TY - GEN
T1 - Development of an autonomous OBEM measurement vehicle for offshore resources exploration
AU - Yamaguchi, Satoru
AU - Hirofumi, Sumoto
AU - Katsu, Taishiro
AU - Kono, Yasuki
N1 - Funding Information:
This work was supported by Grant-in-Aid (JSPS 26289336).
PY - 2017
Y1 - 2017
N2 - An autonomous underwater glider which equips an OBEM (Ocean Bottom Electromagnetometer) for the ocean bottom resources explorations is proposed. The vehicle is composed of a main wing for gliding and tail wings for motion control of the vehicle. Buoyancy and center of gravity control systems, a buttery, sensors and electric devices are contained in water tight vessels under the main wing. This autonomous vehicle has an ability to achieve a long term continuous resources exploration using OBEM. The buoyancy and attitude control mechanism enables the vehicle to move to the next measurement point by gliding. The landing point for the measurement is precisely controlled by the motion control system. In this report, numerical calculations based on CFD are carried out to design a suitable main wing shape and these results are confirmed in comparison with tank experiments. The gliding performance of the vehicle which has a blended wing shape is discussed based on the calculations and the development of a prototype vehicle is also shown.
AB - An autonomous underwater glider which equips an OBEM (Ocean Bottom Electromagnetometer) for the ocean bottom resources explorations is proposed. The vehicle is composed of a main wing for gliding and tail wings for motion control of the vehicle. Buoyancy and center of gravity control systems, a buttery, sensors and electric devices are contained in water tight vessels under the main wing. This autonomous vehicle has an ability to achieve a long term continuous resources exploration using OBEM. The buoyancy and attitude control mechanism enables the vehicle to move to the next measurement point by gliding. The landing point for the measurement is precisely controlled by the motion control system. In this report, numerical calculations based on CFD are carried out to design a suitable main wing shape and these results are confirmed in comparison with tank experiments. The gliding performance of the vehicle which has a blended wing shape is discussed based on the calculations and the development of a prototype vehicle is also shown.
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M3 - Conference contribution
AN - SCOPUS:85038910348
T3 - Proceedings of the International Offshore and Polar Engineering Conference
SP - 326
EP - 330
BT - Proceedings of the 27th International Ocean and Polar Engineering Conference, ISOPE 2017
PB - Society of Petroleum Engineers
T2 - 27th International Ocean and Polar Engineering Conference, ISOPE 2017
Y2 - 25 June 2017 through 30 June 2017
ER -