• 한국항공운항학회지
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• 제18권3호
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• pp.27-33
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• 2010

The goal for the CD&R system is to predict that a conflict is going to occur in the future, communicate the detected conflict to a human operator, and, in some cases, assist in the resolution of the conflict situation. To provide insight into different methods of conflict detection and resolution, a literature review of previous research models and current developmental and operational systems was performed. This paper focuses only on the specific attributes of each model, not on the depth to which a model has been analyzed, validated, or accepted. Thus, care should be taken to remember that a model that seems to be simple according to our categorization scheme may be significantly more viable than an apparently sophisticated model.

• 한국자동차공학회논문집
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• 제7권5호
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• pp.240-248
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• 1999

This paper presents a lane-change collision avoidance control algorithm for autonomous vehicles that will be used in AHS(Automated Highway System). In the proposed control algorithm, nominal control inputs are generated by solving the inverse vehicle dynamic equations of motion for a lane-change maneuver. In addition, a corrective steering input from preview as well as DYC (Direct Yaw Moment Control) may be included to reduce unpredictable errors and to insure yaw directional stability, respectively. The performance of the algorithm is evaluated with an ABS HILS system which consist of 17 DOF vehicle model and real ABS hardware parts. The HILS simulation results show that the proposed algorithm may be used for emergency lane-change maneuvers for autonomous vehicles.

• 한국전문물리치료학회지
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• 제22권1호
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• pp.37-48
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• 2015

This study aimed to investigate the effect of the abdominal drawing-in maneuver (ADIM) and abdominal expansion maneuver (AEM) on trunk stabilization, as well as trunk muscle activities and differences in quadruple visual analogue scale, Korean Oswestry Disability Index, and Fear Avoidance Beliefs Questionnaire scores, in patients with chronic low back pain and lumbar spine instability. To increase intra-abdominal pressure during the trunk stabilization exercise, the technique of pushing the abdomen out using diaphragmatic abdominal breathing suggested by Pavel Koral was used, which we termed the AEM. Fifty patients who tested positive on more than three of the five lumbar spine instability tests were separated from 138 patients with chronic low back pain of these patients, 16 were placed in the control group (trunk stabilization exercise), 17 were placed in the ADIM group (trunk stabilization exercise with ADIM), and 17 were placed in the AEM group (trunk stabilization exercise with AEM). Each group participated in the study for 30 minutes three times weekly for 4 weeks. Surface electromyography was used to measure the trunk muscle activities during the kneeling forward and supine bridging positions, and one-way repeated analysis of variance was used to determine the statistical significance of the trunk muscle activities in the rectus abdominis, internal oblique (IO), erector spinae, and multifidus (MF) muscles. The ADIM and AEM groups showed relatively larger improvements in psychosocial and functional disability level than control group. There were significant changes among the three groups, those from the measured values of the AEM group was significantly higher than the other two groups in changes in IO and MF trunk muscle activities (p<.05). This finding demonstrates that trunk stabilization exercises with AEM is more effective than ADIM for increasing trunk deep muscle activity of chronic low back pain patients with lumbar spine instability.

• 해양환경안전학회지
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• 제14권2호
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• pp.157-162
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• 2008

선박의 충돌회피조선에 있어서 조종성능은 중요한 요소이다. 일반적으로 사용되는 조종성능은 심수역을 대상으로 작성되며, 천수역을 항주하는 선박의 조종성은 일반적으로 선회성은 저하되고 침로안정성 또는 추종성은 향상된다. 이러한 선회성의 변화는 충돌회피에 있어 위험을 초래할 수 있다. 본 연구에서는 천수역의 조종성능을 반영함과 동시에 충돌위험정도를 쉽게 파악할 수 있도록 하기 위한 가변안전경계영역의 새로운 적용기법을 제시하였다. 수학적 수치시뮬레이션 검증을 통하여 새롭게 제안된 기법의 유용성을 확인하였다. 따라서 선박충돌위험에 대한 충분한 충돌회피 조선을 지원할 수 있을 것으로 기대된다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제5권2호
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• pp.188-198
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• 2013

In constructing a collision avoidance system, it is important to determine the time for starting collision avoidance maneuver. Many researchers have attempted to formulate various indices by applying a range of techniques. Among these indices, collision risk obtained by combining Distance to the Closest Point of Approach (DCPA) and Time to the Closest Point of Approach (TCPA) information with fuzzy theory is mostly used. However, the collision risk has a limit, in that membership functions of DCPA and TCPA are empirically determined. In addition, the collision risk is not able to consider several critical collision conditions where the target ship fails to take appropriate actions. It is therefore necessary to design a new concept based on logical approaches. In this paper, a collision ratio is proposed, which is the expected ratio of unavoidable paths to total paths under suitably characterized operation conditions. Total paths are determined by considering categories such as action space and methodology of avoidance. The International Regulations for Preventing Collisions at Sea (1972) and collision avoidance rules (2001) are considered to solve the slower ship's dilemma. Different methods which are based on a constant speed model and simulated speed model are used to calculate the relative positions between own ship and target ship. In the simulated speed model, fuzzy control is applied to determination of command rudder angle. At various encounter situations, the time histories of the collision ratio based on the simulated speed model are compared with those based on the constant speed model.

