2018, 137 pages.
Second Office Action from foreign counterpart Chinese Patent Application No. 201480024528.0, dated Oct. 8, 2018, 7 pages.
Communication pursuant to Article 94(3) EPC for Application No. 14769411.1, dated Dec. 7, 2018, 7 pages.
Communication pursuant to Article 94(3) EPC for Application No. 11876314.3, dated Oct. 19, 2018, 5 pages.
Communication pursuant to Artide 94(3) EPC for Application No. 11876314.3, dated Sep. 24, 2018, 6 pages.
Non-Final Office Action from U.S. Appl. No. 15/354,742, dated Dec. 4, 2018, 54 pages.
Non-Final Office Action from U.S. Appl. No. 15/283,836, dated Dec. 27, 2018, 150 pages.
Notice of Allowance from U.S. Appl. No. 13/824,013, dated Nov. 13, 2018, 12 pages.
Notice of Allowance from U.S. Appl. No. 15/706,056, dated Dec. 28, 2018, 138 pages.
Office Action and Search Report from foreign counterpart Taiwan Patent Application No. 106127331, dated Nov. 23, 2018, 13 pages.
Related Publications (1)
Number Date Country
20180137081 A1 May 2018 US
Provisional Applications (3)
Number Date Country
60792219 Apr 2006 US
60791782 Apr 2006 US
60791649 Apr 2006 US
Continuations (3)
Number Date Country
Parent 14733827 Jun 2015 US
Child 15853323 US
Parent 13691609 Nov 2012 US
Child 14733827 US
Parent 12296919 US
Child 13691609 US