• 항공우주기술
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• 제10권2호
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• pp.87-93
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• 2011

고정밀 태양센서는 인공위성의 자세제어에 중요 센서로서, 위성으로 입사되는 태양 빛의 방향을 측정하거나 위성이 태양을 보지 못하는 상태에 있는지를 판단하기 위해서 사용되고 있다. 또한 정지궤도 위성에서는 전이궤도 및 임무궤도 상에서 기준 자세로 부터 벗어난 자세오차 정보를 획득하기 위해서 또는 이상 발생 시 태양벡터를 획득하기 위해서 고정밀 태양센서를 사용하고 있다. 본 논문에서는 저궤도 위성과 정지궤도 위성용 고정밀 태양센서의 형상에 대한 이해를 바탕으로 태양의 입사각에 대한 출력 전류 관계를 나타내는 전달 함수를 이용하여 고정밀 태양센서 운용 원리를 설명한다.

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

• 항공우주시스템공학회지
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• 제17권5호
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• pp.34-41
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• 2023

본 논문은 최근 각광받고 있는 소형 무인항공기에 결빙효과와 윙락 불확실성을 적용하고 여러 제어기법을 활용하여 자세 제어 시뮬레이션 수행하였으며 그 결과를 다룬다. 먼저 선정 기체인 BWB 형태의 소형 무인 항공기인 Skywalker X8 기체의 기본 형상과 결빙효과가 적용된 형상에 대하여 선형화를 수행하였다. 이후 MATLAB SimulinkⓇ를 활용하여 외란 관측기 기반 PID 제어, 모델 참조 적응 제어, 모델 예측 제어기법을 사용하여 기본 형상과 결빙효과가 적용된 형상에 대하여 roll 및 pitch 자세 제어 시뮬레이션을 수행한다. 또한, 기존 연구에서 진행되지 않았던 윙락 불확실성을 결빙이 적용된 형상에 동시 적용하여 시뮬레이션을 수행하였으며 각 제어기법의 성능을 비교 분석하였다.

• 제어로봇시스템학회논문지
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• 제20권11호
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• pp.1098-1102
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• 2014

Localization of aerial vehicles and map building of flight environments are key technologies for the autonomous flight of small UAVs. In outdoor environments, an unmanned aircraft can easily use a GPS (Global Positioning System) for its localization with acceptable accuracy. However, as the GPS is not available for use in indoor environments, the development of a SLAM (Simultaneous Localization and Mapping) system that is suitable for small UAVs is therefore needed. In this paper, we suggest a vision-based SLAM system that uses vision sensors and an AHRS (Attitude Heading Reference System) sensor. Feature points in images captured from the vision sensor are obtained by using GPU (Graphics Process Unit) based SIFT (Scale-invariant Feature Transform) algorithm. Those feature points are then combined with attitude information obtained from the AHRS to estimate the position of the small UAV. Based on the location information and color distribution, a Gaussian process model is generated, which could be a map. The experimental results show that the position of a small unmanned aircraft is estimated properly and the map of the environment is constructed by using the proposed method. Finally, the reliability of the proposed method is verified by comparing the difference between the estimated values and the actual values.

• 한국치위생학회지
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• 제17권2호
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• pp.295-305
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• 2017

Objectives: This study was performed to provide a reference base to establish foundation for education about dental hygienist-related medical law and introduction of the system. Methods: A survey was conducted on 210 dental hygienists working at a dental clinic/ hospital in Jeollado. Data were analysed through chi-square test, one-way ANOVA, independent t-test, and Pearson's correlation analysis using SPSS 21.0 program. The study instruments included general characteristics of the subjects, knowledge on laws related to dental hygiene, attitude towards dental hygienist-related medical laws, level of understanding of medical related laws, and medical dispute educational hours. Results: The knowledge of dental hygienist-related medical law was high in dental hygienists aged 25 years and younger and with less than 3 years of clinical experience (p<0.05). The attitude towards the law was low in age of younger than 25 years, a three year college degree, a job position as a staff member, more than 5 years of work experience at present work place, and less than 3 years of clinical experience (p<0.05). Understanding of medical related laws was high in clinical staff members and with less than 3 years of clinical experience (p<0.05). Educational needs for medical dispute prevention was high in a job position as a staff member, low level of attitude towards dental hygienist-related medical law, and no attainment of education on medical dispute (p<0.05). Conclusions: The above results demonstrate that education and public relations about laws related with dental hygiene practice are essential. It is imperative to establish a systematic and bureaucratic legal system to prevent dental malpractice.