• 수산해양기술연구
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• 제51권2호
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• pp.257-264
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• 2015

This study is intended to provide navigator with specific information necessary to assist the avoidance of collision and the operation of ships to evaluate the maneuverability of dead weight tonnage 8,000 tons Oil/Chemical tanker. The actual maneuvering characteristics of ship can be adequately judged from the results of typical ship trials. Author carried out sea trials based full scale for turning test, Z" maneuvering test, man overboard rescue maneuver test, inertia stopping test. Consequently, $2^{st}$ Overshoot yaw angle of the semi balanced rudder and flap rudder in ${\pm}20^{\circ}$ zig-zag test showed $22.2^{\circ}$ and $18.0^{\circ}$, respectively. The maneuverability of the vessel was good in the flap rudder. The man overboard rescue maneuver maneuverability test was most favorable in the flap rudder and the full load condition. The results from tests could be compared directly with the standards of maneuverability of IMO and consequently the maneuvering qualities of the ship is full satisfied with its.

• 한국항공우주학회지
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• 제34권4호
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• pp.33-39
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• 2006

본 논문에서는 항공기충돌방지장치인 TCAS-II를 응용한 무인항공기의 충돌회피를 다룬다. TCAS-II의 최소운용성능표준 문서에 기초한 시뮬레이션 프로그램을 구현하고, TCAS-II가 제공하는 다양한 수직회피 명령을 자동조종장치의 입력으로 변환하여 최대고도변화율이 상이한 두 가지 무인항공기의 충돌회피 성능을 비교분석한다. 낮은 최대고도변화율을 가진 무인항공기에 TCAS-II를 적용할 때 발생 가능한 Near Mid-Air Collision을 방지할 수 있는 방안으로서, 최대고도변화율과 고도를 고려한 개선된 알고리듬을 제안하였다. 이 알고리듬은 ADS-B 개념에 의한 보다 넓은 감시범위가 제공된다는 전제하에 사용될 수 있다.

• 융합신호처리학회논문지
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• 제19권2호
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• pp.54-60
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• 2018

본 논문에서는 쿼드콥터 드론의 충돌방지를 위한 효율적인 자동제어 방법을 제안한다. 일반적인 드론조종 방법은 RC 조종기에서 노브의 움직임을 PWM 신호로 변환하여 전송하면 이를 드론의 무선 수신부에서 수신하여 비행제어(FC) 모듈에 전달하는 방식으로 이루어진다. 드론의 수신기와 FC 모듈 사이에 충돌 회피 모듈을 구현하여 쓰로틀, 피치 및 롤 제어 신호를 모니터링하고 변경하는 방식으로 드론 충돌을 방지한다. 충돌을 방지하기 위해 LiDAR 거리 센서와 서보 모터를 설치하여 주기적으로 비행 방향을 중심으로 -45도에서 +45도 이내의 장애물 거리를 측정한다. 충돌이 예상되면 수신된 PWM 신호를 변경하여 FC 모듈로 전송함으로써 충돌을 방지한다. 우리가 제안한 방법을 쿼드콥터 드론에 적용하여 실험을 통해 검증한 결과, 조종자 부주의 혹은 조종 미숙으로 인해 발생할 수 있는 충돌을 방지할 수 있어 안전성이 향상됨을 보였다.

• 한국항공우주학회지
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• 제42권9호
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• pp.752-761
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• 2014

뛰어난 기동성으로 인한 최근 쿼드로터에 대한 관심의 증대는 다양한 형태의 멀티로터 비행체의 개발 및 상용화를 이끌었으며, 레져용으로 사용자들이 쉽게 사용할 수 있는 다양한 쿼드로터 제품들이 등장하고 있다. 이 중에서 최근 Parrot사에서 제작한 AR.Drone은 사용자를 위한 내부 안정화 루프를 탑재하고 있기 때문에 초보자들도 쉽게 제어할 수 있는 장점이 있다. 이러한 AR.Drone의 시스템을 이용하면 다양한 형태의 다수 무인기 시스템을 쉽게 구축할 수 있다. 이러한 특성을 바탕으로 한국항공우주연구원에서는 다수의 AR.Drone을 이용한 실내 군집비행 연구를 진행 중에 있다. 이러한 다수의 무인비행체를 이용한 실내 군집비행을 위해서는 개개의 비행체에 대한 위치제어 및 서로간의 충돌을 방지하기 위한 알고리즘이 필요하다. 이를 위해서 본 논문에서는 다수의 실내 무인기의 원활한 기동을 위해 개발한 충돌회피 기동 제어기를 소개하고자 한다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2004년도 ICCAS
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• pp.1747-1753
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• 2004

CMG(Control Momentum Gyro) is a control device being used for spacecraft attitude control constructing relatively large amount of torque compared to conventional body-fixed reaction wheels. The CMG produces gyroscopic control torque by continuously varying the angular momentum vector direction with respect to the spacecraft body. The VSCMG(Variable Speed Control Momentum Gyro) has favorable advantages with variable speed to lead to better control authority as well as singularity avoidance capability. Attitude dynamics with a VSCMG mounted on a two-axis gimbal system are derived in this study. The dynamic equation may be considered as an extension of the single-axis counterpart. Also, a feedback control law design is addressed in conjunction with the dynamic equations of motion.