• Journal of Aerospace System Engineering
• /
• v.11 no.1
• /
• pp.14-21
• /
• 2017

A Linear parameterized Sigma-Pi neural network (SPNN) is applied to a tilt-duct unmanned aerial vehicle (UAV) which has a very large longitudinal stability ($C_{L{\alpha}}$). It is uncontrollable by a proportional, integral, derivative (PID) controller due to heavy stability. It is shown that the combined inner loop and outer loop of SPNN controllers could overcome the sluggish longitudinal dynamics using a method of dynamic inversion and pseudo-control to compensate for reference model error. The simulation results of the way point guidance are presented to evaluate the performance of SPNN in comparison to a PID controller.

• Journal of the Institute of Electronics Engineers of Korea SC
• /
• v.44 no.1
• /
• pp.25-32
• /
• 2007

In this paper, a new method for first order plus dead time(FOPDT) model identification is proposed, which can identity multiple points on a process step response in terms of classification of time response. The process input and output to the test are decomposed into the transient part and the steady-state part. The steady-state part express one FOPDT model and the transient part express variously FOPDT model using least square estimation method. The optimum parameter tuning algorithm for PID controller of the Smith Predictor is proposed through ITAE as performance index. The Simulation results show the validity and improvement of performance for various processes.

• Proceedings of the KIEE Conference
• /
• 2002.06a
• /
• pp.34-37
• /
• 2002

본 연구에서는 표시형 디지털 정속주행 자동용접캐리지를 개발하고자 한다. 먼저, 용접조건을 결정하는 전류와 전압값의 입력과 출력을 디지털 입력스위치와 D/A 컨버터 출력회로를 구성하여 디지털 제어를 구성한다. 또한 디스플레이제어기의 구성은 정확한 용접조건에 의해서 용접할 수 있는 환경을 설정하여 용접의 효율성을 높이고자 한다. 시스템 제어기는 저가격과 출력전류의 특성이 개선된 RISK-Like 방식의 PIC16C74A를 이용하여 가격과 부피 및 노이즈에 강한 제어기를 구성하였다. 위빙 및 주행모터의 효율성과 응답특성을 개선하기 위해서 디지털 제어기(Digital PID Controller)를 설계하고. 이 제어기법을 이용하여 PWM인버터를 설계 및 제어 사용하여 용접 조건과 효율을 개선하였다.

• The Transactions of the Korean Institute of Power Electronics
• /
• v.14 no.4
• /
• pp.278-284
• /
• 2009

This paper presents a firing angle controller of a thyristor converter for DC power supply using PID controller with parallel data loop to improve the dynamic response. The proposed parallel data loop for firing angle controller of 3-phase semi-converter, generates pre-measured firing angle according to reference voltage and load current. With the approximated firing angle according to operating conditions, the output voltage can fast keep the reference value with small voltage error. And the PID controller compensates the output voltage error from the firing angle of parallel data loop. In order to reduce the sudden changing of the data from current ripple, a simple digital low pass filter is used to determine the output data. The proposed control scheme is verified by the experimental test of a practical 50[A] grade thyristor converter system.

• Proceedings of the KIEE Conference
• /
• 2003.07d
• /
• pp.2218-2220
• /
• 2003

현대 산업현장에서 80%이상 사용되는 PID(proportional integral derivative) 제어기는 제어성, 적응성, 제어이득 조정 등의 특정이 있어나 제어 대상에 대한 PID 제어 계수를 경험적 방법인 수동으로 동조해야하는 문제점이 있다. 이를 개선하기 위해 본 논문에서 PID제어기의 최적 자동동조를 위한 릴레이 동조 방법을 제안한다. 기존의 한계감도법과 과도응답 법으로 초기계수를 결정하는 방법보다 유연성과 적용성이 높고, 이를 마이크로프로세서(DSP : TMS-320C32)에 적용하여 소프트웨어적으로 릴레이의 기능이 이루어지도록 설계했다. 이는 Ziegler-Nichols 계수조정법이 갖는 적용대상의 제약성을 극복한 방법이며, 릴레이에 의해 출력을 강제 진동시키고 출력의 진폭과 주기를 이용하여 PID 계수를 조정하고, 또 상대안정성의 척도인 위상여유를 고려하므로 시스템의 상대안정성과 견실성을 향상시킬 수 있음을 확인하였다.

