• 제어로봇시스템학회논문지
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• 제13권9호
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• pp.896-902
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• 2007

This paper proposes a vision-based kinematic control method for mobile robots with camera-on-board. In the previous literature on the control of mobile robots using camera vision information, the forward velocity is set to be a constant, and only the rotational velocity of the robot is controlled. More efficient motion, however, is needed by controlling the forward velocity, depending on the position in the corridor. Thus, both forward and rotational velocities are controlled in the proposed method such that the mobile robots can move faster when the comer of the corridor is far away, and it slows down as it approaches the dead end of the corridor. In this way, the smooth turning motion along the corridor is possible. To this end, visual information using the camera is used to obtain the perspective lines and the distance from the current robot position to the dead end. Then, the vanishing point and the pseudo desired position are obtained, and the forward and rotational velocities are controlled by the LOS(Line Of Sight) guidance law. Both numerical and experimental results are included to demonstrate the validity of the proposed method.

• 해양환경안전학회지
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• 제19권6호
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• pp.637-642
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• 2013

본 연구는 피예인선의 거동을 결정짓는 예인선의 힘과 작용지점의 해석에 대해 언급하고 있다. 예인대상선박의 간략화된 동역학방정식을 바탕으로 선형화기법을 적용하여 목적으로 하는 피예인선의 자세와 위치를 달성하기 위한 예인력과 예인력이 가해져야 하는 지점을 도출하였다. 이를 위해 LQR제어기법을 적용하였으며, 수치적인 시뮬레이션을 수행하였다. 리카치방정식을 이용하여 피예인선의 자세제어를 위한 제어기 이득과 자세제어에 필요한 무게중심에서의 힘을 도출하였고, 도출한 힘과 예인지점의 역학적인 관계는 의사역행렬을 이용하여 구하였다. 이러한 해석기법을 바탕으로 피예인선을 초기위치로부터 목표위치로 예인할 때 예인지점 및 예인방식에 따른 예인력을 구할 수 있었다. 최종적으로 선박을 예인하기 위한 예인력은 예인지점과 방향에 밀접하게 연관되어 있는 것을 확인할 수 있었고 이러한 연구결과는 사고선박의 구난작업 시 예인선의 배치에도 적용이 가능할 것이다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.33-37
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• 2006

Since 1993, the civil aviation community through RTCA (Radio Technical Commission for Aeronautics) and the ICAO (International Civil Air Navigation Organization) have been working on the definition of GNSS augmentation systems that will provide improved levels of accuracy and integrity. These augmentation systems have been classified into three distinct groups: Aircraft Based Augmentation Systems (ABAS), Space Based Augmentation Systems (SBAS) and Ground Based Augmentation Systems (GBAS). The last one is an implemented system to support Air Navigation in CAT-I approaching operation. It consists of three primary subsystems: the GNSS Satellite subsystem that produces the ranging signals and navigation messages; the GBAS ground subsystem, which uses two or more GNSS receivers. It collects pseudo ranges for all GNSS satellites in view and computes and broadcasts differential corrections and integrity-related information; the Aircraft subsystem. Within the area of coverage of the ground station, aircraft subsystems may use the broadcast corrections to compute their own measurements in line with the differential principle. After selection of the desired FAS for the landing runway, the differentially corrected position is used to generate navigation guidance signals. Those are lateral and vertical deviations as well as distance to the threshold crossing point of the selected FAS and integrity flags. The Department of Applied Science in Naples has create for its study a virtual GBAS Ground station. Starting from three GPS double frequency receivers, we collect data of 24h measures session and in post processing we generate the GC (GBAS Correction). For this goal we use the software Pegasus V4.1 developed from EUROCONTROL. Generating the GC we have the possibility to study and monitor GBAS performance and integrity starting from a virtual functional architecture. The latter allows us to collect data without the necessity to found us authorization for the access to restricted area in airport where there is one GBAS installation.