ON THE DYNAMICS OF FLIGHT VEHICLE CONTRO
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Shih-Ming Yang; S.H. Chao
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Article
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1996
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Elsevier Science
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English
โ 375 KB
The influence of structure modal parameters on the dynamics of an integrated actuator and control surface system is studied in this paper. The control surface is modeled as a uniform thickness plate mounted on a push-pull hydraulic actuator. The transfer function between the command and measurement