Gui-Aee Woo , Jong-Kwon Kim , Kyeum-Rae Cho , Dae-Woo Lee
International Journal of Aeronautical and Space Sicences, vol. 5, no. 1, pp.75-82, 2004

Abstract : Nowadays, many kinds of research for airship have being studied with increase of interests in airship. But these make little progress even now. In flight test, the data acquisition from the actual flight test has lots of difficulties because the airship dynamic response is slow and sensitive to external environment. In this paper, through the actual flight test, appropriateness of the mathematical dynamic model was presented by showing the test results in various conditions. The turning, the acceleration, and the deceleration motions were tested and analyzed.

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