PRESENT STATUS OF THE SURFACE SHIP GRAVITY MEASUREMENTS ON ICEBREAKER SHIRASE

Since the advent of icebreaker SHIRASE for Antarctic research in 1983,the gravity measurements have been conducted on board the SHIRASE during the 25th, 27th, 28th, 29th, 30th, and 32nd Japanese Antarctic Research Expeditions (JARE). The ship-borne gravimeters which were employed for these measureme...

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Main Authors: フクダ ヨウイチ, トウ ヒロアキ, ノギ ヨシフミ, セガワ ジロウ, カミヌマ カツタダ, Yoichi FUKUDA, Hiroaki TOH, Yoshifumi NOGI, Jiro SEGAWA, Katsutada KAMINUMA
Format: Report
Language:English
Published: ABSTRACT 1991
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Online Access:https://nipr.repo.nii.ac.jp/?action=repository_uri&item_id=2697
http://id.nii.ac.jp/1291/00002697/
https://nipr.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2697&item_no=1&attribute_id=18&file_no=1
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Summary:Since the advent of icebreaker SHIRASE for Antarctic research in 1983,the gravity measurements have been conducted on board the SHIRASE during the 25th, 27th, 28th, 29th, 30th, and 32nd Japanese Antarctic Research Expeditions (JARE). The ship-borne gravimeters which were employed for these measurements were NIPR-ORI model-I and model-II. Both gravimeters were developed under a coordination between National Institute of Polar Research and Ocaen Research Institute, University of Tokyo. The model-I was employed before JARE-28 and the model-II, which is a newly developed one, was employed after JARE-29. The model-II gravimeter is composed of mostly the same units as those of the model-I, but the specifications of the units were upgraded. As a result the accuracy of the gravity data has been improved with increasing quantity of data obtained. There still remain some problems on the NIPR-ORI model-II gravimeter. It has a rather large sensor drift. The cause of the drift is under investigation, and we hope that the problems will be overcome in the near future. The course of the cruise is from Harumi back to Harumi, and the obtained-data cover rather wide areas not only around the Japanese Antarctic stations but also along the ship's tracks. The gravity data belonging to JARE-25 were not usable because of much irregularity caused by sensor troubles. The other data were successfully processed to be filed in the final form of gravity anomaly. The most important part of the data processing is the Eotvos corrections. The accuracy of the Eotvos corrections depends on how accurately the ship's positions can be determined. Since the positions of the SHIRASE were determined by Navy Navigation Satellite System (NNSS), we employed a new processing method by which, using the Bayes type discrete spline function, the ship's positions between successive NNSS observations can be interpolated. Because the method takes the errors of NNSS positioning into consideration, it proved superior to the ordinary methods without the error ...