著者

鈴木 真之 浜本 真規子 久利 恭士 上杉 春香 小倉 正義 能勢 有希

出版者

名古屋大学

雑誌

名古屋大学大学院教育発達科学研究科紀要. 心理発達科学 (ISSN:13461729)

巻号頁・発行日

vol.52, pp.183-197, 2005

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It has been ten years since school counseling was installed into Japanese public schools. Their activities were, however, being restricted because of the several limitations. On this condition, primary protection should be focused on for school counselors to be more effective. For the first, in this article, we reviewed conventional activities that had already been conducted in school setting and that could be seen to have the characteristics of primary protection, respectively each for students, families and teachers. Secondary, we pointed out that these programs were not against the conventional Japanese education system, rather the ones that would help it. Thereafter, some of the primary protection programs that had not been prevailed yet, were introduced. Finally, in discussion, we indicated it important for school counselors to give teachers an idea of primary protection and suggested the way to install those programs into current Japanese educational setting.国立情報学研究所で電子化したコンテンツを使用している。

著者

鈴木 真之

出版者

社団法人日本化学会

雑誌

化学と教育 (ISSN:03862151)

巻号頁・発行日

vol.61, no.8, 2013-08-20

著者

鈴木 真之 内山 賢治 Derek J. BENNET Colin R. MCINNES

出版者

一般社団法人 日本航空宇宙学会

雑誌

日本航空宇宙学会論文集 (ISSN:13446460)

巻号頁・発行日

vol.59, no.693, pp.259-265, 2011 (Released:2011-10-21)

参考文献数

16

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This paper attempts to design a guidance law using bifurcating potential fields and velocity field for a swarm of autonomous Unmanned Aerial Vehicles (UAVs). We consider an autonomous flight system that can create different three-dimensional swarming patterns so as to guarantee obstacle and vehicle collision avoidance. The guidance law, which is derived from a steering and repulsive potential field, can express variable geometric patterns for a formation flight of UAVs. The system can transition between different formation patterns by way of a simple parameter change. We also describe the design method for potential field that is flexible enough to respond to a variety of UAV performance and mission. Numerical simulation is performed to verify the validity of the proposed guidance law.