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- W2039823090 abstract "The control configured vehicle concept of relaxing inherent static stability is applied here to design a modern conventional or V/STOL airship that has fixed or vectorable cruise/lift propulsors and may have auxiliary thrust vector controls for pitch and directional control augmentation. It is shown that conventional control criteria can be met while significantly reducing the required empennage surface area, vehicle aerodynamic drag, and weight by using this design approach. Although they are not a prerequisite for this application, the auxiliary thrust vector controls are found to allow greater reduction in fin size and to have favorable influence on the relaxed stability vehicle performance at low speeds. The results are illustrated here by considering an example airship of 2.8 x 10 ft." @default.
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- W2039823090 date "1991-09-01" @default.
- W2039823090 modified "2023-09-25" @default.
- W2039823090 title "Control configuration of a relaxed stability airship" @default.
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- W2039823090 doi "https://doi.org/10.2514/3.46064" @default.
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