• Journal of the Korean Society for Aviation and Aeronautics
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• v.21 no.4
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• pp.34-40
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• 2013

Attitude command response type required for enhanced handling qualities of helicopter can be implemented by mechanical automatic flight control system with SAS actuators which have limited authorities. However, the early saturation of SAS actuator hinders the helicopter from following the attitude command for large stick command. Auto-trim controller can delay SAS actuator's saturation by utilizing trim actuators and allows the attitude command response type for larger stick command. This paper describes the control law for limited authority system of helicopter with auto-trim. Limited authority system is applied to BO-105 linear dynamic model and simulation is performed along with handling quality analysis.

• Proceedings of the Korea Information Processing Society Conference
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• 2016.04a
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• pp.851-853
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• 2016

본 논문은 물류 작업을 위한 지상 보행이 가능한 드론의 제어기를 개선시키기 위한 방법 중 하나로 비선형 자세제어기를 적용한 결과를 보여준다. 로봇은 물류 작업을 위하여 설계되었는데, 페이로드의 변화에 따라서 모델 파라미터가 변하기 때문에 특별한 제어기가 필요하다. 따라서 기존 연구에서 제안되었던 비선형 적응제어기를 채택하여 실험 모델에 적용시켰다. 실험은 실내에서 진행되었고 초기 조건에서 30초 간 자세 안정화 명령의 응답 특성을 확인하는 방식으로 진행되었고, 제어기의 실효성과 안정성을 입증했다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2011.10a
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• pp.609-610
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• 2011

최근 친환경 생활이 강조되는 오늘날, 자전거(bicycle) 이용자 수가 급격히 늘어나고 있다. 때문에 2륜 자전거의 무인화 및 다양한 기구학적 재해석과 구조학적 재해석을 시도하고 있으며 공학적으로 활발한 연구가 진행되고 있다. 본 논문은 복잡한 2륜 자전거의 복잡한 동역학 방정식을 분석한 결과 인버터 팬들럼 모델과 유사한 점을 수학적 전개를 통하여 알 수 있었다. 이렇게 근사화된 방정식 모델을 바탕으로 비선형 제어 알고리즘을 통하여 비선형 제어기를 설계하여 2륜 자전거의 주행 안정성에 대한 진행속도와 조향각(steering angle) 제어에 대한 상관관계에 대한 연구를 시뮬레이션을 통하여 결과를 분석하고자 한다. 이러한 분석을 통한 2륜 자전거의 자세제어를 통하여 기타 로봇의 자세제어 및 다양한 시스템에 적용 가능성을 제시하고자 한다.

• Journal of the Korean Institute of Intelligent Systems
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• v.22 no.4
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• pp.448-453
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• 2012

There are many researches to develop robots that improve its mobility to adapt in various uneven environments. In the paper, a hybrid wheeled and legged mobile robot is designed and a obstacle avoidance algorithm is proposed based on low power walking using LRF(Laser Range Finder). In order to stabilize the robot's motion and reduce energy consumption, we implement a low-power walking algorithm through comparison of the current value of each motors and correction of posture balance. A low-power obstacle avoidance algorithm is proposed by using LRF sensor. We improve walking stability by distributing power consumption and reduce energy consumption by selecting a shortest navigation path of the robot. The proposed methods are verified through walking and navigation experiments with the developed hybrid robot.

• Journal of the Korea Society for Simulation
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• v.28 no.2
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• pp.23-33
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• 2019

A sub-munition which has low aspect ratio does not have flight stability and control of drag force under free-fall condition. In order to satisfy those problems, fin, which is called grid-fin, is designed instead of conventional flight fins and adapted to the sub-munition. The base model of the sub-munition is firstly set and numerical simulation of the model is conducted under transonic condition that is free-fall range of the sub-munition. Wind test is secondly performed to verify the simulation result. The result shows that grid fin adapted sub-munition has high drag force, but the flight stability is still needed. In order to enhance the flight stability, two additional grid-fins are designed which modify web-thickness and numerical simulations of modified models are conducted. As the results, the thinnest web-thickness grid-fin has the highest flight stability and still maintains high drag coefficient. Based on these results, design of grid-fin adapted sub-munition is completed, the path trajectory of the sub-munition can be predicted with acquired aerodynamic datum and it is expected that grid fin can be used to various shape of the flight vehicle and bomb.

