• Title/Summary/Keyword: Nonlinear Actuator

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Servo control of an under actuated system using antagonistic shape memory alloy

  • Sunjai Nakshatharan, S.;Dhanalakshmi, K.;Josephine Selvarani Ruth, D.
    • Smart Structures and Systems
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    • v.14 no.4
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    • pp.643-658
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    • 2014
  • This paper presents the design, modelling and, simulation and experimental results of a shape memory alloy (SMA) actuator based critical motion control application. Dynamic performance of SMA and its ability in replacing servo motor is studied for which the famous open loop unstable balancing ball and beam system direct driven by antagonistic SMA is designed and developed. Simulation uses the mathematical model of ball and beam structure derived from the first principles and model estimated for the SMA actuator by system identification. A PID based cascade control system consisting of two loops is designed and control of ball trajectory for various target positions with settling time as control parameter is verified experimentally. The results demonstrate the performance of SMA for a complicated i.e., under actuated, highly nonlinear unstable system, and thereby it's dynamic behaviour. Control strategies bring out the effectiveness of the actuator and its possible application to much more complex applications such as in aerospace control and robotics.

Constrained Adaptive Backstepping Controller Design for Aircraft Landing in Wind Disturbance and Actuator Stuck

  • Yoon, Seung-Ho;Kim, You-Dan;Park, Sang-Hyuk
    • International Journal of Aeronautical and Space Sciences
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    • v.13 no.1
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    • pp.74-89
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    • 2012
  • An adaptive backstepping controller is designed for the automatic landing of a fixed-wing aircraft. The backstepping control scheme is adopted by using the nonlinear six degree-of-freedom dynamics of the aircraft during the landing phase. The adaptive law is integrated along with the backstepping controller in order to estimate the aircraft modeling errors as well as the external disturbance. The dynamic constraints of the states and the actuator inputs are taken into account in the parameter adaptation. This is done to prevent an aggressive adaptation and to provide reliable control commands. Numerical simulations were performed to verify the performance of the proposed control law for the landing of the aircraft with the presence of gust and actuator stuck.

Iterative Learning Control of Trajectory Generation for the Soft Actuator (궤적 생성 반복 학습을 통한 소프트 액추에이터 제어 연구)

  • Song, Eunjeong;Koo, Jachoon
    • The Journal of Korea Robotics Society
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    • v.16 no.1
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    • pp.35-40
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    • 2021
  • As the robot industry develops, industrial automation uses industrial robots in many parts of the manufacturing industry. However, rigidity-based conventional robots have a disadvantage in that they are challenging to use in environments where they grab fragile objects or interact with people because of their high rigidity. Therefore, researches on soft robot have been actively conducted. The soft robot can hold or manipulate fragile objects by using its compliance and has high safety even in an atypical environment with human interaction. However, these advantages are difficult to use in dynamic situations and control by the material's nonlinear behavior. However, for the soft robot to be used in the industry, control is essential. Therefore, in this paper, real-time PD control is applied, and the behavior of the soft actuator is analyzed by providing various waveforms as inputs. Also, Iterative learning control (ILC) is applied to reduce errors and select an ILC type suitable for soft actuators.

Analytical Approach to Deformation of a Soft Rotary Actuator with Double Curvature Shell Shape (이중 곡률 쉘 모양의 소프트 회전 액추에이터 변형에 대한 수식적 접근)

  • Lee, Young min;Choi, Hyouk ryeol;Koo, Ja choon
    • The Journal of Korea Robotics Society
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    • v.17 no.1
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    • pp.68-75
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    • 2022
  • In this paper, we considered the deformation shape of the soft rotation actuator as a double curvature shell and proceeded with the analytical development. Since the response of the hyperelastic material has a large nonlinear deformation, the analytical approach is very complicated and the solution cannot be easily obtained. it is assumed that the behavior of the flexible body, which is a superelastic material, takes the form of a double curvature shell, and the formulas for calculating the deformation are simplified. In this process, equilibrium equations in the related coordinate system representing a double curvature shell were derived. In addition, assuming a thin shell, the stress component in the thickness direction was ignored, and the equation was developed by adding the assumption of free rotation without load. In order to verify the analytically calculated value in this way, an experiment was conducted and the results were compared.

