• Title/Summary/Keyword: logic simulation

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Study on Chip Design & Implementation of 32 Bit Floating Point Compatible DSP (32비트 부동소수점 호환 DSP의 설계 및 칩 구현에 관한 연구)

  • Woo, Jong-Sik;Seo, Jin-Keun;Lim, Jae-Young;Park, Ju-Sung
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.37 no.11
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    • pp.74-84
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    • 2000
  • This paper deals with procedures for design and implementation of a DSP, which is compatible with TMS320C30 DSP. CBS(Cycle Based Simulator) is developed to study the architecture of the target DSP. The simulator gives us detailed information such as function block operation, control signal values, register condition, bus and memory values when a instruction is being carried out. RTL design is carried out by VHDL. Logic simulation and hardware emulation are employed to verify proper operation of the design. The DSP is fabricated with 0.6${\mu}m$ CMOS technology. The Chip has 450,000 gates complexity, $9{\times}9mm^2$ area, 20 MIPS operation speed. It is confirmed by running 109 instructions out of 114 instructions and 13 kinds of algorithm that the developed DSP has compatibility with TMS320C30.

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A Study on the Improvement of Pitch Autopilot Flight Control Law (세로축 자동조종 비행제어법칙 개선에 관한 연구)

  • Kim, Chong-Sup;Hwang, Byung-Moon;Lee, Chul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.11
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    • pp.1104-1111
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    • 2008
  • The supersonic advanced trainer based on digital flight-by-wire flight control system uses aircraft flight information such as altitude, calibrated airspeed and angle of attack to calculate flight control law, and this information is measured by IMFP(Integrated Multi-Function Probe) equipment. The information has triplex structure using three IMFP sensors. Final value of informations is selected by mid-value selection logic to have more flight data reliability. As the result of supersonic flight test, pitch oscillation is occurred due to IMFP noise when altitude hold autopilot mode is engaged. This tendency may affect stability and handling quality of an aircraft during autopilot mode. This paper addresses autopilot control law design to remove pitch oscillation and these control laws are verified by non-real time simulation and flight test. Also, pitch response characteristics of pitch attitude hold autopilot mode is improved by upgrading the control law structure and feedback gain tuning during bank turn.

Application of Soft Computing Based Response Surface Techniques in Sizing of A-Pillar Trim with Rib Structures (승용차 A-Pillar Trim의 치수설계를 위한 소프트컴퓨팅기반 반응표면기법의 응용)

  • Kim, Seung-Jin;Kim, Hyeong-Gon;Lee, Jong-Su;Gang, Sin-Il
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.25 no.3
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    • pp.537-547
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    • 2001
  • The paper proposes the fuzzy logic global approximate optimization strategies in optimal sizing of automotive A-pillar trim with rib structures for occupant head protection. Two different strategies referred to as evolutionary fuzzy modeling (EFM) and neuro-fuzzy modeling (NFM) are implemented in the context of global approximate optimization. EFM and NFM are based on soft computing paradigms utilizing fuzzy systems, neural networks and evolutionary computing techniques. Such approximation methods may have their promising characteristics in a case where the inherent nonlinearity in analysis model should be accommodated over the entire design space and the training data is not sufficiently provided. The objective of structural design is to determine the dimensions of rib in A-pillar, minimizing the equivalent head injury criterion HIC(d). The paper describes the head-form modeling and head impact simulation using LS-DYNA3D, and the approximation procedures including fuzzy rule generation, membership function selection and inference process for EFM and NFM, and subsequently presents their generalization capabilities in terms of number of fuzzy rules and training data.

Experiment of an ABS-type control strategy for semi-active friction isolation systems

  • Lu, Lyan-Ywan;Lin, Ging-Long;Lin, Chen-Yu
    • Smart Structures and Systems
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    • v.8 no.5
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    • pp.501-524
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    • 2011
  • Recent studies have discovered that a conventional passive isolation system may suffer from an excessive isolator displacement when subjected to a near-fault earthquake that usually has a long-period velocity pulse waveform. Semi-active isolation using variable friction dampers (VFD), which requires a suitable control law, may provide a solution to this problem. To control the VFD in a semi-active isolation system more efficiently, this paper investigates experimentally the possible use of a control law whose control logic is similar to that of the anti-lock braking systems (ABS) widely used in the automobile industry. This ABS-type controller has the advantages of being simple and easily implemented, because it only requires the measurement of the isolation-layer velocity and does not require system modeling for gain design. Most importantly, it does not interfere with the isolation period, which usually decides the isolation efficiency. In order to verify its feasibility and effectiveness, the ABS-type controller was implemented on a variable-friction isolation system whose slip force is regulated by an embedded piezoelectric actuator, and a seismic simulation test was conducted for this isolation system. The experimental results demonstrate that, as compared to a passive isolation system with various levels of added damping, the semi-active isolation system using the ABS-type controller has the better overall performance when both the far-field and the near-fault earthquakes with different PGA levels are considered.

Design of a Fast Adder Using Robust QCA Design Guide (강건 QCA 설계 지침을 이용한 고속 가산기 설계)

  • Lee Eun-Choul;Kim Kyo-Sun
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.43 no.4 s.346
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    • pp.56-65
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    • 2006
  • The Quantum-dot Cellular Automata (QCA) can be considered as a candidate for the next generation digital logic implementation technology due to their small feature sizes and ultra low power consumption. Up to now, several designs using Uh technology have been proposed. However, we found not all of the designs function properly. Furthermore, no general design guidelines have been proposed so far. A straightforward extension of a simple functional design pattern may fail. This makes designing a large scale circuits using QCA technology an extremely time-consuming process. In this paper, we show several critical vulnerabilities related to unbalanced input paths to QCA gates and sneak noise paths in QCA interconnect structures. In order to make up the vulnerabilities, a disciplinary guideline will be proposed. Also, we present a fast adder which has been designed by the discipline, and verified to be functional by the simulation.

