| 摘要 |
Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined in the left-and-right direction. In the airframe position adjusting structure (1), the position adjusting unit (10) is configured such that a component force (FV), in the up-and-down direction of the airframe, of a ground reaction force (F) to be received from the ground (G) may be greater as the rolling angle (φ) when the airframe (A) touches down becomes greater. The component force (FV), in the up-and-down direction of the airframe, of the ground reaction force (F) acts as a force to return the airframe (A) to a horizontal position so that the position of the airframe (A) inclined in the left-and-right direction can be adjusted when the airframe (A) touches down.
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