Adaptive Control for Trajectory Tracking of a Manipulator with Pneumatic Artificial Muscle Actuators (공압인공근육로봇의 궤적추종의 적응제어)

  • Park, H.W.;Park, N.C.;Yang, H.S.;Park, Y.P.
    • Journal of the Korean Society for Precision Engineering
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    • v.14 no.5
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    • pp.100-107
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    • 1997
  • A pneumatic artificial muscle type of actuator, which acts similar to human muscle, is developed recently. In this paper, an adaptive controller is presented for the trajectory tracking problem of a two-degree- of-freedom manipulator using two pairs of pneumatic artificial muscle actuators. Due to the nonlinearity and the uncertainty on the dynamics of the actuator, it is difficult to make the effective control schemes of this system. By the adaptive control law which inclueds a nonlinear "feedforward" term compensating paramet- ric uncertainties in addition to P.I.D. scheme, both golbal stability of the system and convergence of the tracking error are guaranted. The effectiveness of the proposed control method for the manipulator using this actuator is illustrated through experiments.periments.

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Design of $H_{\infty}$ Controller for Underwater Vehicle and Nonlinear Simulation (수중운동체에 대한 $H_{\infty}$ 제어기 설계와 비선형 시뮬레이션)

  • 전찬식;김종해박홍배
    • Proceedings of the IEEK Conference
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    • 1998.06a
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    • pp.215-218
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    • 1998
  • In this paper, we design the $H_{\infty}$ controllers satisfying robust stability and performance for underwater vehicle. The underwater vehicle has computations delay time and input delay. In addition, there exist parameter uncertainties by the roll motion coefficient error, buoyance error, and gravity error. We design the $H_{\infty}$ controllers using model-matching method and check the performance of the proposed controller by nonlinear simulation which includes time delay model, sensor error model, and actuator model.

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Mechanically Modulated Actuators and Branched Finger Detectors for Nano-Precision MEMS Applications

  • Cho, Young-Ho;Lee, Won-Chul;Han, Ki-Ho
    • 제어로봇시스템학회:학술대회논문집
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    • 2002.10a
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    • pp.39.1-39
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    • 2002
  • We present nanoactuators and nanodetectors for high-precision Micro Electro Mechanical System (MEMS) applications. Major technical difficulties in the high-precision MEMS are arising from the fabrication uncertainty and electrical noise problems. In this paper, we present high-precision actuators and detectors, overcoming the technical limitations placed by the conventional MEMS technology. For the nano-precision actuation, we present a nonlinearly modulated digital actuator (NMDA). NMDA composed of a digital microactuator and a nonlinear micromechanical modulator. The nonlinear micromechanical modulator is intended to purify the actuation errors in the stroke of the digital a...

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Jump resonance in anti-windup compensator for systems with saturating actuators (Anti-windup 보상기의 점프공진에 관한 연구)

  • 박영진;장원욱
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10a
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    • pp.1060-1066
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    • 1992
  • One of the undesirable nonlinear phenomenon called 'wind up' occours when the integrator in the controller and the saturated actuator interact. Large overshoot, slow response, instability, limit cycle and jump resonance are the characteristics of wind up phenomenon. Several 'anti-windup' compensators have been developed to prevent some of the aforementioned nonlinear characteristics such as instabilituy and limit cycle, but none has studied the effect of antiwindup compensator on the jump resonance. In this paper, we developed an analyitcal method to design the compensator to prevent not only limit cycle but also jump resonance. An illustrative example is included to show the compensator eliminates jump resonance of effectively.

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Fuzzy proportional -derivative controller with adaptive control resolution

  • Oh, Seok-Yong;Park, Dong-Jo
    • 제어로봇시스템학회:학술대회논문집
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    • 1995.10a
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    • pp.135-137
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    • 1995
  • A new design method is proposed for a fuzzy PD controller. By analyzing phase plane characteristics we can build and optimize the rule base of fuzzy logic controller. Also, a new gain tuning method is used to improve performance in the transient and steady state. The improved performance of the new methodology is shown by an application to the design of control system with a highly nonlinear actuator.

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A Position Control of Nonlinear Hydraulic System using Variable Design-Parameter Fuzzy PID Controller (가변 설계 파라미터 퍼지 PID 제어기를 이용한 비선형 유압시스템의 위치 제어)

  • 김인환;김종화;김진규
    • Journal of Advanced Marine Engineering and Technology
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    • v.28 no.1
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    • pp.136-144
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    • 2004
  • In general a hydraulic system which uses a single rod hydraulic as an actuator is modeled as a nonlinear system and reveals uncertain Parameter characteristics such as the density variation of hydraulic oil and is subject to load variations and severe disturbances during operation. A variable design-parameter fuzzy PID controller is adopted to solve these undesirable internal and external problems and its effectiveness is verified through computer simulations for control performance and real time control possibility.