• Journal of the Korea Institute of Information and Communication Engineering
• /
• v.20 no.11
• /
• pp.2107-2112
• /
• 2016

This paper is designed to develop a Gimbal control stabilizer for drones Gimbal system control for drone for 3D image to make sure clean image in the shaking and wavering environments of drone system. The stabilizer is made of tools which support camera modules and IMU(Inertial Measurement Unit) sensor modules follow exact angles, which can brock vibrations outside of the camera modules. It is difficult for the camera modules to get clean image, because of irregular movements and various vibrations produced by flying drones. Moreover, a general PID controller used for the movements of rolling, pitching and yawing in order to control the various vibrations of various frequencies needs often to readjust PID control parameters. Therefore, this paper aims to conduct the Intelligent-PID controller as well as design the Gimbal control stabilizer to get clean images and to improve irregular movements and various vibrations problems referenced above.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.33 no.3
• /
• pp.47-56
• /
• 2005

This paper presents a performance improvement result with the aid of closed feedback controller loop to a micro gyroscope. The dynamic model of a micro gyroscope is derived and a conventional proportional and derivative controller is designed via frequency domain analysis. The proposed control loop is implemented using several analog devices and applied to the SNU-Bosch MEMS gyroscope to check its performance improvement in real environment. The experiments demonstrated the performance improvement with the proposed feedback control loop. The bandwidth, linearity, and bias stability are improved to 78 Hz, 0.504 %, and 0.043 deg/sec, respectively, from 35 Hz, 2.07 %, and 0.066 deg/sec of open loop system.

• Proceedings of the IEEK Conference
• /
• 2009.05a
• /
• pp.85-87
• /
• 2009

This paper presents a new PID controller for a DC/DC boost converter model that has a parasitic inductor resistance. In order to maintain the robust output regulation property under load variations the proposed controller is designed by using an additional state variable developed via a parallel-damped passivity-based control approach. Simulation results using Matlab/Simulink SimPowerSystems compare the performances of the proposed controller with a conventional PI controller for reference step changes and load uncertainties.

• 제어로봇시스템학회:학술대회논문집
• /
• 1991.10a
• /
• pp.951-956
• /
• 1991

굴삭기 엔진 펌프시스템을 실험결과에 근거해서 모델링하여 수치적으로 시뮬레이션을 행하였다. 엔진.펌프시스템은 그 구성이 복잡할 뿐만 아니라 시스템자체의 비선형성,작업에 따라 시스템에 가해지는 불확실한 외란, 파라미터의 변동으로 인하여 정확한 모델링을 행하기는 다소 어려움이 있었다. 비례제어만을 사용시는 정상상태오차의 발생,초기의 회전수저하등으로 인하여 적합하지 않았다. 이를 개선하기 위하여 PID제어를 사용하였을 경우 정상상태오차는 제거할 수 있으나 정착시간이 길어지는 것을 볼 수 있었다. 슬라이딩모우드에 의한 제어법을 적용하였을 경우 정상상태오차,정착시간,최대회전수저하량을 모두 만족하였으나 과도상태에서 오실레이션이 발생하는 현상을 볼 수 있었다.

• Journal of Institute of Control, Robotics and Systems
• /
• v.16 no.1
• /
• pp.77-82
• /
• 2010

An analytical method for robust design of the multi-loop proportional-integral (PI) controller is proposed for various types of multi-delay processes. On the basis of the direct synthesis and generalized IMC-PID approach, the analytical tuning rules of the multi-loop PI controller are firstly derived for achieving the desired closed-loop response, and the structured singular value synthesis is then utilized for the tradeoffs between the robust stability and performance by adjusting only one design parameter (i.e., the closed-loop time constant). To verify the superiority of the proposed method, the simulation studies have been conducted on a wide variety of multivariable processes. The multi-loop PI controller designed by the proposed method shows a fast, well-balanced and robust response with the minimum integral absolute error (IAE) in compared with other renowned methods.