• International Journal of Aeronautical and Space Sciences
• /
• 제8권1호
• /
• pp.10-20
• /
• 2007

For spacecraft attitude control, reaction wheel (RW) steering laws with more than three wheels for three-axis attitude control can be derived by using a control allocation (CA) approach.1-2 The CA technique deals with a problem of distributing a given control demand to available sets of actuators.3-4 There are many references for CA with applications to aerospace systems. For spacecraft, the control torque command for three body-fixed reference frames can be constructed by a combination of multiple wheels, usually four-wheel pyramid sets. Multi-wheel configurations can be exploited to satisfy a body-axis control torque requirement while satisfying objectives such as minimum control energy.1-2 In general, the reaction wheel steering laws determine required torque command for each wheel in the form of matrix pseudo-inverse. In general, the attitude control command is generated in the form of a feedback control. The spacecraft body angular rate measured by gyros is used to estimate angular displacement also.⁵ Combination of the body angular rate and attitude parameters such as quaternion and MRPs(Modified Rodrigues Parameters) is typically used in synthesizing the control command which should be produced by RWs.¹ The attitude sensor signals are usually corrupted by noise; gyros tend to contain errors such as drift and random noise. The attitude determination system can estimate such errors, and provide best true signals for feedback control.⁶ Even if the attitude determination system, for instance, sophisticated algorithm such as the EKF(Extended Kalman Filter) algorithm⁶, can eliminate the errors efficiently, it is quite probable that the control command still contains noise sources. The noise and/or other high frequency components in the control command would cause the wheel speed to change in an undesirable manner. The closed-loop system, governed by the feedback control law, is also directly affected by the noise due to imperfect sensor characteristics. The noise components in the sensor signal should be mitigated so that the control command is isolated from the noise effect. This can be done by adding a filter to the sensor output or preventing rapid change in the control command. Dynamic control allocation(DCA), recently studied by Härkegård, is to distribute the control command in the sense of dynamics⁴: the allocation is made over a certain time interval, not a fixed time instant. The dynamic behavior of the control command is taken into account in the course of distributing the control command. Not only the control command requirement, but also variation of the control command over a sampling interval is included in the performance criterion to be optimized. The result is a control command in the form of a finite difference equation over the given time interval.⁴ It results in a filter dynamics by taking the previous control command into account for the synthesis of current control command. Stability of the proposed dynamic control allocation (CA) approach was proved to ensure the control command is bounded at the steady-state. In this study, we extended the results presented in Ref. 4 by adding a two-step dynamic CA term in deriving the control allocation law. Also, the strict equality constraint, between the virtual and actual control inputs, is relaxed in order to construct control command with a smooth profile. The proposed DCA technique is applied to a spacecraft attitude control problem. The sensor noise and/or irregular signals, which are existent in most of spacecraft attitude sensors, can be handled effectively by the proposed approach.

• Journal of Power Electronics
• /
• 제16권4호
• /
• pp.1483-1493
• /
• 2016

Multiple parallel inverters have multiple resonant frequencies that are influenced by many factors. This often results in stability and power quality problems. This paper develops a multiple input multiple output model of grid-connected inverter systems using a closed-loop transfer function. The influence factors of the resonant characteristics are analyzed with the developed model. The analysis results show that the resonant frequency is closely related to the number, type and composition ratio of the parallel inverters. To suppress resonance, a scheme based on virtual impedance is presented, where the virtual impedance is emulated in the vicinity of the resonance frequency. The proposed scheme needs one inverter with virtual impedance control, which reduces the design complexity of the other inverter controllers. Simulation and experimental tests are carried out on two single phase converter-based setups. The results validate the correctness of the model, the analytical results and the resonant suppressing scheme.

• 전력전자학회:학술대회논문집
• /
• 전력전자학회 2008년도 하계학술대회 논문집
• /
• pp.106-108
• /
• 2008

This paper deals with the design for speed controller to drive PMSM by matrix converter without DC-link circuit as the power conversion system of AC servo motor drive. To design the speed controller of PMSM drive, the closed-loop transfer function of speed controller is calculated and then the frequency-domain response characteristics are analyzed by bode plot using Matlab. Based on the results by bode plot, the speed control gains are determined. As the real effects of controller designed in the frequency-domain display in the time-domain, the performance of speed controller is confirmed by the step response of speed controller. The design examples are shown and its validity of the design method mentioned in the paper is verified through PSIM simulation.

• 전자공학회논문지SC
• /
• 제42권6호
• /
• pp.1-8
• /
• 2005

슬라이딩 모드 제어기의 성능을 향상시키기 위해서 새로운 프로세스 모델의 파라미터 계산을 제안하였다. Camacho가 제안한 방법은 시간 지연항을 1차 Taylor 급수로 근사화하는 과정에서 발생되는 근사 오차에 의한 오버슈트, 정착시간 등에 문제점이 발생하였다. 본 논문에서는 이러한 문제점을 해결하기 위해 가중치를 고려한 변형된 파데 근사 방법과 이를 토대로 한 새로운 슬라이딩 모드 제어기의 동조 방법을 제안하였다. 제안된 방법은 프로세스 응답을 복잡한 수치적 과정없이 온라인으로 직접 동조 파라미터를 구할 수 있다.

