• 한국항해학회지
• /
• 제17권1호
• /
• pp.91-98
• /
• 1993

This paper presents a class of Bayes estimation of component steady-state availability . Throughout this paper, we will denote the mean time between failure and the mean time between repair by MTBF and MTBR respectively. In section 2 , we investigated Bayes estimation of the steady-state availability for noninformative prior density function and in section 3, we compute Bayes estimation for conjugate prior density function.

• 한국항해학회지
• /
• 제24권3호
• /
• pp.141-145
• /
• 2000

In servo-system which need fast response and accuracy, PID controller has a good steady-state performance, but has a poor transient response performance causing a load be changed. Compared to these features, FLC(Fuzzy Logic Controller) has a good transient response performance for changed load, but has a little Poor steady-state performance. In this paper, Compensated Fuzay Controller which consists of PID controller and FLC is proposed to modify these disadvantages and is examined through simulation to evaluate its functions.

• 한국항해항만학회지
• /
• 제27권6호
• /
• pp.625-630
• /
• 2003

In order to keep the safety of maneuverability under the lateral berthing, it is necessary to estimate the magnitudes and properties of the hydrodynamic forces acting on ship hull quantitatively. In this paper, CFD technique is used to calculate the steady lateral force according to the water depth for Wigley model under the unsteady lateral berthing. The numerical results are analysed into the steady lateral force and the transitional lateral force, and some of reviews for the safety of maneuverability relating to the lateral berthing are discussed based on the computed hydrodynamic forces.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2001년도 ICCAS
• /
• pp.61.2-61
• /
• 2001

The purpose of the initial alignment of a SDINS is to get a coordinate transformation matrix from the body frame to the navigation frame. The initial alignment is one of the most important processes in the navigation system since its error has a large influence on the navigation solution. In this paper, a real-time initial alignment algorithm for the SDINS is developed using the Kalman filter. The steady state error analysis is performed for the developed Kalman filter technique and the gyrocompass loop method. The performance of the developed alignment method is compared with the gyrocompass loop method through the real-time alignment experiments.

• 제어로봇시스템학회논문지
• /
• 제17권2호
• /
• pp.183-189
• /
• 2011

An alignment algorithm for strapdown inertial navigation systems is proposed, in which the psi angle error model is utilized. The proposed alignment algorithm is derived from the Psi angle error model which has been widely used in real-time navigation systems. The equation for expecting steady state alignment error is also derived. The proposed algorithm was verified through real-time experiments. Experimental results show that the proposed algorithm can be used in the inertial navigation system and GNSS/INS integrated navigation system to get an initial attitude of the vehicle.

• 한국항해항만학회:학술대회논문집
• /
• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
• /
• pp.89-93
• /
• 2006

This paper is primarily focused on the safe navigation between overtaking and overtaken vessels in restricted waterways under the external forces, such as wind and current. The maneuvering simulation between two ships was conducted to find an appropriate safe speed and distance, which is required to avoid collision. From the viewpoint of marine safety, a greater transverse distance between two ships is more needed for the smaller vessel. Regardless of external forces, the smaller vessel will get a greater effect of hydrodynamic forces than the bigger one. In the case of close navigation between ships under the forces of wind and current, the vessel moving at a lower speed is potentially hazardous because the rudder force of the lower speed vessel is not sufficient for steady-state course-keeping, compared to that of the higher speed vessel.

• 한국항행학회논문지
• /
• 제7권1호
• /
• pp.6-13
• /
• 2003

본 논문에서는 3GPP HSDPA 모뎀용 비동기식 동기추적회로를 설계하고, 설계된 동기추적회로에 대하여 정상상태 지터 분산과 타이밍 에러의 과도응답 특성을 이론적으로 분석하였다. 우선 AWGN 환경에서의 지터 분산을 펄스성형 필터, 타이밍 오프셋, 신호 대 잡음비, 루프 대역폭에 대한 식으로 유도하였으며, 과도응답 특성 또한 이론적으로 해석하였다. 끝으로 설계된 동기추적회로의 성능을 컴퓨터 시뮬레이션을 통하여 확인하였다.

• 해양환경안전학회:학술대회논문집
• /
• 해양환경안전학회 2006년도 추계학술발표회
• /
• pp.143-149
• /
• 2006

This paper is primarily focused on the safe navigation between overtaking and overtaken vesselsin restricted waterways under the external forces, such as wind and current. The maneuvering simulation between two ships was conducted to find an appropriate safe speed and distance, which is required to avoid collision. From the viewpoint of marine safety, a greater transversedistance between two ships is more needed for the smaller vessel. Regardless of external forces, the smaller vessel will get a greater effect of hydrodynamic forces than the higher one. In the case of close navigation between ships under the forces of wind and current, the vessel moving at a lower speed is potentially hazardous because the rudder force of the lower speed vessel is not sufficient for steady-state course-keeping, compared to that of the higher speed vessel.

• Journal of Advanced Marine Engineering and Technology
• /
• 제36권6호
• /
• pp.788-793
• /
• 2012

본 연구는 해군함정에 탑재되어 있는 주 추진 디젤엔진에서 배출되는 입자상 물질, 황산화물, 이산화탄소 및 질소산화물의 배출량 예측에 초점을 두었다. 국제사회 및 각국의 정부는 인간의 건강 및 환경을 보호하기 위해 선박의 배기가스 규제를 엄격히 적용하고 있으며 선박 제작사들은 이러한 법규에 대응하기 위해 다양한 기술을 선박에 적용시키고 있다. 엄격히 적용되는 배기가스 법규는 선박의 크기에 따라 차이를 보이고 있지만 함정은 규제대상에서 제외된다. 다양한 연구결과에 의해 선박의 배기가스 배출량 계수(emission factor)는 지속적으로 최신화되고 있으나 함정의 배출량 계수는 그 특성의 차이 때문에 설정이 어려운 실정이다. 본 논문은 함정 엔진의 연료소모량과 함정에서 사용하고 있는 연료의 황성분 함량을 분석하여 항해 시 선박에 적용되고 있는 오염물질 기여도 조사(emission inventory) 방법론을 해군함정에 적용시켜 정속항해 조건에서 배기가스 총 배출량을 예측하는 것이다.

• Journal of Astronomy and Space Sciences
• /
• 제26권1호
• /
• pp.59-74
• /
• 2009

Relative navigation system is presented using GPS measurements from a single-channel global positioning system (GPS) simulator. The objective of this study is to provide the real-time inter-satellite relative positions as well as absolute positions for two formation flying satellites in low earth orbit. To improve the navigation performance, the absolute states are estimated using ion-free GRAPHIC (group and phase ionospheric correction) pseudo-ranges and the relative states are determined using double differential carrier-phase data and singled-differential C/A code data based on the extended Kalman filter and the unscented Kalman filter. Furthermore, pseudo-relative dynamic model and modified relative measurement model are developed. This modified EKF method prevents non-linearity of the measurement model from degrading precision by applying linearization about absolute navigation solutions not about the priori estimates. The LAMBDA method also has been used to improve the relative navigation performance by fixing ambiguities to integers for precise relative navigation. The software-based simulation has been performed and the steady state accuracies of 1 m and 6 mm ($1{\sigma}$ of 3-dimensional difference errors) are achieved for the absolute and relative navigation using EKF for a short baseline leader/follower formation. In addition, the navigation performances are compared for the EKF and the UKF for 10 hours simulation, and relative position errors are mm-level for the two filters showing the similar trends.