• Title/Summary/Keyword: Thrust Modeling

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Fuzzy Logic Modeling and Control for Drilling of Composite Laminates ; Simulation

  • Chung, Byeong-Mook;Ye Sheng;Masayoshi Tomizuka
    • International Journal of Precision Engineering and Manufacturing
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    • v.2 no.1
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    • pp.11-17
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    • 2001
  • In drilling of composite laminates, it is important to minimize of reduce occurrences of delaminations. In particular, a peel -up delamination at entrance and push-up delamination at exit are common. Deleaminations may by avoided by regulating the drill thrust force can be controlled by adjusting the feedrate of the drill. Dynamics involved in drilling of composite laminates is time varying and nonlinear. In this paper, a fuzzy logic model and control strategy are proposed. Simulation results show that the fuzzy model can describe the nonlinear time-varying process well. The fuzzy controller realizes a fast rise time and a little overshoot of drilling force.

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Theoretical Modeling of Pulsed Plasma Thruster Performance with Teflon Ablation

  • Cho, Mingyoung;Sung, Hong-Gye
    • International Journal of Aeronautical and Space Sciences
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    • v.18 no.1
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    • pp.138-143
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    • 2017
  • A performance analysis for a pulsed plasma thruster(PPT) has been conducted to predict the thrust and current change. Two models were implemented - a one-dimensional lumped circuit analysis model and the Teflon ablation model provided by Michael Keidar. The circuit model incorporating resistance and inductance models was adapted to predict the magnitude of the discharge current. Numerical simulations like current discharge rates with different voltages were reasonably well compared with experimental data. The effects of Teflon ablation on thruster characteristics were investigated.

The effect of vehicle velocity and drift angle on through-body AUV tunnel thruster performance

  • Saunders, Aaron;Nahon, Meyer
    • Ocean Systems Engineering
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    • v.1 no.4
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    • pp.297-315
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    • 2011
  • New applications of streamlined Autonomous Underwater Vehicles require an AUV capable of completing missions with both high-speed straight-line runs and slow maneuvers or station keeping tasks. At low, or zero, forward speeds, the AUV's control surfaces become ineffective. To improve an AUV's low speed maneuverability, while maintaining a low drag profile, through-body tunnel thrusters have become a popular addition to modern AUV systems. The effect of forward vehicle motion and sideslip on these types of thrusters is not well understood. In order to characterize these effects and to adapt existing tunnel thruster models to include them, an experimental system was constructed. This system includes a transverse tunnel thruster mounted in a streamlined AUV. A 6-axis load cell mounted internally was used to measure the thrust directly. The AUV was mounted in Memorial University of Newfoundland's tow tank, and several tests were run to characterize the effect of vehicle motion on the transient and steady state thruster performance. Finally, a thruster model was modified to include these effects.

A study on the speed characteristic of linear induction motor (유도형 리니어 모터의 속도특성에 관한 연구)

  • CHUNG B. H.;CHOI M. H.;CHO G. B.;BAEK H. L.;SEO J. Y.;KIM D. G.
    • Proceedings of the KIPE Conference
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    • 2004.07a
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    • pp.151-154
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    • 2004
  • To use the SLIM for servo system, the exact account of thrust about the initial speed is needed, but analyzing by equivalent circuit analyzing methode such as rotary induction motor, the error occurs because of the end effect. So, we applied the equivalent circuit considering the end effect of SLIM in this paper. The current control system is advanced the space vector pulse width modulation by using high arithmetic performance microprocessor such as DSP. In this paper, we use the dynamic characteristic analyzing methode that can calculate efficiently the end effect by using equivalent circuit methode in the operating SLIM system modeling and examine the output characteristics of SVPWM with PI controller.

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Preliminary Design Program for a High Thrust Liquid Rocket-Engine : Dynamic Characteristic Prediction Program Overview and Technical Achievements (대추력 액체로켓엔진 예비설계 프로그램 : 비정상작동.동특성 예측 기술 개요 및 현황)

  • Ko, Tae-Ho;Kim, Sang-Min;Kim, Hyung-Min;Yoon, Woong-Sup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.417-418
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    • 2009
  • Aiming at time-dependent performance prediction of Liquid Rocket Engine(LRE) system, Program for Dynamic Characteristic Prediction of LRE is overviewed, and a modeling and dynamic analysis of rocket engine system with reference to developed transient simulator for LRE is outlined.