• 전자공학회논문지
• /
• 제50권5호
• /
• pp.253-261
• /
• 2013

본 논문에서는 복합 비동기 순차 머신을 제어하는 방법을 다룬다. 논문에서 고려하는 비동기 머신은 입력/상태 머신 두 개가 직렬 결합된 것으로서 선행 머신의 출력 값이 후행 머신의 입력으로 전달된다. 제어 목적은 폐루프 시스템의 입력과 출력의 정상 상태 특성을 원하는 모델의 동작과 일치시키는 모델 정합 문제를 구현하는 교정 제어기를 꾸미는 일이다. 교정 제어기는 후행 머신의 상태 피드백 정보만 전달 받기 때문에 선행 머신의 상태를 정확하게 알 수 없는 불확실성이 존재한다. 본 논문에서는 그러한 불확실성 하에서 모델 정합 교정 제어기가 존재할 조건을 구하고 설계 알고리듬을 제안한다. 또한 사례 연구를 통해서 제안된 제어기의 설계 과정을 예시한다.

• Journal of Power Electronics
• /
• 제1권2호
• /
• pp.117-126
• /
• 2001

A synchronous motor(SM) with q-axis special field winding of which the q-axis field-current compensates and cancels armature reaction can be driven at unity power factor under the conditions of transient state as well as steady state. The motor operates in high efficiency in all conditions. However, in order to obtain maximum performance of the motor, it is required that the time constant of armature circuit corresponds to that of q-axis field circuit. Inverse LQ(ILQ) design method on a basis of the pole assignment is suitable for this problem:(1) The time constants of the output responses can be designed for desired specifications, (2) Relations between feedback gains and response of closed loop system are very clear and (3) Optimal solutions can be given by simple procedure of ILQ method without solving the Ricaati's equation, compared to the usual LQ design method. Accordingly, the ILQ method can make the responses of armature current and q-axis field-current correspond. In this paper, it is proved by numerical simulations and experiments that the ILQ method is very effective for optimal regulator design of this plant and realizes a high-performance motor with unity power factor and high efficiency.

• 전자공학회논문지SC
• /
• 제49권4호
• /
• pp.61-68
• /
• 2012

본 논문에서는 리니어 컴프레서를 위한 폐루우프 센서리스 스트로크 제어시스템이 구성되었다. 피스톤 위치를 정확히 알아내기 위해 모터 매개변수를 피스톤 위치와 모터 전류의 함수로 추정하였다. 이 매개변수 데이터는 ROM 테이블에 저장한 뒤 차 후 피스톤 위치를 정확히 알아내는데 사용된다. 또한, 추정된 전동기 매개변수의 데이터 크기를 줄이기 위해 여러 형태의 곡면 함수로 근사화 하는 작업을 수행하였고, 공간분할을 통해 추정오차를 줄일 수 있었다. 곡면함수의 차수와 공간분할의 개수가 매개변수의 추정오차와 연산시간에 미치는 영향을 분석하였다.

• 비파괴검사학회지
• /
• 제28권4호
• /
• pp.372-376
• /
• 2008

We report experimental results on the correlations between welding penetration depth and the frequencies of the radiation from the welding pool. Various welding samples such as SUS304, brass, SUS316, etc. have been investigated with 2 kW CW Nd:YAG laser welding machine. The radiation signals from the plume generated by the interactions between the welding sample and laser with respect to the defocusing length was measured with fiber system collecting the plume signal. Analysis of the frequencies by using fast Fourier transform (FFT) shows that the penetration depth is deep as plume signal frequencies are low, shallow penetration depth for high frequencies. Frequencies up to 250 Hz for obtained signals can be analyzed with the discrete FFT. This is the useful method fur closed loop control of the laser power with respect to the welding penetration depth and is used for real time inspection of the welding quality.

• 로봇학회논문지
• /
• 제18권3호
• /
• pp.299-307
• /
• 2023

In the midst of accelerating wars around the world, unmanned robot technology that can guarantee the safety of human life is emerging. ERP-42 is a modular platform that can be used according to the application. In the field of defense, it can be used for transporting supplies, reconnaissance and surveillance, and medical evacuation in conflict areas. Due to the nature of the military environment, atypical environments are predominant, and in such environments, the platform's path followability is an important part of mission performance. This paper focuses on reducing the minimum turning radius in terms of improving path followability. The minimum turning radius of the existing 2WS/2WD in-wheel platform was reduced by increasing the torque of the independent driving in-wheel motor on the rear wheel to generate oversteer. To determine the degree of oversteer, two GPS were attached to the center of the front and rear wheelbases and measured. A closed-loop speed control method was used to maintain a constant rotational speed of each wheel despite changes in load or torque.

• 대한토목학회논문집
• /
• 제26권5A호
• /
• pp.849-859
• /
• 2006

본 연구에서는 벤치마크 사장교를 이용해 다양한 불확실성에 대해서 복합시스템에 사용된 ${\mu}$-제어기의 강인성 해석을 수행하였다. 복합 시스템에 추가적으로 사용된 능동제어 장치로 인하여 전체 시스템의 강인성이 저하되거나 불안정성이 발생할 수 있다. 따라서 본 연구에서는 복합 시스템의 강인성을 향상 시키기 위해 기본적으로 신뢰성이 확보되는 수동장치와 함께 불확실성을 포함한 시스템의 성능과 안정성(강인성능)을 보장하는 ${\mu}$-합성법을 능동제어 장치에 사용하였다. 교량상판에 추가적인 질량, 구조물 강성행렬에 대한 섭동, 능동제어 장치의 시간지연, 그리고 이들의 조합을 이용하여 ${\mu}$-합성법의 강인성을 조사하였다. 수치해석 결과 다양한 불확실성에 대해 제안된 시스템은 제어성능의 저하 없이 뛰어난 강인성을 보여 주었다. 또한 제어시스템의 강인성은 다른 불확실성에 비해 구조물의 강성행렬 섭동에 더 큰 영향을 받는다. 따라서 ${\mu}$-합성법으로 제어되는 복합 시스템은 불확실성이 많은 지진하중을 받는 사장교에 개선된 제어기법으로 제안될 수 있다.