• 재활복지공학회논문지
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• 제9권2호
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• pp.137-144
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• 2015

본 논문은 하지의 움직임을 측정하고 분석할 수 있는 관성센서 기반 보행분석 시스템에 관한 것이다. 본 시스템 구현을 위해 자이로스코프, 가속도계 및 지자계 신호를 이용한 자세 방위 측정장치 모듈을 일체형으로 개발하였으며, 다수의 모듈을 환자의 분절에 부착하여 공간상에서 각 분절의 방위각을 제공할 수 있도록 하였다. 또한 재활과 관련된 많은 응용에 있어 중요한 생체역학 측정값인 신체 분절간의 관절각을 추출하는 알고리즘을 제안하였다. 개발한 자세 방위 측정장치 모듈의 성능을 평가하기 위하여 3차원 공간상의 변위 및 방위를 밀리미터 해상도로 제공할 수 있는 Vicon을 참조 측정 시스템으로 이용하였으며, yaw와 pitch에서 1.08, 1.72도의 평균 제곱근 오차를 얻을 수 있었다. 보행 분석 시스템의 성능 검증을 위하여 7개의 AHRS 모듈을 하지에 부착하고 고관절, 무릎, 발목에 대한 관절각을 계산하여, Vicon과의 비교 실험을 수행하였다. 실험 결과 본 연구에서 개발한 시스템은 뇌졸중 후 회복단계 동안 사지 및 보행 동작을 실시간으로 분석, 제공함으로서 재활의 효과, 난이도 조절 및 피드백 요소를 제공할 수 있을 것으로 판단된다.

• International Journal of Aeronautical and Space Sciences
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• 제11권3호
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• pp.240-245
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• 2010

The controller of a model reference adaptive control monitors the plant's inputs and outputs to acknowledge its characteristics. It then adapts itself to the characteristics it encounters instead of behaving in a fixed manner. An important part of every adaptive scheme is the adaptive law for estimating the unknown parameters on line. A more precise model is required to improve performance and to stabilize a given dynamic system, such as a satellite in which performance varies over time and the coefficients change due to disturbances, etc. After model identification, the robust controller ($H{\infty}$) is designed to stabilize the rigid body and flexible body of a satellite, which can be perturbed due to disturbance. The result obtained by the $H{\infty}$ controller is compared with that of the proportional and integration controller which is commonly used for stabilizing a satellite.

• 한국정보통신학회논문지
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• 제3권2호
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• pp.397-402
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• 1999

본 논문에서는 모형 헬리콥터의 동적방정식을 유도하고 이 헬리콥터의 자세를 제어하기 위해서 신경망을 이용한 제어법을 제안하였다. 신경망의 결합계수들은 제어계의 출력과 기준시간의 오차를 최소화하도록 조종된다. 제안한 제어기의 이득은 신경망의 역전파 알고리즘에 의해서 자동적으로 조정된다. MATLAB을 이용한 시뮬레이션 결과를 제시하였다.

• 한국컴퓨터정보학회논문지
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• 제20권10호
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• pp.113-119
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• 2015

In this paper, we propose an efficient freedom of information and Information access right which improves transparent and speedy administration process. To build open Information, we scrutinize that causes of non access right and change of civil service consciousness, attitude for open information by effectively open system circumstances. The Important thing is basic information that is available to the public through an agency's FOIA Reference Guide, all agencies must notify potential FOIA requesters of the formal rules and requirements for the making and handling of FOIA request, through their FOIA regulations. The characteristics of this paper focused on Information access right, causes of non access right and proposed policy. In this paper, The author emphasize are as follows: first, to examine freedom of information' necessity and problem that scrutinize a theoretic analysis, second, to understand civil servant's attitude for the freedom of information, third, to suggest action plan and agenda for the better of Good Governance and Democracy of information.

• 한국항공우주학회지
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• 제44권5호
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• pp.416-422
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• 2016

본 논문에서는 연세대학교 천문우주학과 우주비행제어연구실에서 개발 중인 인공위성 편대비행 테스트베드에 대한 예비 성능분석 결과를 제시하였다. 동역학 모델에 포함되지 않은 동특성과 측정 잡음 등에 의한 불확실성의 영향을 받는 반작용 휠의 응답 성능을 향상시키기 위하여 간단한 1차 선형시스템을 기준 모델로 하는 적응제어기를 설계하였다. 또한 자세 측정값에 잡음이 포함된 환경에서도 원활한 제어를 수행하기 위해 최소제곱법 기반의 실시간 파라미터 추정기법을 이용하여 관성모멘트를 추정하였다. 수치 시뮬레이션과 하드웨어 실험을 통해 설계된 모델 기준 적응제어기의 적합성과 향후 적용가능성을 검토하였고, 전 시간에 걸친 자세 추적오차가 $0.25^{\circ}$ 이내에 머무는 것을 확인하였다. 하지만 하드웨어 실험을 통해 드러난 제어 입력에 대한 데드존의 영향을 줄이기 위해서는 인공위성 시뮬레이터의 설계 변경이 필요하다고 판단된다.