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- W2993036360 abstract "Many engineers have attempted to optimize the design of a spacecraft structure. They usually utilize a simplified criterion or objective function (e.g., fully stressed, minimum cost) that addresses only one aspect of the design. The real-world dilemma is closer to having to select among competing designs using multiple criteria of varying importance as the time or emphasis changes. This paper presents a method for evaluating candidate designs that allows the user to assign weights to the various criteria. These weights can be altered as the program objectives change. The method makes use of the experts from the numerous disciplines involved in the design, analysis, manufacture, and operation of a spacecraft." @default.
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- W2993036360 date "1990-04-02" @default.
- W2993036360 modified "2023-09-26" @default.
- W2993036360 title "What is an Optimal Spacecraft Structure?" @default.
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- W2993036360 doi "https://doi.org/10.2514/6.1990-1051" @default.
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