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Performance Analysis of EEGR Valve (EEGR 밸브의 성능해석)

  • 김호상;김덕진;최진경;윤대호;박상권
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.389-392
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    • 2000
  • This paper presents a performance Analysis of electrically exhaust gas recirculation valve using commercial electromagnetic simulation software, Flux2D. Under the assumption of 2D axi-symmetric magnetic field, the characteristics of EEGR valve by revising the design parameter, has ken investigated by estimating the variation of thrust force with respect to the pintle position. The mode shapes and the frequency response functions were computed by using three dimensional finite element modeling of the whole EEGR valve and their accuracies were verified with experimental FFT analysis technique.

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Analysis of High Speed Linear Motor Feed System Characteristics (리니어모터 응용 고속 이송시스템 특성분석에 관한 연구)

  • 유송민
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.993-996
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    • 2000
  • A brushless linear motor is suitable for a high-accuracy servo mechanism. It is also suitable for operation with higher speed and precision. Since it does not involve some sort of mechanical coupling, linear driving force can be applied directly. Basic models including magetomotive force and electromotive forces are introduced and simplified. Both conventional PID and fuzzy controllers are implemented and performance results using those controllers are compared. Along with better simulated performance observed using fuzzy controller, further fabrication is to be included with various empirical results. Several system operational characteristics have been observed. Typical nonlinearities as friction, cogging and torque or thrust ripple that might deteriorate system performance would be tackled using presumably effective method such as neural network based learning controller.

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Development of High Speed Feed System using Linear Motor (리니어모터 응용 고속이송계 제어기술 개발)

  • 유송민
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.05a
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    • pp.973-976
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    • 2000
  • A brushless linear motor is suitalbe fur a high-accuracy servo mechanism. It is also suitable for operation with higher speed and precision. Since it does not involve some sort of mechanical coupling, linear driving force can be applied directly. Basic models including magetomotive farce and electromotive forces are introduced and simplified. Both conventional PID and fuzzy controllers are implemented and performance results using those controllers are compared. Along with better simulated performance observed using fuzzy controller, further fabrication is to be included with various empirical results. Typical nonlinearities as friction, cogging and torque or thrust ripple that might deteriorate system performance would be tackled using presumably effective method such as neural network based learning controller.

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Analysis of Combustor and Nozzle for Monopropellant Satellite Thruster (단일추진제 위성추력기 내 연소기 및 노즐 유동 해석)

  • Lee, Sung-Nam;Baek, Seung-Wook;Kim, Su-Kyum;Yu, Myoung-Jong
    • Journal of the Korean Society of Combustion
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    • v.15 no.2
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    • pp.12-18
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    • 2010
  • A numerical analysis was performed to predict the thermo-fluid dynamic characteristics of hydrazine monopropellant reaction in the thruster combustor and nozzle. A 1-D porous model was introduced to simulate catalytic reaction by iridium in the combustor while 2-D axisymmetric analysis was applied to predict the nozzle flow. The chemical species and temperature variations were predicted by changing the injection pressure and mass flow rate and their results were validated by comparison with limited experimental data. The thrust variation with injection pressure could be estimated using the current 1-D combustor modeling.

Characterization of Linear Motor Feed System with AE and Acceleration Signal (AE 및 가속도 신호를 이용한 리니어 모터 이송시스템의 특성분석)

  • 유송민
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2000.10a
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    • pp.299-303
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    • 2000
  • A brushless linear motor is suitable for operation with higher speed and precision. Since it does not involve mechanical coupling, linear driving force can be applied directly. Conventional PID and fuzzy controllers are implemented and performance results using those controllers are compared. Along with better simulated performance observed using fuzzy controller, further fabrication is to be included with various empirical results. Several system operational characteristics have been observed. Typical nonlinearities as friction, cogging and torque or thrust ripple that might deteriorate system performance would be tackled using presumably effective method such as neural network based learning controller.

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