NASA/SP-8079, Noll*, R. B. and Zvara*, J., Structural interaction with control systems , NASA Langley Research Center (Hampton, VA, United States), *Aerospace Systems Inc., November,1971, pp. 56, Format(s): PDF 3255k |
A monograph which assesses the state of the art of space vehicle design and development is presented. The monograph presents criteria and recommended practices for determining the structural data and a mathematical structural model of the vehicle needed for accurate prediction of structure and control-system interaction; for design to minimize undesirable interactions between the structure and the control system; and for determining techniques to achieve the maximum desirable interactions and associated structural design benefits. All space vehicles are treated, including launch vehicles, spacecraft, and entry vehicles. Important structural characteristics which affect the structural model used for structural and control-system interaction analysis are given.
| Keywords: | space vehicles, prediction analysis techniques, spacecraft control, spacecraft design, structural stability, mathematical models, quality control |
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| CASI Document ID Number: | 72N17920 |
| Subjects: | Engineering: Structural Mechanics: Structural Tests and Reliability |
| ID Code: | 114 |
| Deposited On: | 16 May 2002 |