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oaioai:casi.ntrs.nasa.gov:19730013107

Structural control interaction

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1973
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Abstract

The basic guidance and control concepts that lead to structural control interaction and structural dynamic loads are identified. Space vehicle ascent flight load sources and the load relieving mechanism are discussed, along with the the characteristics and special problems of both present and future space vehicles including launch vehicles, orbiting vehicles, and the Space Shuttle flyback vehicle. The special dynamics and control analyses and test problems apparent at this time are summarized

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This paper was published in NASA Technical Reports Server.

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