Proposal of a Novel Flying Master Bus Architecture For System On a Chip and Its Evaluation (SoC를 위한 새로운 플라잉 마스터 버스 아키텍쳐 구조의 제안과 검증)

  • Lee, Kook-Pyo;Kang, Seong-Jun;Yoon, Yung-Sup
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.47 no.1
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    • pp.69-78
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    • 2010
  • To implement the high performance SoC, we propose the flying master bus architecture that a specially defined master named as the flying master directly accesses the selected slaves with no regard to the bus protocol. The proposed bus architecture was implemented through Verilog and mapped the design into Hynix 0.18um technology. As master and slave wrappers have around 150 logic gate counts, the area overhead is still small considering the typical area of modules in SoC designs. In TLM performance simulation about proposed architecture, 25~40% of transaction cycle and 43~60% of bus efficiency are increased and 43~77% of request cycle is decreased, compared with conventional bus architecture. Conclusively, we assume that the proposed flying master bus architecture is promising as the leading candidate of the bus architecture in the aspect of performance and efficiency.

Optimum design and vibration control of a space structure with the hybrid semi-active control devices

  • Zhan, Meng;Wang, Sheliang;Yang, Tao;Liu, Yang;Yu, Binshan
    • Smart Structures and Systems
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    • v.19 no.4
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    • pp.341-350
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    • 2017
  • Based on the super elastic properties of the shape memory alloy (SMA) and the inverse piezoelectric effect of piezoelectric (PZT) ceramics, a kind of hybrid semi-active control device was designed and made, its mechanical properties test was done under different frequency and different voltage. The local search ability of genetic algorithm is poor, which would fall into the defect of prematurity easily. A kind of adaptive immune memory cloning algorithm(AIMCA) was proposed based on the simulation of clone selection and immune memory process. It can adjust the mutation probability and clone scale adaptively through the way of introducing memory cell and antibody incentive degrees. And performance indicator based on the modal controllable degree was taken as antigen-antibody affinity function, the optimization analysis of damper layout in a space truss structure was done. The structural seismic response was analyzed by applying the neural network prediction model and T-S fuzzy logic. Results show that SMA and PZT friction composite damper has a good energy dissipation capacity and stable performance, the bigger voltage, the better energy dissipation ability. Compared with genetic algorithm, the adaptive immune memory clone algorithm overcomes the problem of prematurity effectively. Besides, it has stronger global searching ability, better population diversity and faster convergence speed, makes the damper has a better arrangement position in structural dampers optimization leading to the better damping effect.

Control Performance Evaluation of Smart Mid-story Isolation System with RNN Model (RNN 모델을 이용한 스마트 중간층 면진시스템의 제어성능 평가)

  • Kim, Hyun-Su
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.1
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    • pp.774-779
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    • 2020
  • The seismic response reduction capacity of a smart mid-story isolation system was investigated using the RNN model in this study. For this purpose, an RNN model was developed to make a dynamic response prediction of building structures subjected to seismic loads. An existing tall building with a mid-story isolation system was selected as an example structure for realistic research. A smart mid-story isolation system was comprised of an MR damper instead of existing lead dampers. The RNN model predicted the seismic responses accurately compared to those of the FEM model. The simulation time of the RNN model can be reduced significantly compared to the FEM model. After the numerical simulations, the smart mid-story isolation system could effectively reduce the seismic responses of the existing building compared to the conventional mid-story isolation system.

Robust Speed Control of a Permanent Magnet Synchronous Motor using a Fuzzy Logic Controller (퍼지제어기를 이용한 영구자석 동기전동기의 강인한 속도제어)

  • Choi, Young-Sik;Yu, Dong-Young;Jung, Jin-Woo
    • The Transactions of the Korean Institute of Power Electronics
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    • v.15 no.5
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    • pp.343-351
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    • 2010
  • This paper proposes a new fuzzy speed controller based on the Takagi-Sugeno fuzzy method to achieve a robust speed control of a permanent magnet synchronous motor (PMSM). The proposed controller requires the information of the load torque, so the second-order load torque observer is used to estimate it. The LMI condition is derived for the existence of the proposed fuzzy speed controller, and the gains of the controller are provided. It is proven that the augmented control system including the fuzzy speed controller and the load torque observer is exponentially stable. To evaluate the performance of the proposed fuzzy speed controller, the simulation and experimental results are presented under motor parameter variations. Finally, it is clearly verified that the proposed control method can accurately control the speed of a permanent magnet synchronous motor.

Adaptive Fuzzy Sliding Mode Control for Nonlinear Systems without Parameter Projection Method (파라미터 투영 기법이 필요 없는 비선형 시스템의 적응 퍼지 슬라이딩 모드 제어)

  • Seo, Sam-Jun
    • Journal of the Korean Institute of Intelligent Systems
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    • v.21 no.4
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    • pp.499-505
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    • 2011
  • In this paper, we proposed an adaptive fuzzy sliding mode control for nonlinear systems without parameter projection method. By modifying the controller structure, the parameters of the estimated input gain function are guaranteed not being identically zero and it is shown that the control scheme will not cause any implementation problem even if the estimated value of input gain function is zero at any moment during on-line operations. Except for the input gain function which an approximate estimate for its lower bound is needed, the proposed control scheme does not assume a priori the exact values of the bounding parameters. Based on Lyapunov synthesis methods, the overall control system guarantees that the tracking error asymptotically converges to zero and that all signals involved in controller are uniformly bounded. This can be illustrated by the simulation results for an inverted pendulum system.