• Journal of Navigation and Port Research
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• v.28 no.6
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• pp.469-474
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• 2004

In this paper, we study the posture control of an underwater vehicle with nonholonomic constraint. Generally, systems with nonholnomic constraints cannot be stabilized to an equilibrium points by smooth state feedback control. For the nonholonomic underwater vehicle system, we applied coordinate transformation to get multi-chained system We proposed non smooth feedback controller using backstepping method for stabilizing the multi chained form system Applying inverse input transformation to the non smooth feedback controller, we can get posture controller of the underwater vehicle with nonholonomic constraint. The proposed control scheme is applied to the posture control qf an underwater vehicle and verified the effectiveness of control strategy by numerical simulation.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.176.2-176.2
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• 2012

다목적실용위성 3호의 태양전지판은 위성의 -Z축 방향에 고정되어 있는 방식으로 사용되고 있다. 이로 인해 위성이 임무수행을 위한 자세기동을 하게 되면 태양전지판의 태양입사각 변화에 따라 전력생산량이 변하게 되고 이를 예측하여 최대 방전률(DOD : Depth of Discharge)을 넘지 않는 제한조건 내에서 임무 계획을 수행해야 한다. 전력생산량 및 전력소비량을 예측하기 위해서는 전력 모의실험을 수행해야 하며 이를 위해 위성의 자세 및 위치정보, 임무를 고려한 Mission Profile, 태양입사각, 초기 방전률 값을 생성해야 한다. 본 논문은 태양입사각 계산을 위해 위성의 임무(영상 촬영, 지상국 교신)를 반영한 자세 및 위치 정보를 생성하고, 이 결과를 태양입사각 계산 로직에 적용하여 태양입사각을 생성한 결과를 정리하였다. 생성된 결과의 타당성을 검토하기 위해 상용 툴인 STK를 이용하여 비교를 수행하였다. 또한, 전력 모의실험에 사용된 Mission Profile은 위성 운용에 안정성을 높이며 복잡한 임무 시나리오에 적용이 용이하도록 운용 Margin을 고려하여 생성하였다. 본 논문에서 제시한 방안을 실제 수행된 임무 시나리오에 적용하여 전력 모의실험을 수행하였으며, 그 결과를 임무 수행 후 획득된 위성 Telemetry를 이용한 실측값과 비교하여 전력 모의 실험 결과에 대한 타당성을 검증하였다. 실제 초기 운영결과 제한된 전력 허용 범위 내에서 적용이 가능함을 확인할 수 있었다.

• Journal of the Korean Society of Physical Medicine
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• v.3 no.3
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• pp.169-176
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• 2008

Purpose : Tandem stance is a clinical measure of standing balance considered to assess postural steadiness in a heel-to-toe position by a temporal measurement. The aim of this study is to investigate postural steadiness and to explore the weight distribution between legs during 25s of quiet stance and tandem stance(right foot was leading) in healthy young adults. Methods : 107 healthy young adults(mean age 21.1 years) are participated. Weight distribution beneath both feet and sway distance were recorded while the subjects performed 25s of quiet stance and tandem stance. Results : Subjects placed more weight on the rear leg in tandem stance and on the left foot in quiet stance. So, quiet stance and tandem stance is not a task for equal weight bearing. Subjects show larger sway distance in anteroposterior direction of tandem stance than quiet stance. Conclusion : The results of this study will be useful to researchers and clinicians using tandem stance measures to evaluate postural steadiness and to predict fall. The results suggest that tandem stance is useful to treat of weight distribution and to improve of balace in elderly adults and stroke patients.

• Journal of Auto-vehicle Safety Association
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• v.7 no.2
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• pp.32-38
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• 2015

A sine with dwell test is well known as a test scenario for evaluation of performance of electronic stability control(ESC) on passenger vehicles and heavy commercial vehicles. However, when it comes to ESC for medium commercial vehicles, the test scenario has not been established yet. In this paper, the sine with dwell test was modified considering characteristics of medium commercial vehicles. The three main modifications of the original test scenario are the steering angle level, steering frequency, and loading condition of the vehicle. These modifications are derived from simulation study for different medium commercial vehicles. From simulation study, it was shown that the ESC system for medium commercial vehicle is objectively evaluated by the proposed test scenario. A clear improvement on vehicle stability was seen in the results when ESC system was used.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.23 no.1
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• pp.67-73
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• 2015

The previous limited authority system capable of implementing attitude command response type and translational command response type by operating SAS actuator has the problem of early saturation of SAS actuator since SAS actuator should compensate the mechanical linkage displacement caused by control sick movement. In this paper, a limited authority system where flight control computer receives the command from the control stick which is not connected to the mechanical linkage is described. In this system the compensation by the SAS actuator is not necessary and SAS actuator saturate later. SAS actuator saturation problem can be further relaxed by using the trim actuator. This new limited authority system is applied to BO-105 model, simulation is performed for the doublet input and pirouette maneuver is also simulated and analyzed.