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(3)  ¼ ; < L  ½. = . ,**3  +, 3 1 4 ,*+*  / 3 +. 4. Development of an Unmanned Observation Aerial Vehicle (UAV) as a Tool for Volcano Survey Kazuto SAIKI῍ and Takeshi OHBA῍῍ An unmanned aerial vehicle (UAV) named “Osaka University Sky-+” was developed as a field survey tool based on the concept that the researchers and the sta# of the municipality who investigate volcanic field were able to operate it easily, safely, and at low cost. Sky-+ is a radio control airplane with wingspan of 3* cm. It is controlled by three channel signal for motor, aileron, and elevator. Remote control distance is about .** m limited by human distance vision. The strong points of Sky-+ are as follows ; custom-designed manufacturing of the black polypropylene foam for the airframe material, an electric ducted fan is employed to secure the safety, portable on one’s back because of the new design of the airframe division, the payload that reaches -** g is secured, and achievement of the high flight performance against the strong wind around +* m/s. Field test for Sky-+ was performed at Kusatsu-Shirane volcano on +/ May ,**2. During the field tests, Sky-+ obtained movies of the crater lake and data of H, S gas concentration in the air. A training course in assembly and operation of Sky-+ was held at Osaka University and Kansai Mokei Airport (KMA) on -ῌ. August ,**2. By the field test and the training course, we proved that the development concept of Sky-+ had been achieved. Key words : Unmanned Aerial Vehicle (UAV), radio control, airplane, volcanic survey. +ῌ ῐ ῎ ῑ ῏. 5,6789:;<=>?@A:B/C&>. D EF=GHIJKL+,MNO+L. "#$%&'()*+,-./ 01 2. +,&PK-QRGS TU V%MW. X ,**.. Y! Z[\-]^G" G#$_`%9:B. aJb+,?>cd:W_e&fg9hR. / 01ijk&NO+Flmn o'p(qrR. 9:n o)_ns*>tB: aJb+,>uZ. &+v_ ,*** >,wWx5 ,**+ >y-*W. .789 zZ_uZ.>gS{h/|}7HIJ. x57+BZ  [\_~^7.:B/ (Nonami,. K_€/R_ 0‚./Bnƒ&„1&W †7. ,**1) ‡h 2Y &ˆ‰Šm*‹>ŒA/C&_. fgŽ/R>~9h-./ EE3 +31/. n 4 EF_N  +7 5 0hC&C.S (Nonami,. @r>6"&‘7_ +33+ >’“8”•>tB:C . ,**1) –9>n$—%&˜™š>›!Ž/Rœ0. †fg-G@Ah (Nogami et al., ,**+) D_n ž&. rA:B/ †Ÿ mˆ™¡¢&Ÿ ¡£¤™*¥m™. W¦-aJbˆ™Š‹' §™7Œd:†¡¨*. ©n ª,GC&«r¬­GC&®R¥m™©7¯. °mW&W±7fg9h-./ (Taddeucci et al.,.  Z[\M ²x5_³´&µ¶7·¸ o)_n. ,**1) ‡h aJb,>cd:W&Z[\79h. C~9:B/Lx5,_./R¹0/ ‡h x. R9:n aJblm)£Š™_yºW»:tc.

(4) /0*ῌ**.-  +ῌ+     Department of Earth and Space Science, Graduate School of Science, Osaka University, +ῌ+ Machikaneyama, Toyonaka /0*ῌ**.-, Osaka, Japan.

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(6)   .ῌ+ῌ+  !. Department of Chemistry, School of Science, Tokai University, .ῌ+ῌ+ Kitakaname, Hiratsuka-shi, Kanagawa ,/3ῌ+,3,, Japan. Corresponding author : Kazuto Saiki e-mail : [email protected].

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(130) 144.  . Fig. 2. A screenshot of the observation video on the H,S measurement mission. The main frame is an objective view of Sky-+ flight. Sub frame is the view of an onboard wireless video camera shooting the indicator of a portable H, S sensor. These two frame are synchronized by a video-editing software.. Fig. 3. A photo of the training course for assembly of Sky-+ at Osaka University on - August ,**2..  KMA 

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Table . Specifications of “Osaka University Sky- ”.
Fig. . Observation equipments installable on Sky- . (a) H S sensor, (b) GPS, (c) SD-video camera, (d) Wireless camera ( m range), (e) Wireless camera ( m range), and (x) Wireless camera receiver
Fig. . The flight absolute altitude of Sky- obtained by an onboard GPS and the ground elevation of the sub-airplane point on the air photography mission for the crater lake.
Fig. . A photo of the training course for assembly of objective view of Sky- flight. Sub frame is the
+2

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